Time Limits /

Maintenance Checks

Note: For the list of A/C effectivity supported by this manual, refer to the Aircraft
Maintenance Manual (AMM).

Publication No. BD-700 TLMC

GLOBAL EXPRESS* (MODEL BD-700-1A10)
TIME LIMITS / MAINTENANCE CHECKS

Bombardier Aerospace
P. O. Box 6087, Station Centre-ville
Montreal, Quebec, Canada H3C 3G9

http://www.cic.bombardier.com

For more information regarding Technical Publications please contact:

Bombardier Customer Services Business Aircraft

Customer Response Center (CRC)

North America: 1-866-JET-1247 (1-866-538-1247)

Outside North America: 1-514-855-2999
Fax: 1-514-855-2535
Email: bbad.user.comments@aero.bombardier.com

Distribution & Ordering

Fax: 1-514-855-2770
Email: bbad.pubs.dist@aero.bombardier.com

To ease the ordering process, the following Document

Identification Number should be used: GL 700 TLMC

It is understood that this documentation, comprising technical data and other information in any media
shall not be reproduced or disclosed in whole or in part without Bombardier's written authorization, is
proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade
secret and other intellectual property rights therein belong to Bombardier. Such documentation,
technical data and other information shall not be modified, translated, reverse assembled, reverse
engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft.

Copyright © 1998-2013 by Bombardier Inc. All rights reserved.

*Trademark of Bombardier Inc. or its subsidiaries.
Printed in Canada
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

REVISION 32 − HIGHLIGHTS

1. This package contains Revision 32 to the Bombardier Global Express®, model

BD−700−1A10, Time Limits/Maintenance Checks manual. To bring your manual up to date,
remove the superseded pages and insert the revised pages dated May 19/2021.

2. The Maintenance Planning Document has been revised concurrently with this revision.

HIGHLIGHTS − PART 2

1. In section 5−10−25, added paragraphs 1. Introduction and 2. Organization

(RS−BD700−1A10−055).

2. In section 5−10−26, revised paragraph 2. Organization (RS−BD700−1A10−055).

3. Made the changes that follow in section 5−10−30:

CHECK # RS # INTERVAL DESCRIPTION OF CHANGE

53−30−00−119* RS−BD700− Refer to Task Revised task title

1A10−069

4. Made the changes that follow in section 5−10−40:

CHECK # RS # INTERVAL DESCRIPTION OF CHANGE

27−11−35−103** RS−BD700− 30 M New task, previously issued as TR

1A10−115 5−2−51

27−11−35−104** RS−BD700− 15 M New task, previously issued as TR

1A10−115 5−2−51

This revision incorporates Temporary Revision 5−2−51.

EFFECTIVITY: ALL
Page 1
HIGHLIGHTS May 19/2021
 USER COMMENTS
ON ERRORS, OMISSIONS, PROCEDURES (IF APPLICABLE), ETC.

To: Bombardier Business Aircraft, Customer Support

Department 631 (Technical Publications and Information)

From: Date:
Address:

E−mail: Aircraft S/N:

Telephone No. (please print)

The following publication requires correction or clarification:

Publication: Page Date:

Chap./Sect. No. Page No. Para No. Fig. No.
Comments:

You can send your user comment as follows:

− by telephone at (514) 855−9304
− by e−mail to bbad.user.comments@aero.bombardier.com
− by fax at (514) 855−7894
− by mailing it to the address on the back of this page.
Bombardier Business Aircraft, Customer Support
P.O. Box 6087, Station Centre−ville
Montreal, Quebec, Canada H3C 3G9

Attn: User Comments Coordinator

Department 631
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF REVISIONS

A signature in the "INSERTED BY" column shows that

the publication holder has incorporated the revision.

REVISION NO. ISSUE DATE DATE INSERTED INSERTED BY

1 Apr 30/1999 Apr 30/1999 Bombardier

2 Nov 03/1999 Nov 03/1999 Bombardier

3 Feb 14/2000 Feb 14/2000 Bombardier

4 Oct 23/2000 Oct 23/2000 Bombardier

5 Oct 01/2001 Oct 01/2001 Bombardier

6 Jun 02/2003 Jun 02/2003 Bombardier

7 Dec 12/2003 Dec 12/2003 Bombardier

8 Mar 12/2004 Mar 12/2004 Bombardier

9 Jan 18/2005 Jan 18/2005 Bombardier

10 Mar 28/2006 Mar 28/2006 Bombardier

11 Jul 26/2007 Jul 26/2007 Bombardier

12 Jun 24/2008 Jun 24/2008 Bombardier

13 Sep 15/2008 Sep 15/2008 Bombardier

14 May 26/2010 May 26/2010 Bombardier

15 Aug 03/2010 Aug 03/2010 Bombardier

16 Nov 09/2010 Nov 09/2010 Bombardier

17 May 24/2011 May 24/2011 Bombardier

18 Nov 30/2011 Nov 30/2011 Bombardier

19 Aug 17/2012 Aug 17/2012 Bombardier

20 Aug 22/2013 Aug 22/2013 Bombardier

21 Dec 11/2013 Dec 11/2013 Bombardier

22 Nov 26/2014 Nov 26/2014 Bombardier

 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF REVISIONS

A signature in the "INSERTED BY" column shows that

the publication holder has incorporated the revision.

REVISION NO. ISSUE DATE DATE INSERTED INSERTED BY

23 May 11/2015 May 11/2015 Bombardier

24 Aug 06/2015 Aug 06/2015 Bombardier

25 Feb 10/2016 Feb 10/2016 Bombardier

26 Jul 29/2016 Jul 29/2016 Bombardier

27 Sep 06/2016 Sep 06/2016 Bombardier

28 Nov 13/2017 Nov 13/2017 Bombardier

29 May 03/2018 May 03/2018 Bombardier

30 Nov 22/2019 Nov 22/2019 Bombardier

31 Aug 17/2020 Aug 17/2020 Bombardier

32 May 19/2021 May 19/2021 Bombardier

 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF TEMPORARY REVISIONS

TEMPORARY SECTION AND PAGE ISSUE DATE INSERTED DATE REMOVED

REV. NO. NO. DATE INSERTED BY REMOVED BY

5−2−1 5−10−30 (10) Jun 30/1999 Jun 30/1999 Bombardier Dec 01/1999 REV 2

5−2−2 5−10−40 (2) Jul 08/1999 Jul 08/1999 Bombardier Dec 01/1999 REV 2

5−2−3 5−10−40 (2) Jul 26/1999 Jul 26/1999 Bombardier Dec 01/1999 REV 2

5−2−4 5−10−11 (1) Jul 14/1999 Jul 14/1999 Bombardier Dec 01/1999 REV 2

5−2−5 5−10−11 (4) Dec 23/1999 Dec 23/1999 Bombardier Feb 17/2000 REV 3

5−3−1 5−21−10 (4) Feb 07/2000 Feb 07/2000 Bombardier Oct 23/2000 REV 4

5−2−6 5−10−40 (2) Apr 25/2000 Apr 25/2000 Bombardier Oct 23/2000 REV 4

5−2−7 5−10−11 (1) Apr 25/2000 Apr 25/2000 Bombardier Jun 26/2000 TR 5−2−8

5−3−2 5−21−10 (11) Nov 14/2000 Nov 14/2000 Bombardier Oct 01/2001 REV 5

5−2−8 5−10−11 (1) Jun 26/2000 Jun 26/2000 Bombardier Oct 23/2000 REV 4

5−2−9 5−10−11 (1) Nov 20/2000 Nov 20/2000 Bombardier May 02/01 TR 5−2−15

5−2−10 5−10−30 (16) Mar 23/2001 Mar 23/2001 Bombardier Oct 01/2001 REV 5

5−2−11 5−10−30 (17) Mar 23/2001 Mar 23/2001 Bombardier Oct 01/2001 REV 5

5−2−12 5−10−30 (19) Mar 23/2001 Mar 23/2001 Bombardier Oct 01/2001 REV 5

5−2−13 5−10−30 (26) Mar 23/2001 Mar 23/2001 Bombardier Oct 01/2001 REV 5

5−2−14 5−10−30 (27) Mar 23/2001 Mar 23/2001 Bombardier Oct 01/2001 REV 5

5−2−15 5−10−11 (1) May 02/2001 May 02/2001 Bombardier Sep 05/01 TR 5−2−18

5−2−16 5−10−13 May 02/2001 May 02/2001 Bombardier Oct 01/2001 REV 5

5−2−17 5−10−40 (6) Apr 25/2001 Apr 25/2001 Bombardier Oct 01/2001 REV 5

5−2−18 5−10−11 (1) Sep 05/2001 Sep 05/2001 Bombardier Oct 01/2001 REV 5
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF TEMPORARY REVISIONS

TEMPORARY SECTION AND PAGE ISSUE DATE INSERTED DATE REMOVED

REV. NO. NO. DATE INSERTED BY REMOVED BY

5−3−3 5−21−10 (25) Apr 09/2002 Apr 09/2002 Bombardier Jun 02/2003 REV 6

5−3−4 5−21−10 (9) Aug 09/2002 Aug 09/2002 Bombardier Jun 02/2003 REV 6

5−3−5 5−21−10 (3) Sep 27/2002 Sep 27/2002 Bombardier Jun 02/2003 REV 6

5−2−19 5−10−11 (1) Nov 28/2002 Nov 28/2002 Bombardier Jun 02/2003 REV 6

5−2−20 5−10−40 (2) Mar 20/2003 Mar 20/2003 Bombardier Jun 02/03 REV 6

5−2−21 5−10−40 (3) Mar 20/2003 Mar 20/2003 Bombardier Jun 02/2003 REV 6

5−2−22 5−10−40 (5) Mar 20/2003 Mar 20/2003 Bombardier Jun 02/2003 REV 6

5−3−6 5−21−10 Jun 03/2003 Jun 03/2003 Bombardier Mar 12/2004 REV 8

5−2−23 5−10−11 (1) Nov 10/2003 Nov 10/2003 Bombardier Dec 12/2003 REV 7

5−3−7 5−23−10 (5) Jul 21/2004 Jul 21/2004 Bombardier Aug 02/2005 REV 9

5−2−24 5−10−11 (1) Apr 28/2005 Apr 28/2005 Bombardier Aug 02/2005 REV 9

5−10−20 Following
5−2−25 Apr 28/2005 Apr 28/2005 Bombardier Aug 02/2005 REV 9
5−10−19

5−2−26 5−10−30 (24) Aug 25/2005 Aug 25/2005 Bombardier Mar 28/2006 REV 10

5−2−27 5−10−30 (1) Dec 20/2005 Dec 20/2005 Bombardier Feb 03/2006 TR 5−2−28

5−3−8 5−21−10 (10) Jan 30/2006 Jan 30/2006 Bombardier Mar 28/2006 TR 5−3−9

5−2−28 5−10−30 (1) Feb 03/2006 Feb 03/2006 Bombardier Oct 01/2007 TR 5−2−33

5−3−9 5−21−10 (12) Mar 28/2006 Mar 28/2006 Bombardier Jul 26/2007 REV 11

5−3−10 5−21−10 (3) May 09/2006 May 09/2006 Bombardier Jul 26/2007 REV 11

5−2−29 5−10−11 (2) Jun 22/2006 Jun 22/2006 Bombardier Feb 26/2007 TR 5−2−30

5−2−30 5−10−11 (2) Feb 26/2007 Feb 26/2007 Bombardier Jul 26/2007 REV 11
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF TEMPORARY REVISIONS

TEMPORARY SECTION AND PAGE ISSUE DATE INSERTED DATE REMOVED

REV. NO. NO. DATE INSERTED BY REMOVED BY

5−2−31 5−10−11 (3) Feb 26/2007 Feb 26/2007 Bombardier Jul 26/2007 REV 11

5−2−32 5−10−40 (1) Mar 28/2007 Mar 28/2007 Bombardier Jul 26/2007 REV 11

5−2−33 5−10−30 (1) Oct 01/2007 Oct 01/2007 Bombardier Feb 18/2008 TR 5−2−34

5−2−34 5−10−30 (1) Feb 18/2008 Feb 18/2008 Bombardier Jun 24/2008 REV 12

5−3−11 5−22−10 (7) Jun 25/2008 Jun 25/2008 Bombardier May 26/2010 REV 14

5−2−35 5−10−30 (50) Jul 09/2008 Jul 09/2008 Bombardier Sep 15/2008 REV 13

5−3−12 5−21−10 (9) Mar 02/2009 Mar 02/2009 Bombardier May 26/2010 REV 14

5−3−13 5−21−10 (10) Mar 02/2009 Mar 02/2009 Bombardier May 26/2010 REV 14

5−2−36 5−10−20 (2) Jul 01/2009 Jul 01/2009 Bombardier May 26/2010 REV 14

5−2−37 5−10−11 (3) Jan 15/2010 Jan 15/2010 Bombardier May 26/2010 REV 14

Following Section
5−2−38 Aug 17/2010 Aug 17/2010 Bombardier Aug 17/2012 REV 19
5−10−50

5−4−1 5−30−10 (2) Sep 21/2010 Sep 21/2010 Bombardier Nov 09/2010 REV 16

5−4−2 5−30−11 (2) Sep 21/2010 Sep 21/2010 Bombardier Nov 09/2010 REV 16

5−4−3 5−30−11 (1) Sep 28/2010 Sep 28/2010 Bombardier Oct 08/2010 TR 5−4−4

5−4−4 5−30−11 (1) Oct 08/2010 Oct 08/2010 Bombardier Nov 09/2010 REV 16

5−2−39 5−10−11 (2) Apr 01/2011 Apr 01/2011 Bombardier May 24/2011 REV 17

5−4−6 5−30−11 (1) Jan 16/2012 Jan 16/2012 Bombardier Feb 28/2012 TR 5−4−7

5−2−40 5−10−20 (2) Feb 14/2012 Feb 14/2012 Bombardier Aug 17/2012 REV 19

5−1−1 5−1−1 (1) Feb 28/2012 Feb 28/2012 Bombardier Aug 17/2012 REV 19

5−4−7 Part 4 (1) Feb 28/2012 Feb 28/2012 Bombardier Aug 17/2012 REV 19
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RECORD OF TEMPORARY REVISIONS

TEMPORARY SECTION AND PAGE ISSUE DATE INSERTED DATE REMOVED

REV. NO. NO. DATE INSERTED BY REMOVED BY

5−2−41 5−10−11 (2) Jun 07/2012 Jun 07/2012 Bombardier Aug 17/2012 REV 19

5−2−42 5−10−30 (54) Aug20/2012 Aug20/2012 Bombardier Aug 22/2013 REV 20

5−2−43 5−10−11 (2) Nov 16/2012 Nov 16/2012 Bombardier Aug 22/2013 REV 20

5−3−14 5−21−10 (22) Jan 14/2013 Jan 14/2013 Bombardier Aug 22/2013 REV 20

5−3−15 5−21−10 (3) Jan 15/2013 Jan 15/2013 Bombardier Aug 22/2013 REV 20

5−2−44 5−10−11 (4) Jun 04/2014 Jun 04/2014 Bombardier Nov 26/2014 REV 22

5−2−45 5−10−30 (1) Dec 18/2014 Dec 18/2014 Bombardier May 11/2015 REV 23

5−2−46 5−10−20 (2) May 19/2015 May 19/2015 Bombardier Aug 06/2015 REV 24

5−3−16 Cancelled prior to issue Bombardier

5−3−17 5−20−05 (5) Jun 05/2015 Jun 05/2015 Bombardier Jul 29/2016 REV 26

5−3−18 5−20−05 (7) Jun 05/2015 Jun 05/2015 Bombardier Jul 29/2016 REV 26

5−2−47 5−10−40 (3) Nov 24/2015 Nov 24/2015 Bombardier Feb 10/2016 REV 25

5−2−48 5−10−30 (1) Dec 13/2016 Dec 13/2016 Bombardier Nov 13/2017 REV 28

5−2−49 5−10−20 (2) Dec 06/2017 Dec 06/2017 Bombardier May 03/2018 REV 29

5−2−50 5−10−11 (2) May 04/2018 May 04/2018 Bombardier Nov 22/2019 REV 30

5−2−51 5−10−40 (3) Dec 03/2020 Dec 03/2020 Bombardier May 19/2021 REV 32
BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 1

GENERAL

Cover
PART 1 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 1

GENERAL

LIST OF EFFECTIVE PAGES

Section Effectivity Page Date Section Effectivity Page Date

Title Page Cover Dec 11/2013 20131211

Effective Pages 1 May 19/2021 20210519

Effective Temporary
Revisions 1 May 19/2021 20210519

Contents 1 Dec 11/2013 20131211

5−00−00 ALL 1 Dec 11/2013 20131211

5−00−05 ALL 1 Dec 11/2013 20131211

2 Dec 11/2013 20131211

3 Dec 11/2013 20131211

4 Nov 22/2019 20191122

5 Nov 22/2019 20191122

6 Nov 22/2019 20191122

7 Nov 22/2019 20191122

8 Nov 22/2019 20191122

9 Nov 22/2019 20191122

10 Nov 22/2019 20191122

11 Nov 22/2019 20191122

12 Nov 22/2019 20191122

EFFECTIVITY: ALL
PART 1 Page 1
EFFECTIVE PAGES May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 1

GENERAL

LIST OF EFFECTIVE TEMPORARY REVISIONS

NO TEMPORARY REVISIONS ARE APPLICABLE AT THIS TIME

TEMPORARY PART, SECTION ISSUE DATE INSERTED DATE REMOVED

REV. NO. AND PAGE NO. DATE INSERTED BY REMOVED BY

NOTE: This list represents only those TRs which are currently in use in Part 1 of this manual.

EFFECTIVITY: ALL
PART 1 EFFECTIVE Page 1
TEMPORARY REVISIONS May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 1

GENERAL

TABLE OF CONTENTS

Subject Section Page

GENERAL 5−00−00
Introduction 5−00−05
Scope 1
Manual Organization 1
Complementary Information 2
Program Glossary and Definitions 2
Abbreviations 9

EFFECTIVITY: ALL
PART 1 Page 1
CONTENTS Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 1
SECTION 5−00−00

GENERAL

EFFECTIVITY: ALL
PART 1 Page 1
5−00−00 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

INTRODUCTION

1. Scope

The Time Limits/Maintenance Checks (TL/MC) manual shows tasks that are Airworthiness
Limitations (life limited components, airworthiness limitation items and certification
maintenance requirements) and tasks approved by the Maintenance Review Board (MRB).
These tasks are required to make sure of the continued airworthiness of the aircraft. The
Airworthiness Limitations section and MRB section are approved by Transport Canada (TC).

The MRB Report forms the basis of the manufacturer’s recommended

inspection/maintenance program. The Airworthiness Limitations section of this manual lists
the mandatory discard tasks, structures inspection tasks and system inspection tasks.
Together, these form the basis of an aircraft operator’s approved maintenance program.

The MRB Report contains the initial minimum maintenance/inspection requirements in

compliance with Instructions for Continued Airworthiness. It does not include the Mandatory
Airworthiness Inspection tasks that follow:
− Life Limited Components
− Airworthiness Limitation Items (ALI)
− Certification Maintenance Requirements (CMR).

2. Manual Organization

The TLMC manual includes the front matter that follows:

− Title Page
− Record of Revisions
− Record of Temporary Revisions
− List of Effective Pages
− List of Effective Temporary Revisions
− Table of Contents
− Transmittal Letter.

The TL/MC manual is divided into the sections that follow:

− PART 1 − 5−00−00 General
− PART 2 − 5−10−00 Airworthiness Limitations
− PART 3 − 5−20−00 Maintenance Review Board (MRB) Report

For extension tolerances to the inspection intervals, refer to the Maintenance Planning
Document (MPD).

EFFECTIVITY: ALL
PART 1 Page 1
5−00−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

3. Complementary Information

This manual has references to the manuals that follow:

− Aircraft Maintenance Manual (AMM)
− Structural Repair Manual
− Component Maintenance Manual
− Non−Destructive Test Manual.

Aircraft stations and zones data can be found in the AMM, Chapter 6.

Engine inspection procedures can be found in the Rolls−Royce publication, BR710 Engine
Maintenance Manual, M−710−2BR.

The BR−710 engine is operated under the Task Oriented Maintenance Program and has no
mandatory scheduled overhaul or hot section inspection maintenance. This program lists
borescope inspections of internal and external components and other tasks that can be done
without the removal of the engine from the airframe.

Data from the Trend Monitoring Program is intended to compliment the Task Oriented
Maintenance Program of the MRB report.

4. Program Glossary and Definitions

A. Accidental Damage

Physical deterioration of an item caused by contact or impact with an object or influence

which is not a part of the aircraft, or by human error during manufacturing, operation of
the aircraft, or maintenance practices.

B. Age Exploration

A systematic evaluation of an item based on analysis of collected information from

in−service experience. It verifies the item’s resistance to a deterioration process with
respect to increasing age.

C. Airworthiness Limitations Section

A section of the Instructions for Continued Airworthiness that contains each mandatory
replacement time, inspection interval, and related inspection procedure for structural
items (ALIs) and for systems items (CMRs). This section also includes mandatory
replacement times, inspection intervals and related inspection procedures resulting from
custom installations and/or repairs on Principal Structural Elements (PSEs). The
information contained in the Airworthiness Limitations section may be changed to reflect
service and/or test experience or new analysis methods but only with the approval of
Transport Canada.

EFFECTIVITY: ALL
PART 1 Page 2
5−00−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

D. Airworthiness Limitations Items

Mandatory structural inspections for the basic aircraft.

E. APU Cycles

One cycle equals a start or attempted start reaching at least 95 percent (RPM) APU
speed and subsequent shutdown.

F. Certification Maintenance Requirements

A required periodic task, established during the design certification of the airplane as an
operating limitation of the type certificate.

G. Corrosion

The gradual deterioration of a metal or alloy as a result of chemical interaction with its
environment.

H. Corrosion − Level 1

Corrosion damage that does not require structural reinforcement or replacement OR

corrosion occurring between successive inspections which exceeds allowable limits, but
is local and can be attributed to an event not typical of operator usage of other aircraft in
the same fleet (e.g. Mercury spill).

I. Damage Tolerant

A qualification standard for aircraft structure. An item is judged to be damage tolerant if it

can sustain damage and the remaining structure can withstand reasonable loads without
structural failure or excessive structural deformation until the damage is detected.

J. Direct Adverse Effect on Operating Safety

Direct − To be direct, the functional failure or resulting secondary damage must achieve
its effect by itself, not in combination with other functional failures (no redundancy exists
and it is a primary dispatch item).

Adverse Effect on Safety − This implies that the consequences are extremely serious or
possibly catastrophic and might cause the loss of aircraft or injury to occupants.

Operating − This is defined as the time interval during which passengers and crew are
on board for the purpose of flight.

K. Discard

The removal from service of an item at a specified life limit.

EFFECTIVITY: ALL
PART 1 Page 3
5−00−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

L. Economic Effects

Failure effects which do not prevent aircraft operation, but are economically undesirable
due to added labor and material cost for aircraft or shop repair.

M. Engine Cycles (Eng C)

An Engine Cycle is a sequence covering the aircraft taxis and takes−off until it lands and
taxis to the gate at its destination. Each Touch−and−Go operation is considered an
Engine Cycle. Each Missed Approach/Go−Around operation is considered an Engine
Cycle.

N. Engine Hours (Eng H)

See Flight Hours.

O. Environmental Deterioration

Physical deterioration of an item’s strength or resistance to failure as a result of chemical

interaction with its climate or environment.

P. Failure

The inability of an item to perform within previously specified limits.

Q. Failure Cause

Why the functional failure occurs.

R. Failure Effect

What is the result of the functional failure.

S. Fatigue Damage

The initiation of a crack or cracks due to cyclic loads and subsequent propagation.

T. Fleet Leader Concept

The concentration of sample inspections on the pieces of equipment which have the
highest operating ages to identify the first evidence of changes in their condition with
increasing age.

U. Flight Hours

Accumulated time interval between wheels−off to wheels−on.

EFFECTIVITY: ALL
PART 1 Page 4
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

V. Function

The normal characteristic actions of an item.

W. Functional Test

A quantitative test to determine if one or more functions of an item performs within

specified limits.

X. Functional Failure

How an item failed to perform its function.

Y. Hidden Function

A function which is normally active and whose cessation will not be evident to the
operating crew during performance of normal duties OR a function which is normally
inactive and whose readiness to perform, prior to it being needed, will not be evident to
the operating crew during performance of normal duties.

Z. Inherent Level of Reliability and Safety

That level which is built into the unit and, therefore, inherent in its design. This is the
highest level of reliability and safety that can be expected from a unit, system, or aircraft
if it receives effective maintenance. To achieve higher levels of reliability generally
requires modification or redesign.

AA. Inspection

An examination of an item against a specific standard.

AB. Inspection − Detailed

An intensive visual examination of a specific structural area, system installation or

assembly to detect damage, failure or irregularity. Available lighting is normally
supplemented with a direct source of good lighting at an intensity deemed appropriate by
the inspector. Inspection aids such as mirrors, hand lens, etc., surface cleaning and
elaborate access procedures may be required.

AC. Inspection − General Visual

A visual examination of an interior or exterior area, installation or assembly to detect

obvious damage, failure or irregularity. This level of inspection is made under normally
available lighting conditions such as daylight, hangar lighting, flashlight or drop−light and
may require removal or opening of access panels or doors. Stands, ladders or platforms
may be required to gain proximity to the area being checked. A General Visual
Inspection cannot be a candidate for transfer to Zonal Working Group if it originated from
a route 5 or 8.

EFFECTIVITY: ALL
PART 1 Page 5
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

AD. Inspection − Special Detailed

An intensive examination of a specific item(s), installation, or assembly to detect

damage, failure or irregularity. The examination is likely to make extensive use of
specialized inspection techniques and/or equipment. Intricate cleaning and substantial
access or disassembly procedure may be required.

AE. Item

Any level of hardware assembly (i.e.: system, sub−system, module, accessory,

component, unit, part, etc.).

AF. Landing

A sequence covering the approach and touchdown phases. Each touch−and−go

operation is considered a landing.

AG. Life−Limited Items

An item which must be removed from service and discarded before a specified time is
achieved.

AH. Lubrication and Servicing

Any act of lubricating or servicing for the purpose of maintaining inherent design
capabilities.

AI. Maintenance Significant Item

Items identified by the manufacturer whose failure

(1) could affect safety (on ground or in flight), and/or

(2) is undetectable during operations, and/or

(3) could have significant operational impact, and/or

(4) could have significant economic impact.

AJ. Multiple Site Fatigue Damage

The presence of a number of adjacent small cracks that might coalesce to form a single
long crack.

AK. Operating Crew Normal Duties

Operating Crew − Qualified cockpit and cabin attendant personnel who are on duty.

EFFECTIVITY: ALL
PART 1 Page 6
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

Normal Duties − Those duties associated with the routine operation of the aircraft, on a
daily basis, to include the following:

(1) Procedures and checks performed during aircraft operation;

(2) Recognition of abnormalities or failures by the operating crew through the use of
normal physical senses (e.g., odor, noise, vibration, temperature, visual observation
of damage or failure, changes in physical input force requirements, etc.)

AL. Operational Effects

Failure effects which interfere with the completion of the aircraft mission. These failures
cause delays, cancellations, ground or flight interruptions, high drag coefficients, altitude
restrictions, etc.

AM. Operational Test

An operational test is a task to determine that an item is fulfilling its intended purpose.
This test does not require quantitative tolerances. This is a failure finding task.

AN. Other Structure

Structure which is judged not to be a Structural Significant Item. "Other Structure" is

defined both externally and internally within zonal boundaries.

AO. Principal Structural Element (PSE)

Elements of primary structure which contribute significantly to carrying flight, ground,

pressurization or control loads, and whose failure could result in catastrophic failure of
the airplane. PSEs are a subset of SSIs (every PSE is an SSI or contained within an
SSI).

AP. Residual Strength

The strength of a damaged structure.

AQ. Restoration

That work necessary to return the item to a specific standard. Restoration may vary from
cleaning or replacement of single parts up to a complete overhaul.

AR. Safe Life Limit

Time at which safe−life component must be removed from service.

EFFECTIVITY: ALL
PART 1 Page 7
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

AS. Safe Life Structure

Structure which can withstand the repeated loads of variable magnitude expected during
its service life without detectable cracks,

AT. Scheduled Maintenance Check

Any of the maintenance opportunities which are prepackaged and are accomplished on
a regular basis.

AU. Structural Assembly

One or more structural elements which together provide a basic structural function.

AV. Structural Detail

The lowest functional level in an aircraft structure. A discrete region or area of a

structural element, or a boundary intersection of two or more elements.

AW. Structural Element

Two or more structural details which together form an identified manufacturer’s assembly
part.

AX. Structural Function

The mode of action of aircraft structure. It includes acceptance and transfer of specific
loads in items (details/elements/assemblies) and provides consistently adequate aircraft
response and flight characteristics.

AY. Structural Significant Item

Any detail, element or assembly, which contributes significantly to carrying flight, ground,
pressure or control loads and whose failure could affect the structural integrity necessary
for the safety of the aircraft.

AZ. Tasks − Maintenance

An action or set of actions required to achieve a desired outcome which restores an item
to, or maintains an item in serviceable condition, including inspection and determination
of condition.

BA. Threshold

The initial accomplishment of a specific maintenance task expressed in flight cycle, flight
hours, and/or calendar time

EFFECTIVITY: ALL
PART 1 Page 8
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

BB. Visual Check

A visual check is an observation to determine that an item is fulfilling its intended

purpose. Does not require quantitative tolerances. This is a failure finding task.

5. Abbreviations

AC Advisory Circular
ACO Aircraft Certification Office
AD Accidental Damage
AEG Aircraft Evaluation Group
AFCS Automatic Flight Control System
ALI Airworthiness Limitation Item
AMA Airworthiness Manual Advisory
AMM Aircraft Maintenance Manual
AMTOSS Aircraft Maintenance Task Oriented Support System
APU Auxiliary Power Unit
ATA Air Transport Association
ATC Air Traffic Control
BBA Bombardier Business Aircraft
BL Buttock Line
CAIMS Central Aircraft Information and Maintenance System
CCMR Candidate Certification Maintenance Requirement
CIC Corrosion Inhibiting Compound
CMM Component Maintenance Manual
CMR Certification Maintenance Requirements
CPCP Corrosion Prevention and Control Program
CRES Corrosion Resistant Steel
DI Detailed Inspection
DME Distance Measuring Equipment
DTR Damage Tolerance Rating
ED Environmental Deterioration

EFFECTIVITY: ALL
PART 1 Page 9
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

EFIS Electronic Flight Instrument System

EICAS Engine Indicating and Crew Alerting System
ELT Emergency Locator Transmitter
FAA Federal Aviation Administration (USA)
FAR Federal Aviation Regulation
FC Flight Cycles
FD Fatigue Damage
FMEA Failure Mode and Effects Analysis
FMQGC Flight Management and Quantity Gauging Computer
FMS Flight Management System
FOD Foreign Object Damage
FS Fuselage Station
GPS Global Positioning System
GPWS Ground Proximity Warning System
GVI General Visual Inspection
H Hours
HASC High Altitude Special Condition
ICA Instructions for Continued Airworthiness
IRS Inertial Reference System
ISC Industry Steering Committee
IWG Industry Working Group
JAA Joint Aviation Authorities
JAR Joint Aviation Requirements
L Landings
L/HIRF Lightning/High Intensity Radiated Field
LBL Left Buttock Line
LEP List of Effective Pages
LRU Line Replaceable Unit
M Months
ME Maintenance Engineering

EFFECTIVITY: ALL
PART 1 Page 10
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

MEL Minimum Equipment List

MMEL Master Minimum Equipment List
MLG Main Landing Gear
MPD Maintenance Planning Document
MPE Maintenance Planning Engineering
MPP Maintenance Program Proposal
MPS Material Process Specification
MRB Maintenance Review Board
MSG−3 Maintenance Steering Group − 3rd Task Force
MSI Maintenance Significant Item
MTBF Mean Time Between Failure
MTBUR Mean Time Between Unscheduled Removal
NDI Non−Destructive Inspection
NDT Non−Destructive Test
NLG Nose Landing Gear
P/N Part Number
PPH Policy and Procedures Handbook
PROP Propulsion
PSE Principal Structural Element
R Repeat
RBL Right Buttock Line
REF Reference
REO Repair Engineering Order
REV Revision
SACD Structural Airworthiness Control Document
SATCOM Satellite Communication System
SB Service Bulletin
SDI Special Detailed Inspection
SID Supplemental Inspection Document
SIP Structural Inspection Program

EFFECTIVITY: ALL
PART 1 Page 11
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

SRM Structural Repair Manual

SSA System Safety Analysis
SSI Structural Significant Item
STR Stringer
STRU Structures
SWG Structural Working Group
SYS System
T Threshold
TBD To Be Determined
TC Transport Canada
TCAS Traffic Alert and Collision Avoidance System
TLMC Time Limits/Maintenance Checks
TR Temporary Revision
TSOP Technical Support Operating Procedure
VS Vertical Stabilizer
WG Working Group
WL Waterline
WS Wing Stations
ZIN Zonal Identification Number
ZL Zonal
ZWG Zonal Working Group

EFFECTIVITY: ALL
PART 1 Page 12
5−00−05 Nov 22/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2

AIRWORTHINESS LIMITATIONS

The Airworthiness Limitations section is approved by Transport Canada and specifies

maintenance required by any applicable airworthiness or operational rule unless an alternative
program has been approved by the Minister of Transport.

Approved by: (Signed original page on file at Bombardier)

Chief, Engineering,
Aircraft Certification Branch
Transport Canada

Cover
PART 2 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2

AIRWORTHINESS LIMITATIONS

LIST OF EFFECTIVE PAGES

Section Effectivity Page Date Section Effectivity Page Date

Title Page Cover Dec 11/2013 20131211 5−10−19 Cover Dec 11/2013 20131211

Effective Pages 1 May 19/2021 20210519 5−10−19 ALL 1 Dec 11/2013 20131211

2 May 19/2021 20210519

3 May 19/2021 20210519 5−10−20 ALL 1 Dec 11/2013 20131211

2 May 03/2018 20180503

Effective Temporary
Revisions 1 May 19/2021 20210519 5−10−25 Cover Dec 11/2013 20131211

Contents 1 May 19/2021 20210519 5−10−25 ALL 1 May 19/2021 20210519

5−10−00 ALL 1 Dec 11/2013 20131211 5−10−26 Cover Dec 11/2013 20131211

5−10−05 ALL 1 Dec 11/2013 20131211 5−10−26 ALL 1 May 19/2021 20210519

2 Dec 11/2013 20131211

3 Dec 11/2013 20131211 5−10−30 Cover Dec 11/2013 20131211

4 Dec 11/2013 20131211

5 Dec 11/2013 20131211 5−10−30 ALL 1 Nov 13/2017 20171113

6 Dec 11/2013 20131211 2 Sep 06/2016 20160906

7 Dec 11/2013 20131211 3 Sep 06/2016 20160906

8 Dec 11/2013 20131211 4 May 03/2018 20180503

5 May 03/2018 20180503

5−10−10 ALL 1 Dec 11/2013 20131211 6 May 03/2018 20180503

2 Dec 11/2013 20131211 7 May 03/2018 20180503

3 Dec 11/2013 20131211 8 May 03/2018 20180503

4 Dec 11/2013 20131211 9 May 03/2018 20180503

10 May 03/2018 20180503

5−10−11 ALL 1 Dec 11/2013 20131211 11 May 03/2018 20180503

2 Nov 22/2019 20191122 12 May 03/2018 20180503

3 Aug 17/2020 20200817 13 May 03/2018 20180503

4 Aug 17/2020 20200817 14 May 03/2018 20180503

15 May 03/2018 20180503

5−10−13 ALL 1 Dec 11/2013 20131211 16 May 03/2018 20180503

2 Dec 11/2013 20131211 17 May 03/2018 20180503

18 May 03/2018 20180503

19 May 03/2018 20180503

20 May 03/2018 20180503

21 May 03/2018 20180503

EFFECTIVITY: ALL
PART 2 Page 1
EFFECTIVE PAGES May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

Section Effectivity Page Date Section Effectivity Page Date

5−10−30 ALL 22 May 03/2018 20180503 5−10−30 ALL 70 May 03/2018 20180503

23 May 03/2018 20180503 71 May 03/2018 20180503

24 May 03/2018 20180503 72 May 03/2018 20180503

25 May 03/2018 20180503 73 May 03/2018 20180503

26 May 03/2018 20180503 74 May 03/2018 20180503

27 May 03/2018 20180503 75 May 03/2018 20180503

28 May 03/2018 20180503 76 May 03/2018 20180503

29 May 03/2018 20180503 77 May 03/2018 20180503

30 May 19/2021 20210519 78 May 03/2018 20180503

31 May 03/2018 20180503 79 May 03/2018 20180503

32 May 03/2018 20180503 80 May 03/2018 20180503

33 May 03/2018 20180503 81 May 03/2018 20180503

34 May 03/2018 20180503 82 May 03/2018 20180503

35 May 03/2018 20180503 83 May 03/2018 20180503

36 May 03/2018 20180503 84 May 03/2018 20180503

37 May 03/2018 20180503 85 May 03/2018 20180503

38 May 03/2018 20180503 86 May 03/2018 20180503

39 May 03/2018 20180503 87 May 03/2018 20180503

40 May 03/2018 20180503 88 May 03/2018 20180503

41 May 03/2018 20180503 89 May 03/2018 20180503

42 May 03/2018 20180503 90 May 03/2018 20180503

43 May 03/2018 20180503 91 May 03/2018 20180503

44 May 03/2018 20180503 92 May 03/2018 20180503

45 May 03/2018 20180503 93 May 03/2018 20180503

46 May 03/2018 20180503 94 May 03/2018 20180503

47 May 03/2018 20180503 95 May 03/2018 20180503

48 May 03/2018 20180503 96 May 03/2018 20180503

49 May 03/2018 20180503 97 May 03/2018 20180503

50 May 03/2018 20180503 98 May 03/2018 20180503

51 May 03/2018 20180503 99 May 03/2018 20180503

52 May 03/2018 20180503 100 May 03/2018 20180503

53 May 03/2018 20180503 101 May 03/2018 20180503

54 May 03/2018 20180503 102 May 03/2018 20180503

55 May 03/2018 20180503 103 May 03/2018 20180503

56 May 03/2018 20180503 104 May 03/2018 20180503

57 May 03/2018 20180503 105 May 03/2018 20180503

58 May 03/2018 20180503 106 May 03/2018 20180503

59 May 03/2018 20180503 107 May 03/2018 20180503

60 May 03/2018 20180503 108 May 03/2018 20180503

61 May 03/2018 20180503 109 May 03/2018 20180503

62 May 03/2018 20180503 110 May 03/2018 20180503

63 May 03/2018 20180503 111 May 03/2018 20180503

64 May 03/2018 20180503

65 May 03/2018 20180503 5−10−40 Cover Dec 11/2013 20131211

66 May 03/2018 20180503

67 May 03/2018 20180503

68 May 03/2018 20180503

69 May 03/2018 20180503

EFFECTIVITY: ALL
PART 2 Page 2
EFFECTIVE PAGES May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

Section Effectivity Page Date Section Effectivity Page Date

5−10−40 ALL 1 Nov 26/2014 20141126

2 Dec 11/2013 20131211

3 May 19/2021 20210519

4 May 19/2021 20210519

5 May 19/2021 20210519

6 May 19/2021 20210519

7 May 19/2021 20210519

8 May 19/2021 20210519

9 May 19/2021 20210519

10 May 19/2021 20210519

11 May 19/2021 20210519

5−10−50 Cover Dec 11/2013 20131211

5−10−50 ALL 1 Dec 11/2013 20131211

2 Dec 11/2013 20131211

3 Dec 11/2013 20131211

4 Dec 11/2013 20131211

5 Dec 11/2013 20131211

6 Dec 11/2013 20131211

7 Dec 11/2013 20131211

8 Dec 11/2013 20131211

9 Dec 11/2013 20131211

10 Dec 11/2013 20131211

11 Dec 11/2013 20131211

12 Dec 11/2013 20131211

13 Dec 11/2013 20131211

5−10−90 ALL 1 Dec 11/2013 20131211

2 Dec 11/2013 20131211

3 Dec 11/2013 20131211

4 Nov 22/2019 20191122

EFFECTIVITY: ALL
PART 2 Page 3
EFFECTIVE PAGES May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2

AIRWORTHINESS LIMITATIONS

LIST OF EFFECTIVE TEMPORARY REVISIONS

NO TEMPORARY REVISIONS ARE APPLICABLE AT THIS TIME

TEMPORARY PART, SECTION ISSUE DATE INSERTED DATE REMOVED

REV. NO. AND PAGE NO. DATE INSERTED BY REMOVED BY

NOTE: This list represents only those TRs which are currently in use in Part 2 of this manual.

EFFECTIVITY: ALL
PART 2 EFFECTIVE Page 1
TEMPORARY REVISIONS May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2

AIRWORTHINESS LIMITATIONS

TABLE OF CONTENTS

Subject Section Page

AIRWORTHINESS LIMITATIONS 5−10−00

Introduction and Rules 5−10−05
General 1
Scope 1
Records and Reports 4
Airworthiness Limitations 4
Certification Maintenance Requirements 5
High Altitude Special Conditions (HASC) 8
Life Limits (Structures) 5−10−10
Life Limits (Systems) 5−10−11
RVSM Qualified Aircraft 5−10−13
Time Limits by Aircraft Effectivity 5−10−19
Introduction 1
Organization 1
Time Limits − Supplementary Limitations 5−10−20
Tasks by Aircraft Effectivity − Custom Installations 5−10−25
Introduction 1
Organization 1
Tasks by Aircraft Effectivity − Repairs 5−10−26
Introduction 1
Organization 1
Airworthiness Limitation Items 5−10−30
Certification Maintenance Requirements 5−10−40
High Altitude Special Conditions Requirements 5−10−50
Life Limits (Structures) 5−10−90

EFFECTIVITY: ALL
PART 2 Page 1
CONTENTS May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−00

AIRWORTHINESS LIMITATIONS

EFFECTIVITY: ALL
PART 2 Page 1
5−10−00 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

INTRODUCTION AND RULES

1. General

The Airworthiness Limitations section is approved by Transport Canada (TC). It shows the
mandatory maintenance required by the Airworthiness Manual, chapter 525.1529, Appendix
H. The rules applicable to Certification Maintenance Requirements (CMRs) are shown in
paragraph 5.

2. Scope

All airworthiness limitation maintenance tasks are identified with a * (one star) or a ** (two
stars).

* (one star) shows that the task is mandatory and cannot be changed, escalated (increased)
or deleted without the approval of the certification airworthiness authority.

** (two stars) shows that the task interval can be adjusted to agree with an operator’s
approved escalation practices or an approved reliability program, but the task can not be
changed or deleted without prior approval of the airworthiness authority.

The tasks included in this section are as follows:

NOTE: The life limits for individual engine components are given in BMW Rolls−Royce
Time Limits Manual T−710−2BR, sections 05−10−01, 5−10−02 and 5−10−03.

A. Life Limits − Structures (Section 5−10−10)

These tasks are discard tasks which make sure that structural items are discarded
before critical failure occurs.

B. Life Limits − Systems (Section 5−10−11)

These tasks are discard tasks which make sure that items are discarded before critical
failure occurs.

C. Aircraft Operation in RVSM Airspace (Section 5−10−13)

Tasks in this section are required to ensure continued airworthiness of aircraft that fly in
Reduced Vertical Separation Minimum (RVSM) airspace.

D. Airworthiness Limitation Tasks by Aircraft Effectivity (Section 5−10−19)

This shows discard tasks (retirement lives) for structural components on specific aircraft.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

E. Supplementary Airworthiness Limitation Tasks (Section 5−10−20)

This section lists supplementary maintenance limitations. These tasks are required to
ensure continued airworthiness of the aircraft.

F. Airworthiness Limitation Tasks by Aircraft Effectivity (Section 5−10−25/26)

These are maintenance tasks due to structural repairs, systems changes and custom
installations done on individual aircraft or groups of aircraft.

These tasks must be controlled by the operator. Operators receive only those pages
which show tasks applicable to their aircraft. A combined list of effective
pages/transmittal letter is given for each aircraft, if applicable, and is revised as required.

G. Airworthiness Limitation Tasks by Chapter 5 Task Number (Section 5−10−30)

The tasks are the mandatory structural inspections for the basic aircraft.

(1) The first (left) column contains the engineering source document and the revision
level for the specific Principal Structural Elements (PSE).

(2) The second column contains the ATA number of the PSE as shown in the source
document in the first column.

(3) The third column contains the Task Number. It is made up of 4 parts
XX−XX−XX−YZZ and a *(one star). The description of the parts is as follows:
− XX−XX−XX is the ATA number.
− Y is 1 to show a mandatory, non−escalatable (see Rule 4.A.)
airworthiness−limitation task.
− ZZ is the task sequence identifier. The task sequence identifier starts at 01 for
each variation to the full ATA number sequence of the Task Number.

(4) The fourth column contains the task title. This title includes the inspection level and
a brief description of the area or items to be inspected.

(5) The fifth column contains the inspection intervals threshold (T) and repeat (R)
values which are the maximum allowable as approved by Transport Canada. The
repeat interval is defined from the last time that particular task was done. The
inspection intervals in this column are in landings (L).

H. CMR Tasks by Chapter 5 Task Number (Section 5−10−40)

These are maintenance tasks due to aircraft system safety analysis. The tasks are the
mandatory systems tasks for the basic aircraft.

(1) The first (left) column contains the engineering source document and the revision
level for the specific CMR.

EFFECTIVITY: ALL
PART 2 Page 2
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

(2) The second column shows the paragraph number of the source document shown in
the first column.

(3) The third column shows the Task Number. It is made up of 4 parts
XX−XX−XX−YZZ and either a * (one star) or ** (two stars). The description of the
parts is as follows:
− XX−XX−XX is the ATA number.
− Y is 1 to show a mandatory CMR task.
− ZZ is the task sequence identifier. The task sequence identifier starts at 01 for
each variation to the full ATA number sequence of the Task Number.

(4) The fourth column contains the task title. The title shows the type of task and a brief
description of the system.

(5) The fifth column contains the task intervals. The task interval is defined from the
last time that particular task was done. The task intervals in this column are Hours
(H), Months (M) or Landings (L).

If two intervals are shown, for example 1000 H and 24 M, the task must be done at
whichever interval occurs first. The task is repeated at whichever interval occurs
first from the last time the task was done.

(6) The sixth column shows the exceptional short term interval extension that can be
used to cover an uncontrollable or unexpected situation (see Rule 5.A.). The time
intervals are hours (H), months (M) or landings (L). If there is no data in this column
for a given task, then there is no allowable extension.

I. HASC Tasks by Chapter 5 Task Number (Section 5−10−50)

These tasks are mandatory structural inspections required for aircraft certified for flight
above 41,000 feet, required in accordance with airworthiness regulations. The tasks are
considered safety tasks, whose intervals are not escalatable.

(1) The first (left) column contains the engineering source document and the revision
level.

(2) The second column shows the requirement source.

(3) The third column shows the Task Number. It is made up of 4 parts
XX−XX−XX−YZZ and a * (one star). The description of the parts is as follows:
− XX−XX−XX is the ATA number.
− Y is 1 to show a mandatory, non−escalatable (see Rule 6.A.) airworthiness
limitation task.
− ZZ is the task sequence identifier. The task sequence identifier starts at 01 for
each variation to the full ATA number sequence of the Task Number.

(4) The fourth column contains the task title. This title includes the inspection level and
a brief description of the area or items to be inspected.

EFFECTIVITY: ALL
PART 2 Page 3
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

(5) The fifth column contains the inspection intervals threshold (T) and repeat (R)
values which are the maximum allowable as approved by Transport Canada. The
repeat interval is defined from the last time that particular task was done. The
inspection intervals in this column are in landings (L).

3. Records and Reports

Operators must report any event that affects the continued airworthiness of the aircraft to the
applicable airworthiness authority and Bombardier Aerospace (Canadair), Maintenance
Engineering (ME).

A record of the maintenance tasks that are done on the aircraft must be made. The record
must include signatures or stamps of the persons that were authorized to do the tasks.

Records on all components affected by tasks and replacements must be made.

4. Airworthiness Limitations

The rules that follow are applicable to Airworthiness Limitations (Section 5−10−30).

A. The aircraft is Type Approved as Damage Tolerant, and as a result, some maintenance
tasks are mandatory. These tasks are identified with a * (one star) and cannot be deleted
from the program. The check intervals cannot be increased without the approval of
Aircraft Certification Branch of Transport Canada or other applicable foreign
airworthiness authorities.

B. The Inspection Program in section 5−10−30 has been substantiated as follows (Aircraft
Initial Design Goal):

(1) 25000 landings for metallic structure on aircraft operating at 93,500 lbs MTOW or
96,000 lbs MTOW, Pre SB 700−21−034

(2) 15000 landings for metallic structure on aircraft operating at 98,000 lbs MTOW or
99,500 lbs MTOW, or any aircraft Post SB 700−21−034

(3) 15000 landings for composite structure.

Operation beyond the above limits requires additional substantiation and operators
wishing to do so should contact Bombardier for the development of a Supplemental
Structural Integrity Document.

C. Mandatory tasks from the damage tolerance evaluation are divided into the two time
intervals that follow:

(1) Threshold (T) tasks are done once only at or before the aircraft time value shown.
This time period is measured from the zero time of the aircraft.

EFFECTIVITY: ALL
PART 2 Page 4
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

(2) Repeat (R) tasks are done at or before the interval shown. This interval is
measured from when the threshold or last repeat check was done.

D. Any task with a repeat (R) interval only, must be incorporated into the aircraft inspection
program at or before this interval (R), unless required earlier to comply with the
inspection frequency defined in an airworthiness directive.

5. Certification Maintenance Requirements

The rules that follow are applicable to Certification Maintenance Requirements (Section
5−10−40).

A. The number or value in the sixth column (Allowable Extension) represents a short term
increase of a CMR interval that can be used when an uncontrollable or unexpected
situation prevents the accomplishment of a task at its prescribed interval. Operators
should notify their local regulatory authorities (as required) as soon as practical
whenever an extension has been used.

CMR tasks with a NOTE A in the sixth column (Allowable Extension) have an
"Allowable Task Tolerance", the value of which is indicated above the NOTE A . This
gives the start and end of the envelope for the published interval in column 5.

In accordance with the definition of the "Allowable Task Tolerance":

− If a CMR task is accomplished within the +/− "Allowable Task Tolerance" envelope,
the next due time shall be calculated from the time at which the CMR task was
initially due, not from the point of completion of the task (as explained in examples A
and B).
− If a task is accomplished early, before the start of the "Allowable Task Tolerance"
envelope, the next due point envelope starts earlier by the same amount. The length
of the envelope remains unchanged (as explained in example C).
− A task cannot be accomplished later than the maximum "Allowable Task Tolerance"
limit. Local regulatory authorities must approve, prior to use, any desired extension
beyond the maximum "Allowable Task Tolerance" unless first approved in
accordance with local regulatory requirements.

Example A (Refer to Figure 1)

Inspections accomplished late, but within the "Allowable Task Tolerance" must have that
period subtracted from the interval at which the inspection was accomplished, in order to
keep the original schedule.

Using a "500 hours" or "15 months" interval as an example, an inspection due at 1000
hours or 30 months is done at 1040 hours or 32 months (within the "Allowable Task
Tolerance"). The next inspection window will be centered at:

time accomplished (1040H) − late period (40H) + TLMC interval (500H) = next inspection
window center (1500H)

EFFECTIVITY: ALL
PART 2 Page 5
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

or

time accomplished (32M) − late period (2M) + TLMC interval (15M) = next inspection
window center (45M)

Example B (Refer to Figure 1)

Inspections accomplished early, but within the Allowable Task Tolerance envelope, must
have that early period added to the interval at which the next inspection was
accomplished, in order to keep the original schedule.

Using a "500 hours" or"15 months" TLMC interval as an example, an inspection due at
1000 hours or 30 months is accomplished at 960 hours or 28 months (within the
"Allowable Task Tolerance"), the next inspection window will be centered at:

time accomplished (960H) + early (40H) + TLMC interval (500H) = next inspection
window center (1500H)

or

time accomplished (28M) + early (2M) + TLMC interval (15M) = next inspection window
center (45M)

Example C (Refer to Figure 1)

Inspections accomplished earlier than the minimum value of the "Allowable Task
Tolerance" envelope will require a new schedule.

Using a "500 hours" or"15 months" interval as an example, an inspection due at 1000
hours or 30 months is accomplished at 900 hours or 24 months (not within the"Allowable
Task Tolerance"). The next inspection window will be centered at:

time accomplished (900H) + minimum "Allowable Task Tolerance" (50H) + TLMC

interval (500H) = next inspection window center (1450H)

or

time accomplished (24M) + minimum "Allowable Task Tolerance" (3M) + TLMC interval
(15M) = next inspection window center (42M)

EFFECTIVITY: ALL
PART 2 Page 6
5−10−05 Dec 11/2013
 INSPECTION DUE AT 1000H OR 30M NEXT INSPECTION DUE AT 1500H OR 45M
(+/−50H OR 3M) (+/−50H OR 3M)
−50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE −50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE
TASK TOLERANCE TASK TOLERANCE TASK TOLERANCE TASK TOLERANCE

EFFECTIVITY:
950H OR 27M 1050H OR 33M 1450H OR 42M 1550H OR 48M

ALL
INSPECTION DONE LATE AT 1040H OR 32M
(WITHIN ALLOWABLE TASK TOLERANCE)

INSPECTION DUE AT 1000H OR 30M NEXT INSPECTION DUE AT 1500H OR 45M

(+/−50H OR 3M) (+/−50H OR 3M)
−50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE −50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE
TASK TOLERANCE TASK TOLERANCE TASK TOLERANCE TASK TOLERANCE

Figure 1
950H OR 27M 1050H OR 33M 1450H OR 42M 1550H OR 48M

INSPECTION DONE EARLY AT 960H OR 28M

(WITHIN ALLOWABLE TASK TOLERANCE)

NEW SCHEDULE:
BD−700 TIME LIMITS/MAINTENANCE CHECKS

INSPECTION DUE AT 1000H OR 30M NEXT INSPECTION DUE AT 1450H OR 42M

Examples of Allowable Task Tolerances

(+/−50H OR 3M) (+/−50H OR 3M)
−50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE
TASK TOLERANCE TASK TOLERANCE

5−10−05
PART 2
950H OR 27M 1050H OR 33M 1400H OR 39M 1500H OR 45M
−50H OR −3M ALLOWABLE +50H OR +3M ALLOWABLE
INSPECTION DONE EARLY AT 900H OR 24M TASK TOLERANCE TASK TOLERANCE
(NOT WITHIN ALLOWABLE TASK TOLERANCE)

GMP_021

Dec 11/2013
Page 7
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

6. High Altitude Special Conditions (HASC)

The rules that follow are applicable to High Altitude Special Conditions (HASC) (Section
5−10−50).

A. These mandatory tasks are classified as safety related tasks, whose intervals cannot be
increased without the approval of Aircraft Certification Branch of Transport Canada or
other applicable foreign airworthiness authority.

B. The published intervals are defined as follows:

(1) Due time for the Threshold (T) inspection is calculated from zero time of the aircraft.

(2) Due time for a Repeat (R) inspection is calculated using the published Repeat (R)
interval. The inspection is done at or before the time calculated from the last time
the inspection was done.

EFFECTIVITY: ALL
PART 2 Page 8
5−10−05 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

LIFE LIMITS (STRUCTURES)

1. The structural life limits of the Safe−Life items shown on the pages that follow are taken from
the Structural Airworthiness Control Document. Discard is mandatory at the expiry of the
specified structural life limit for the item. These life limit values may be superseded by the life
limits contained in section 5−10−19, for specific serialized components.

NOTES: [1] Individual Main and Nose Landing Gear component utilization must be
recorded from the time of initial installation.

[2] If no dash number is specified, the life limit is applicable to all the dash
numbers of the part numbers listed.

[3] For aircraft under the Commonwealth of Independent States (CIS) (Russia)
operations, the life limits in section 5−10−10 must be superseded by those in
section 5−10−90. Section 5−10−90 is available as a supplement from
Bombardier Business Aircraft Technical Publications.

[4] The non−serialized pin/bolts must be discarded on removal from aircraft and at
intervals not exceeding the discard time presented in this section.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−10 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−11−01−101 * Discard the Main Landing Gear (MLG) Connecting Shock 15000 L
Rev. E4 32−11−105 (one star) Strut/Trailing Arm Pin, Part No. 21115 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−11−01−102 * Discard the Main Landing Gear (MLG) Connecting Shock 15000 L
Rev. E4 32−11−105 (one star) Strut/Main Fitting Pin, Part No. 21260 and 21274−1 COMPONENT

RAS−C700−990 32−11−01−103 * Discard the Main Landing Gear (MLG) Shock Strut 15000 L
Rev. E4 32−11−105 (one star) Cylinder, Part No. 21206 and 21209 COMPONENT

RAS−C700−990 32−11−01−104 * Discard the Main Landing Gear (MLG) Shock Strut Piston, 15000 L
Rev. E4 32−11−105 (one star) Part No. 21216 and 21218 COMPONENT

RAS−C700−990 32−11−01−105 * Discard the Main Landing Gear (MLG) Connecting Shock 10999 L
Rev. E4 32−11−105 (one star) Strut/Trailing Arm Pin, Part No. 21194−1 COMPONENT

RAS−C700−990 32−11−09−101 * Discard the Main Landing Gear (MLG) Trailing Arm/Axle, 15000 L
Rev. E4 32−11−103 (one star) Part No. 21410 COMPONENT
32−11−106

RAS−C700−990 32−11−09−102 * Discard the Main Landing Gear (MLG) Pivot Pin, Part No. 15000 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Rev. E4 32−11−103 (one star) 21114 COMPONENT

RAS−C700−990 32−11−17−101 * Discard the Main Landing Gear (MLG) Side−Stay 11168 L
Rev. E4 32−11−104 (one star) Lower−Pin, Part No. 21113 COMPONENT

RAS−C700−990 32−11−17−102 * Discard the Main Landing Gear (MLG) Side Brace Rod 8683 L

5−10−10
PART 2
Rev. E4 32−11−104 (one star) End, Part No. 21510 COMPONENT

RAS−C700−990 32−11−17−103 * Discard the Main Landing Gear (MLG) Side Brace Piston, 8683 L
Rev. E4 32−11−104 (one star) Part No. 21512 COMPONENT

Dec 11/2013
Page 2
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−11−17−104 * Discard the Main Landing Gear (MLG) Side Brace Cylinder, 8683 L
Rev. E4 32−11−104 (one star) Part No. 21521 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−11−29−101 * Discard the Main Landing Gear (MLG) Main Fitting, Part 15000 L
Rev. E4 32−11−102 (one star) No. 21310 COMPONENT

RAS−C700−990 32−11−29−102 * Discard the Main Landing Gear (MLG) Pintle Pin, Part No. 11271 L
Rev. E4 32−11−102 (one star) 21112 COMPONENT

RAS−C700−990 32−11−29−103 * Discard the Main Landing Gear (MLG) Pintle Pin/Cross Pin, 15000 L
Rev. E4 32−11−102 (one star) Part No. 21116−1 COMPONENT

RAS−C700−990 32−21−01−101 * Discard the Nose Landing Gear (NLG) Shock Strut Axle, 15000 L
Rev. E4 32−21−105 (one star) Part No. 1286−0201 and 1286−0203 COMPONENT

RAS−C700−990 32−21−01−102 * Discard the Nose Landing Gear (NLG) Shock Strut Piston 15000 L
Rev. E4 32−21−103 (one star) (Sliding Tube), Part No. 1286−0001 and 1286−0077 COMPONENT

RAS−C700−990 32−21−01−103 * Discard the Nose Landing Gear (NLG) Shock Strut Main 11295 L
Rev. E4 32−21−102 (one star) Fitting, Part No. 1286−0101 COMPONENT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RAS−C700−990 32−21−05−101 * Discard the Nose Landing Gear (NLG) Upper Drag Brace, 12540 L
Rev. E4 32−21−104 (one star) Part No. 22511 COMPONENT

RAS−C700−990 32−21−05−102 * Discard the Nose Landing Gear (NLG) Lower Drag Brace, 11520 L
Rev. E4 32−21−104 (one star) Part No. 22516 COMPONENT

5−10−10
PART 2
RAS−C700−990 32−21−05−105 * Discard the Nose Landing Gear (NLG) Drag Brace Apex 11190 L
Rev. E4 32−21−104 (one star) Pin, Part No. 22530 COMPONENT

Dec 11/2013
Page 3
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−21−05−106 * Discard the Nose Landing Gear (NLG) Drag Brace 11220 L
Rev. E4 32−21−104 (one star) Trunnion Pin, Part No. 22534 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−32−01−105 * Discard the Main Landing Gear (MLG) Retraction Actuator 25000 L
Rev. E4 (one star) Assembly, Part No. 21600 COMPONENT

RAS−C700−990 32−32−05−107 * Discard the Main Landing Gear (MLG) Uplock Assembly, 25000 L
Rev. E4 (one star) Part No. 21900 COMPONENT

RAS−C700−990 32−33−01−105 * Discard the Nose Landing Gear (NLG) Retraction Actuator 20000 L
Rev. E4 (one star) Assembly, Part No. 22400−101/−103 COMPONENT

RAS−C700−990 32−33−05−106 * Discard the Nose Landing Gear (NLG) Uplock Assembly, 25000 L
Rev. E4 (one star) Part No. 22600−101/−103 COMPONENT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−10
PART 2
Dec 11/2013
Page 4
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

LIFE LIMITS (SYSTEMS)

1. The systems life limits are taken from the design compliance reports. Discard is mandatory at
the expiry of the specified system life limit for the item.

The life limit items shown are in flight hours (H), landings (L) or calendar years (Years)

EFFECTIVITY: ALL
PART 2 Page 1
5−10−11 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RBR−C700−301 21−71−17−101 * Discard the Humidifier Control Unit, Part No. 2000 H
Rev. W (one star) GG546−2088−3 COMPONENT

EFFECTIVITY: ALL
RBR−C700−301 21−71−21−101 * Discard the Humidifier Level Sensor, Part No. 2000 H
Rev. W (one star) GG436−2100−3 COMPONENT

RBR C700−301 27−31−05−101 * Discard the Pitch Disconnect Mechanism, Part No. 1200 L
Rev. W (one star) GC415−3250−5 COMPONENT

RBR C700−301 27−41−09−104 * Discard the Pitch Trim Actuator, Part No. GT412−4001−3 4000 H
Rev. W (one star) COMPONENT

RBR C700−301 27−41−09−105 * Discard the Pitch Trim Actuator, Part No. GT412−4001−5/7 17000 H
Rev. AU (one star) COMPONENT

RBR−C700−301 30−12−05−101 * Discard the Wing Anti−Icing Telescopic−Duct (LH), Part 2500 H
Rev. AC (one star) No. GG468−4022−3 (S/N 0001, 0002, 0023, 0029, 0044, COMPONENT
0045, 0048 and 0056)

RBR−C700−301 30−12−05−102 * Discard the Wing Anti−Icing Telescopic−Duct (LH), Part 15000 H
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Rev. W (one star) No. GG468−4022−3 (serial numbers not covered by task COMPONENT
30−12−05−101*)

RBR−C700−301 30−12−05−103 * Discard the Wing Anti−Icing Telescopic−Duct (RH), Part 2500 H
Rev. AC (one star) No. GG468−4022−4 (S/N 0001, 0002, 0003, 0031, 0038, COMPONENT
0047, 0049, 0056, 0057, 0058 and 0061)

5−10−11
PART 2
RBR−C700−301 30−12−05−104 * Discard the Wing Anti−Icing Telescopic−Duct (RH), Part 15000 H
Rev. W (one star) No. GG468−4022−4 (serial numbers not covered by task COMPONENT
30−12−05−103*)

Nov 22/2019
Page 2
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RBR−C700−301 30−12−13−101 * Discard the Wing Anti−Icing Flexible−Joints, Part No. 15000 H
Rev. W (one star) GG468−4025−1 COMPONENT

EFFECTIVITY: ALL
RBR−C700−301 32−32−13−101 * Discard the Main−Gear Door Uplock, Part No. 6250 L
Rev. W (one star) GW415−2200−5/6 COMPONENT

RBR−C700−301 32−33−13−101 * Discard the Nose−Gear Forward−Door Uplock, Part No. 2850 L
Rev. W (one star) GW415−2300−1 COMPONENT

RBR−C700−301 32−43−37−101 * Discard the No. 2 Brake Accumulator, Part No. 8366 L
Rev. AR (one star) GW415−1250−1 COMPONENT

RBR−C700−301 32−44−05−101 * Discard the No. 3 Brake Accumulator, Part No. 5816 L
Rev. AR (one star) GW415−1200−1 COMPONENT

RBR−C700−301 34−13−00−101 * Discard the Pitot−Static Probe, Part No. 0856TT1/2/3/4 (for 9600 H
Rev. W (one star) RVSM operators only) COMPONENT

RBR−C700−301 36−11−61−101 * Discard the Uroseal Joints, Part No. 8000 H

Rev. AD (one star) GG468−4054−1/3/7/9/11/15/17/19/21/23/25 COMPONENT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RBR−C700−301 49−14−05−101 * Discard the APU Door Linear Actuator, Part No. 8653M9 5000 H
Rev. W (one star) COMPONENT

5−10−11
PART 2
Aug 17/2020
Page 3
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RBR−C700−301 52−11−41−101 * Discard the Passenger Door Tensator Spring, Part No. 650 L
Rev. AK−1 (one star) GS321−0580−1 COMPONENT
PHASE−IN: For aircraft with passenger door tensator

EFFECTIVITY: ALL
springs with more than 550 Landings COMPONENT, as of
the date of TL/MC Temporary Revision 5−2−44 (Jun
04/2014), this task must be accomplished within 6 Months
from the date of TR 5−2−44 or
1500 Landings COMPONENT, whichever comes first.
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−11
PART 2
Aug 17/2020
Page 4
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

RVSM QUALIFIED AIRCRAFT

1. For all RVSM approved operators, in order to ensure continued airworthiness of aircraft
qualified to operate in Reduced Vertical Separation Minimum (RVSM) airspace, the tasks
shown on page 2 are required at the intervals shown.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−13 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAZ−C700−123 34−11−00−101 * Functional Test of the Air Data Computer, 24 M

Rev. NC−1 7.2.1 (one star) Post SB 700−34−014, RVSM Qualified A/C
NOTE: This task has been absorbed by a CMR (see

EFFECTIVITY: ALL
section 5−10−40).

RAZ−C700−123 34−13−00−101 * Discard Task of the Pitot−Static Probes, 9600 H

Rev. NC−1 7.2.1 (one star) (Post SB 700−34−014, RVSM Qualified A/C) COMPONENT
NOTE: This task has been absorbed by a System Life Limit
(see Section 5−10−11).
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−13
PART 2
Dec 11/2013
Page 2
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−19

TIME LIMITS BY AIRCRAFT EFFECTIVITY

EFFECTIVITY: ALL
PART 2 Cover
5−10−19 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

TIME LIMITS BY AIRCRAFT EFFECTIVITY

1. Introduction

Section 5−10−19 tabulates the revised life limits of repaired or modified components by
individual aircraft effectivity. Thus, the life limits published in section 5−10−19, applicable to
repaired and modified components only, supersede the baseline life limits given in section
5−10−10.

Operators receive only those pages applicable to their aircraft, consequently section 5−10−19
is not available on microfiche or CD−ROM and is not published in the Maintenance Planning
Document.

The operator must control record keeping of the repaired or modified components and their
removal from service at the revised life limit published in section 5−10−19.

2. Organization

Section 5−10−19 is arranged as follows:

− Introduction
− List of Effective Pages (if applicable)
− Individualized life limits as shown on the aircraft specific list of effective pages.

The list of effective pages will be revised with each new or revised repair.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−19 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

TIME LIMITS − SUPPLEMENTARY LIMITATIONS

1. This section lists supplementary maintenance limitations. The following mandatory checks
and inspections are required at the intervals shown in order to ensure continued airworthiness
of the aircraft.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−20 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RBR C700−301 27−41−09−106 * Restoration of the Pitch Trim Actuator (Gear Housing 3750 H
Rev. W (one star) Replacement), Part No. GT412−4001−3 or GT412−4001−5 COMPONENT

EFFECTIVITY: ALL
RBR−C700−301 32−33−01−111 * Restoration of the Nose Landing Gear (NLG) Shock−Strut 1500 L
Rev. AR (one star) Assembly to Retraction−Actuator Main−Fitting Joint (Post COMPONENT
SB 700−32−035 PART C)
NOTE: This restoration task is for:
− Inspection of Part No. 1286−0116
− Inspection of Part No. 1286−0117
− Discard of Part No. 1285−0041
− Discard of Part No. 22193−1 or 1285−0046
− Discard of Part No. 22195−1 or 1285−0048
− Discard of Part No. 22194−1 or 1285−0047
− Discard of Part No. 22407−1
NOTE: Time tracking of the above non−serialized parts is
to be done at the NLG assembly level (Part No.
GW311−1100−XX).
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RBR−C700−301 52−11−25−101 * Restoration of the Passenger Door Actuator Motor, Part 850 L
Rev. AH (one star) No. GS321−0591−9 (Gearhead, Part No. 2H4A321809A) COMPONENT

5−10−20
PART 2
Page 2
May 03/2018
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−25

TASKS BY AIRCRAFT EFFECTIVITY − CUSTOM

INSTALLATIONS

EFFECTIVITY: ALL
PART 2 Cover
5−10−25 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

TASKS BY AIRCRAFT EFFECTIVITY − CUSTOM INSTALLATIONS

1. Introduction

Section 5−10−25 is customized to the requirements of individual aircraft, where applicable. It

contains Airworthiness Limitation checks by aircraft effectivity, to impose additional
maintenance requirements as a result of structural modifications or installations carried out on
those aircraft.

These tasks must be controlled by the operator.

NOTE: Operators receive only those pages applicable to their aircraft. This section is not
available on microfiche or CD−ROM.

2. Organization

Section 5−10−25 is arranged as follows:

− Introduction
− List of Effective Pages (if applicable)
− Individualized inspection tasks as shown on the aircraft specific list of effective pages.

The list of effective pages will be revised with each new or revised task.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−25 May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−26

TASKS BY AIRCRAFT EFFECTIVITY − REPAIRS

EFFECTIVITY: ALL
PART 2 Cover
5−10−26 Dec 11/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

TASKS BY AIRCRAFT EFFECTIVITY − REPAIRS

1. Introduction

Section 5−10−26 is customized to the requirements of individual aircraft, where applicable. It

contains Airworthiness Limitation checks by aircraft effectivity, to impose additional
maintenance requirements as a result of structural repairs carried out on those aircraft.

New repairs will be released showing interim approval of the Repair Engineering Order
(REO). Each interim approval will then be superseded by a final approval showing threshold
and repeat inspection intervals in the usual manner, and identifying the applicable inspection
procedure(s).

These tasks must be controlled by the operator.

NOTE: Operators receive only those pages applicable to their aircraft. This section is not
available on microfiche or CD−ROM.

2. Organization

Section 5−10−26 is arranged as follows:

− Introduction
− List of Effective Pages (if applicable)
− Individualized life limits as shown on the aircraft specific list of effective pages.

The list of effective pages will be revised with each new or revised task.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−26 May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−30

AIRWORTHINESS LIMITATION ITEMS

Tasks by Chapter 5 Task Number

EFFECTIVITY: ALL
PART 2 Cover
5−10−30 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 27−41−09−101 * Special Detailed Inspection of the Horizontal Stabilizer Trim T 7500 L
Rev. F 27−41−101A (one star) Actuator (Excluding Aircraft Attachment Pins) COMPONENT
R 2338 L
COMPONENT

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Nov 13/2017
Page 1
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−22−00−101 * Special Detailed Inspection of the Nose Gear Forward

Rev. F−1 32−22−101A (one star) Doors

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Sep 06/2016
Page 2
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 52−11−00−101 * Detailed Inspection of the Outer Skin of the Passenger

Rev. E 52−11−103A (one star) Door

93500 lbs MTOW Pre SB 700−21−034 T 8196 L

EFFECTIVITY: ALL
R 3987 L

96000 lbs MTOW Pre SB 700−21−034 T 7993 L

R 3778 L

98000 lbs MTOW and any aircraft Post T 5255 L

SB 700−21−034 R 2593 L

RAS−C700−990 52−11−00−102 * Special Detailed Inspection of the Passenger Door

Rev. F−1 52−11−105B (one star) Mounting Side Frames

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Sep 06/2016
Page 3
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 52−11−00−103 * Detailed Inspection of the Passenger Door Mounting

Rev. F−1 52−11−105A (one star) Side−Frames, Stops, Skin and Stiffeners − Internal
52−11−107A
52−11−111A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 52−21−00−104 * Detailed Inspection of the Over−Wing Emergency Exit Door

Rev. G1 52−21−101A (one star)
52−21−101B
52−21−101C

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8265 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8265 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 6500 L

Page 4
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 52−30−00−101 * Detailed Inspection of the Baggage Door

Rev. G 52−31−101A (one star)
52−31−102A
52−31−103B

EFFECTIVITY: ALL
52−31−104A

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7700 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7700 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5500 L

A/C 9096 T 8500 L

R 5500 L

RAS−C700−990 52−30−00−105 * Special Detailed Inspection of the Baggage Door Skin

Rev. F−1 52−31−105A (one star) Between Door Upper Skin Edge and Vent Door

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 2767 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2760 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2767 L

5−10−30
PART 2
A/C 9096 T 8500 L
R 2767 L

Page 5
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 52−30−00−106 * Detailed Inspection of the Vent Door of the Baggage Door
Rev. F−1 52−31−106A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 5667 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5667 L

A/C 9096 T 8500 L

R 5667 L

RAS−C700−990 52−30−00−107 * Special Detailed Inspection of the Baggage Door

Rev. F−1 52−31−103A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 6
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−101 * Detailed Inspection of the Nose Wheel Well and Frame,
Rev. F−1 53−10−101A (one star) FS251.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 4585 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4502 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4585 L

A/C 9096 T 8500 L

R 4585 L

RAS−C700−990 53−10−00−102 * Detailed Inspection of the Landing Gear Box

Rev. F−1 53−10−102A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 9872 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 7
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−103 * Detailed Inspection of the Floor Attachment to the

Rev. F−1 53−10−104A (one star) Bulkhead, FS202.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−10−00−104 * Detailed Inspection of the Bulkhead, FS202.00

Rev. F−1 53−10−106A (one star)
53−10−106B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 4974 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4974 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

A/C 9096 T 8500 L

R 4974 L

5−10−30
PART 2
Page 8
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−105 * General Visual Inspection of the Frame, FS251.00

Rev. F−1 53−10−108A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5470 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5454 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5470 L

A/C 9096 T 8500 L

R 5470 L

RAS−C700−990 53−10−00−106 * Special Detailed Inspection of the Frame, FS280.00 −

Rev. G1 53−10−109B (one star) External

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 9
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−107 * Detailed Inspection of the Frame, FS280.00 − Internal

Rev. F−1 53−10−110A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 3568 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3568 L

A/C 9096 T 8500 L

R 3568 L

RAS−C700−990 53−10−00−108 * Special Detailed Inspection of the Splice at Stringers 16A

Rev. F−1 53−10−111A (one star) and 23

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 10
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−109 * Detailed Inspection of the Sheet Metal Frame, FS210.00,

Rev. F−1 53−10−112A (one star) FS220.00, FS235.00, FS265.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6894 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 6894 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−10−00−110 * Detailed Inspection of the Stringers 16A and 23, from
Rev. G 53−10−113A (one star) FS202.00 to FS280.00
53−10−114A

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 11
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−112 * Special Detailed Inspection of the Cockpit Window

Rev. G 53−10−121B (one star) Surround Structure
53−10−121D

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 7485 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8462 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−10−00−114 * Detailed Inspection of the Cockpit Skin Panels

Rev. F−1 53−10−111B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 12
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−115 * Special Detailed Inspection of the Cockpit Window Center

Rev. G 53−10−121A (one star) Post

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−10−00−116 * Special Detailed Inspection of the Cockpit Window Lower

Rev. E 53−10−121C (one star) Sill at the Center Post Attachment near BL0

93500 lbs MTOW Pre SB 700−21−034 T 6620 L

96000 lbs MTOW Pre SB 700−21−034 R 633 L
98000 lbs MTOW and any aircraft Post
SB 700−21−034
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 13
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−124 * Detailed Inspection of the Access Panel Surround Structure

Rev. G 53−10−122A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 8197 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8197 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−10−00−125 * Detailed Inspection of the Skin Splice, FS280.00 − External

Rev. G1 53−10−109A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6209 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6209 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 6209 L

A/C 9096 T 8500 L

R 6209 L

5−10−30
PART 2
Page 14
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−126 * Detailed Inspection of the Cockpit Window Surround

Rev. G2 53−10−121E (one star) Structure, Gusset and Side Plates

93500 lbs MTOW Pre SB 700−21−034 T 8166 L

EFFECTIVITY: ALL
R 5574 L

96000 lbs MTOW Pre SB 700−21−034 T 6639 L

R 4530 L

98000 lbs MTOW and any aircraft Post T 6639 L

SB 700−21−034 R 4530 L

A/C 9096 T 6639 L

R 4530 L

RAS−C700−990 53−20−00−101 * Detailed Inspection of the Fuselage Upper Skin and

Rev. G 53−21−101A (one star) Longitudinal Joints from, FS381.00 to FS557.00 − External
53−21−103A
53−21−105A
53−21−117A
53−21−139A
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1681 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2002 L

98000 lbs MTOW and any aircraft Post T 7500 L

5−10−30
PART 2
SB 700−21−034 R 605 L

A/C 9096 T 8500 L

R 605 L

Page 15
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−104 * Special Detailed Inspection of the Fuselage Keel Beam

Rev. E 53−21−107A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 7240 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 1399 L

98000 lbs MTOW and any aircraft Post T 6082 L

SB 700−21−034 R 1243 L

RAS−C700−990 53−20−00−105 * Special Detailed Inspection of the Over−Wing Longeron,

Rev. F−1 53−21−109A (one star) FS525.00 to FS574.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 10933 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5711 L

A/C 9096 T 8500 L

R 5711 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 16
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−106 * Special Detailed Inspection of the Pressure Floor and the
Rev. F−1 53−21−111A (one star) Stiffeners of the Pressure Bulkhead from FS557.00 to
53−21−113A FS574.50

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 4470 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3768 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1250 L

A/C 9096 T 8500 L

R 1250 L

RAS−C700−990 53−20−00−109 * Special Detailed Inspection of the Skin and Fuselage Joints
Rev. G 53−21−117B (one star) from, FS281.00 to FS557.00 − External

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1430 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 493 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 493 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 493 L

Page 17
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−110 * Detailed Inspection of the Fuselage Skin from, FS281.00 to

Rev. F−1 53−21−119A (one star) FS381.00 − External
53−21−121A
53−21−123A

EFFECTIVITY: ALL
53−21−125A
53−21−127A
53−21−139A
53−21−139B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1233 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1229 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 461 L

A/C 9096 T 8500 L

R 461 L

RAS−C700−990 53−20−00−117 * Detailed Inspection of the Passenger Door Cutout Structure

BD−700 TIME LIMITS/MAINTENANCE CHECKS

Rev. E 53−21−133A (one star) and Fittings

53−21−133B

93500 lbs MTOW Pre SB 700−21−034 T 5848 L

R 1963 L

96000 lbs MTOW Pre SB 700−21−034 T 5737 L

5−10−30
PART 2
R 1963 L

98000 lbs MTOW and any aircraft Post T 5848 L

SB 700−21−034 R 1963 L

Page 18
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−118 * Special Detailed Inspection of the Fuselage Barrel Joint,

Rev. F−1 53−21−135A (one star) FS381.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−20−00−119 * Special Detailed Inspection of the Internal Structure of the

Rev. F−1 53−21−136A (one star) Fuselage Barrel Joints, FS381.00 and FS557.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 19
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−120 * Special Detailed Inspection of the Fuselage Barrel Joint,

Rev. F−1 53−21−137A (one star) FS557.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−20−00−122 * Detailed Inspection of the Machined Fittings and Skin

Rev. F−1 53−21−141A (one star) Around the Service Door, FS295.00 to FS310.00 and
Stringers 22R and 24R

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 8021 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 20
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−123 * Detailed Inspection of the Avionics Bay Door and

Rev. F−1 53−21−143A (one star) Surrounding Skin

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 11393 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 10530 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−20−00−124 * Detailed Inspection of the Wing Inspection Light Installation

Rev. F−1 53−21−145A (one star)
53−21−145B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 21
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−125 * Detailed Inspection of the Stringers and Frames from,

Rev. F−1 53−21−101B (one star) FS381.00 to FS557.00
53−21−103B
53−21−105B

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 2133 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 605 L

A/C 9096 T 8500 L

R 605 L

RAS−C700−990 53−20−00−126 * Detailed Inspection of the Fuselage Stringers and Frames

Rev. F−1 53−21−119B (one star) from, FS281.00 to FS381.00
53−21−121B
53−21−123B
53−21−125B
53−21−127B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1233 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1229 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 461 L

5−10−30
PART 2
A/C 9096 T 8500 L
R 461 L

Page 22
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−127 * General Visual Inspection of the Pressure Bulkhead

Rev. F−1 53−21−111B (one star) FS557.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−102 * Special Detailed Inspection of the Panel Joint, FS557.00 to

Rev. F−1 53−31−102A (one star) FS781.00, Stringer 6

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8914 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5355 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 4730 L

A/C 9096 T 8500 L

R 4730 L

5−10−30
PART 2
Page 23
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−103 * Detailed Inspection of the Panel Joint, FS557.00 and

Rev. G 53−31−103A (one star) FS797.00, Stringers 18L to 18R

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 8511 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8511 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−104 * Detailed Inspection of the Fuselage Skin at the Cabin

Rev. F−1 53−31−104A (one star) Window Cutouts, FS557.00 to FS797.00
53−31−104B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1855 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1175 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1855 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 1855 L

Page 24
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−105 * Special Detailed Inspection of the Front Spar Frame Outer
Rev. G 53−31−105A (one star) Flange, FS574.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2450 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2450 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2450 L

A/C 9096 T 8500 L

R 2303 L

RAS−C700−990 53−30−00−106 * Special Detailed Inspection of the Rear Spar Frame,

Rev. G 53−31−106A (one star) FS719.30

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2597 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 2597 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2597 L

A/C 9096 T 8500 L

R 2597 L

5−10−30
PART 2
Page 25
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−107 * Detailed Inspection of the Intermediate Frames

Rev. F−1 53−31−107A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 9022 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8503 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−110 * Special Detailed Inspection of the Fuselage Skin and Splice
Rev. G 53−31−110B (one star) Strap at Stringer 18
53−31−110C

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7932 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7932 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 6500 L

Page 26
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−111 * Detailed Inspection of the Pressure Floor Panels and

Rev. F−1 53−31−111A (one star) Beams from FS719.30 to FS781.00
53−31−112A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4631 L

A/C 9096 T 8500 L

R 4631 L

RAS−C700−990 53−30−00−113 * Detailed Inspection of the Keel Beam, FS719.30 to

Rev. F−1 53−31−113A (one star) FS781.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2702 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

A/C 9096 T 8500 L

R 2702 L

5−10−30
PART 2
Page 27
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−114 * Special Detailed Inspection of the Rear Spar Bulkhead,

Rev. F−1 53−31−114A (one star) FS719.30

93500 lbs MTOW Pre SB 700−21−034 T 8964 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 8113 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2880 L

A/C 9096 T 8500 L

R 2880 L

RAS−C700−990 53−30−00−115 * Detailed Inspection of the Frame, FS781.00

Rev. G 53−31−115A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 6654 L

R 1997 L

96000 lbs MTOW Pre SB 700−21−034 T 6654 L

R 1997 L

98000 lbs MTOW and any aircraft Post T 6654 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 1997 L

5−10−30
PART 2
Page 28
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−116 * Detailed Inspection of the Rear Spar Frame, FS719.30

Rev. G 53−31−106B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5126 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5126 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5126 L

A/C 9096 T 8500 L

R 5126 L

RAS−C700−990 53−30−00−118 * Special Detailed Inspection of the Pressure Floor Panels

Rev. F−1 53−31−111B (one star) from FS719.30 to FS781.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 29
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−119 * Special Detailed Inspection of Stringer 6 from FS574.00 to

Rev. F−1 53−31−102B (one star) FS781.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5054 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3303 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5054 L

A/C 9096 T 8500 L

R 5054 L

RAS−C700−990 53−30−00−120 * Special Detailed Inspection of the Front Spar Frame

Rev. G 53−31−105B (one star) Outboard and Inboard Flanges, FS574.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1714 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1714 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1714 L

A/C 9096 T 8500 L

R 1703 L

5−10−30
PART 2
Page 30
May 19/2021
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−121 * Special Detailed Inspection of the Front Spar Frame

Rev. G 53−31−105C (one star) Attachment to the Center Wing Box, FS574.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2450 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2450 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2450 L

A/C 9096 T 8500 L

R 2450 L

RAS−C700−990 53−30−00−122 * Special Detailed Inspection of the Rear Spar Frame

Rev. G 53−31−106C (one star) Attachment to the Center Wing Box, FS719.30

93500 lbs MTOW Pre SB 700−21−034 T 10125 L

R 1570 L

96000 lbs MTOW Pre SB 700−21−034 T 10125 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1570 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1570 L

A/C 9096 T 8500 L

R 1570 L

5−10−30
PART 2
Page 31
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−123 * Special Detailed Inspection of the Frame Splice, Stringers 5

Rev. G 53−31−109B (one star) and 15, FS574.50 and FS719.30

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 8428 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8428 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−131 * Special Detailed Inspection of the Emergency Door Cutout

Rev. G1 53−31−108A (one star) and Latch Fitting

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1230 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 782 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1095 L

A/C 9096 T 8500 L

R 1095 L

5−10−30
PART 2
Page 32
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−132 * Special Detailed Inspection of the Fuselage Skin and Splice
Rev. G1 53−31−110A (one star) Strap at Stringer 18

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 7932 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7932 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−133 * Special Detailed Inspection of the Fuselage Skin Splices at

Rev. G 53−31−103B (one star) FS737.00 from STR15 to STR19 and at STR15 Between
FS737.00 and FS787.70

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 11382 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 11382 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 6500 L

Page 33
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−134 * Special Detailed Inspection of the Rear Spar Frame

Rev. G 53−31−106D (one star) Outer−Cap, FS719.30 at BL47.61

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−135 * Detailed Inspection of the Fuselage Skin Panel and

Rev. G 53−31−110D (one star) Stringer 18 − Internal

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 34
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−136 * Special Detailed Inspection of the Frame, FS781.00

Rev. G 53−31−115B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 7905 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7905 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−30−00−137 * Detailed Inspection of the Center Fuselage Skin

Rev. G1 53−31−101A (one star) Panel−Assembly from FS557.00 to FS797.60

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 35
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−138 * Detailed Inspection of the Frame Splice, FS574.00 to

Rev. G1 53−31−109A (one star) FS781.00, STR5 and STR15

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 11630 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 11630 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−101 * Detailed Inspection of the Fuselage Skin from FS781.00 to

Rev. F−1 53−41−101A (one star) FS861.00 − External
53−41−109A
53−41−110A

93500 lbs MTOW Pre SB 700−21−034 T 10267 L

R 1895 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 7918 L

R 1156 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1895 L

5−10−30
PART 2
A/C 9096 T 8500 L
R 1895 L

Page 36
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−102 * Special Detailed Inspection of the Rear Fuselage Skin

Rev. G 53−41−102A (one star) Longitudinal Joints

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 3554 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3222 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3222 L

A/C 9096 T 8500 L

R 3222 L

RAS−C700−990 53−40−00−103 * Detailed Inspection of the Baggage Door Surround

Rev. E 53−41−103A (one star) Structure and Pressure Bulkhead
53−41−108A

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2330 L

5−10−30
PART 2
Page 37
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−104 * Detailed Inspection of the Frames at FS925.00 and

Rev. F−1 53−41−105A (one star) FS987.00 and the Rear Fuselage Longeron Platform
53−41−119A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 3540 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2588 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3540 L

A/C 9096 T 8500 L

R 3540 L

RAS−C700−990 53−40−00−105 * Detailed Inspection of the Forward Face of the Pressure

Rev. F−1 53−41−106A (one star) Bulkhead at FS861.00, and the Floor Beams FS789.00 to
53−41−113A FS861.00
53−41−113B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6215 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5515 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5506 L

5−10−30
PART 2
A/C 9096 T 8500 L
R 5506 L

Page 38
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−106 * General Visual Inspection of the Fuselage Skin from

Rev. G1 53−41−107A (one star) FS861.00 to Rear Spar Frame − External

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 8700 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6028 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−108 * Detailed Inspection of the Baggage Door Surround

Rev. F−1 53−41−109B (one star) Structure, Lower Sill

93500 lbs MTOW Pre SB 700−21−034 T 12185 L

96000 lbs MTOW Pre SB 700−21−034 R 3825 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 3480 L

A/C 9096 T 8500 L

R 3480 L

5−10−30
PART 2
Page 39
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−109 * Detailed Inspection of the Baggage Door Surround

Rev. F−1 53−41−110B (one star) Structure, Frame and Reinforcing Strap

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 1895 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1890 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1895 L

A/C 9096 T 8500 L

R 1895 L

RAS−C700−990 53−40−00−110 * Detailed Inspection of the Rear−Pressure Bulkhead

Rev. F−1 53−41−111A (one star) Upper−Horizontal−Beam

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4600 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 4458 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4600 L

A/C 9096 T 8500 L

R 4600 L

5−10−30
PART 2
Page 40
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−111 * Detailed Inspection of the Pressure Bulkhead at FS861.00

Rev. F−1 53−41−112A (one star) Vertical Stiffeners and Baggage Door Sill Fitting
53−41−117A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 8905 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7892 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−113 * Special Detailed Inspection of the Floor Structure, Seat Rail
Rev. F−1 53−41−114A (one star) and Lateral Floor Beam Joints

93500 lbs MTOW Pre SB 700−21−034 T 8100 L

96000 lbs MTOW Pre SB 700−21−034 R 2911 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2784 L

A/C 9096 T 8500 L

R 2784 L

5−10−30
PART 2
Page 41
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−114 * Special Detailed Inspection of the Baggage Door Surround

Rev. F−1 53−41−115A (one star) Structure Upper Sill Joint at FS813.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 5330 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5330 L

A/C 9096 T 8500 L

R 5330 L

RAS−C700−990 53−40−00−115 * Special Detailed Inspection of the Baggage Door Surround

Rev. F−1 53−41−116A (one star) Structure Upper Sill Joint, Forward of FS861.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12000 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6349 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 42
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−117 * General Visual Inspection of the Rear Fuselage Keel Beam
Rev. F−1 53−41−118A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−119 * Detailed Inspection of the Rear−Fuselage Skin

Rev. F−1 53−41−120A (one star) Engine−Mount−Cutouts

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8465 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 43
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−120 * Special Detailed Inspection of the Inner Flap Track

Rev. F−1 53−41−121A (one star) Support−Fittings on the Rear Fuselage

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−121 * Detailed Inspection of the Fuselage Frame at the Vertical

Rev. F−1 53−41−122A (one star) Stabilizer Front−Spar

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2327 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1949 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 2327 L

A/C 9096 T 8500 L

R 2327 L

5−10−30
PART 2
Page 44
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−122 * Detailed Inspection of the Fuselage Frame at the Vertical

Rev. F−1 53−41−123A (one star) Stabilizer Mid−Spar

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5067 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4624 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5067 L

A/C 9096 T 8500 L

R 5067 L

RAS−C700−990 53−40−00−123 * Detailed Inspection of the Fuselage Frame at the Vertical

Rev. F−1 53−41−124A (one star) Stabilizer Rear−Spar

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3700 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 3264 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3700 L

A/C 9096 T 8500 L

R 3700 L

5−10−30
PART 2
Page 45
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−124 * Special Detailed Inspection of the Fuselage Support

Rev. F−1 53−41−105B (one star) Frames for the Engine Beams, Inner Flange

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 11667 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6789 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−40−00−125 * Special Detailed Inspection of the Fuselage Frame at the

Rev. F−1 53−41−122B (one star) Vertical Stabilizer Front Spar, Inboard Flange

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4667 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 3530 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4667 L

A/C 9096 T 8500 L

R 4667 L

5−10−30
PART 2
Page 46
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−126 * Detailed Inspection of the Floor Structure, Seat Rail and
Rev. F−1 53−41−114B (one star) Lateral Floor Beams

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2644 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2465 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2187 L

A/C 9096 T 8500 L

R 2187 L

RAS−C700−990 53−40−00−127 * Special Detailed Inspection of the Rear Fuselage Skin

Rev. G 53−41−102B (one star) Circumferential Joints

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8231 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7076 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7076 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 47
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−128 * Detailed Inspection of the Fuselage Skin Around the

Rev. E 53−41−103B (one star) Baggage Door

93500 lbs MTOW Pre SB 700−21−034 T 7450 L

EFFECTIVITY: ALL
R 1300 L

96000 lbs MTOW Pre SB 700−21−034 T 6603 L

R 1152 L

98000 lbs MTOW and any aircraft Post T 7450 L

SB 700−21−034 R 1300 L

RAS−C700−990 53−40−00−137 * Special Detailed Inspection of the Rear Pressure Bulkhead

Rev. G 53−41−106B (one star) at FS861.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6215 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5515 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 5910 L

A/C 9096 T 8500 L

R 5910 L

5−10−30
PART 2
Page 48
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−138 * Special Detailed Inspection of the Baggage Door Surround

Rev. G 53−41−108B (one star) Structure − Pressure Bulkhead

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2330 L

A/C 9096 T 8500 L

R 2330 L

RAS−C700−990 53−40−00−139 * Special Detailed Inspection of the Rear Fuselage Skin

Rev. G 53−41−125B (one star) Cutouts from FS781.00 to FS1066.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 9030 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7880 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 49
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−140 * Detailed Inspection of the Rear Fuselage Skin Cutouts from
Rev. G1 53−41−125A (one star) FS781.00 to FS1066.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 9030 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7880 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 53−50−00−101 * Detailed Inspection of the Vertical Stabilizer Front−Spar

Rev. F−1 53−51−101A (one star) Cap and Cruciform Fitting
55−31−101A

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3540 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2586 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3540 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 3540 L

Page 50
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−50−00−102 * Detailed Inspection of the Vertical Stabilizer Attachment at

Rev. F−1 53−51−102A (one star) the Fuselage Frames
53−51−103A
53−51−104A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 3540 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2586 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3540 L

A/C 9096 T 8500 L

R 3540 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 51
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 54−51−00−101 * Special Detailed Inspection of the Engine Beam

Rev. F−1 54−51−101A (one star) Attachment−Lugs

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 54−51−00−102 * Special Detailed Inspection of the Engine Beam Pylon,

Rev. F−1 54−51−102A (one star) Upper and Lower Caps

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2757 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1528 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 2757 L

A/C 9096 T 8500 L

R 2757 L

5−10−30
PART 2
Page 52
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 54−51−00−103 * Special Detailed Inspection of the Engine Beam

Rev. F−1 54−51−103A (one star) Thrust−Strut

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 3333 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3284 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3333 L

A/C 9096 T 8500 L

R 3333 L

RAS−C700−990 54−51−00−106 * Special Detailed Inspection of the Engine Beam Pylon,

Rev. F−1 54−51−102B (one star) Fuselage Joint

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7237 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 5026 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7237 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 53
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 54−51−00−107 * Detailed Inspection of the Engine Pylon Skins and Drag
Rev. G2 54−51−104A (one star) Angles
54−51−105A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 54
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−00−101 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−101A (one star) Tailplane−Actuator Fitting−Lugs Including Pins

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 4982 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4982 L

A/C 9096 T 8500 L

R 4982 L

RAS−C700−990 55−10−00−102 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−102A (one star) Pivot Fittings
55−11−102B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 4842 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4842 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

A/C 9096 T 8500 L

R 4842 L

5−10−30
PART 2
Page 55
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−00−103 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−105A (one star) Tailplane Hinge−Fitting Lugs and Pins

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−10−00−104 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−106A (one star) Rear Spar Joint

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 6454 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 6454 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6454 L

RAS−C700−990 55−10−00−105 * Detailed Inspection of the Internal Skin and Structure of the T 7500 L
Rev. E 55−11−107A (one star) Horizontal−Stabilizer R 7500 L
55−11−109A
55−11−110A

5−10−30
PART 2
Page 56
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−00−108 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. G 55−11−111A (one star) PCU Fittings

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 10536 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−10−00−109 * Detailed Inspection of the Horizontal−Stabilizer Tailplane

Rev. F−1 55−11−105B (one star) Hinge−Fittings

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 57
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−00−110 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−106B (one star) Front Spar Joint

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6454 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 6454 L

A/C 9096 T 8500 L

R 6454 L

RAS−C700−990 55−10−09−101 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−103A (one star) Pivot−Fitting Support−Structure Baseplate

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 58
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−09−102 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−104A (one star) Tailplane Center−Line Joint−Straps

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 11042 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−10−09−103 * Detailed Inspection of the Attachment of the Actuator Fitting

Rev. F−1 55−11−108A (one star) to the Horizontal−Stabilizer

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 59
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−10−09−104 * Detailed Inspection of the Horizontal−Stabilizer

Rev. F−1 55−11−103B (one star) Pivot−Fitting Support−Structure

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−10−09−105 * Special Detailed Inspection of the Attachment of the

Rev. F−1 55−11−108B (one star) Actuator Fitting to the Horizontal−Stabilizer Yaw Restraint

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 11218 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 60
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−20−00−101 * Special Detailed Inspection of the Elevator, Actuator and

Rev. F−1 55−21−101A (one star) Hinge Fitting

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−20−00−102 * Detailed Inspection of the Elevator − Composite Parts T 7500 L

Rev. E 55−21−102A (one star) R 7500 L

RAS−C700−990 55−30−00−102 * General Visual Inspection of the Vertical Stabilizer

Rev. F−1 55−31−104A (one star) Skin/Stringer Panels

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7505 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7308 L

98000 MTOW and any aircraft Post SB T 7500 L

700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 61
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−103 * Special Detailed Inspection of the Surround Structure of the

Rev. F−1 55−31−105A (one star) Access Hole on the Vertical Stabilizer

93500 lbs MTOW Pre SB 700−21−034 T 11750 L

EFFECTIVITY: ALL
R 3333 L

96000 lbs MTOW Pre SB 700−21−034 T 11725 L

R 3326 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3333 L

A/C 9096 T 8500 L

R 3333 L

RAS−C700−990 55−30−00−104 * Special Detailed Inspection of the Vertical Stabilizer Pivot

Rev. F−1 55−31−106A (one star) and Actuator Fittings for the Horizontal Stabilizer
55−31−106B
55−31−108A
55−31−113A
55−31−114A
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 6500 L

Page 62
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−105 * Detailed Inspection of the Backup Structure of the

Rev. F−1 55−31−108B (one star) Horizontal−Stabilizer Actuator Attachment to the Vertical
Stabilizer

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−30−00−106 * Detailed Inspection of the Vertical Stabilizer Front−Spar

Rev. F−1 55−31−110A (one star) Strap

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5600 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5394 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5600 L

A/C 9096 T 8500 L

R 5600 L

5−10−30
PART 2
Page 63
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−107 * Special Detailed Inspection of the Vertical Stabilizer Rudder

Rev. F−1 55−31−111A (one star) Hinge Fittings and Pins
55−31−112A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 9767 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−30−00−111 * Special Detailed Inspection of the Horizontal−Stabilizer

Rev. G 55−31−115A (one star) Trim−Actuator Pin
NOTE: Replacement of pin and all associated hardware
(e.g.; nut, washers, and cotter pin) restarts the inspection
threshold.

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 10667 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 64
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−112 * General Visual Inspection of the Vertical Stabilizer Drag

Rev. G 55−31−116A (one star) Angles

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 7500 L

R 7500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−30−00−113 * Special Detailed Inspection of the Vertical Stabilizer

Rev. F−1 55−31−118A (one star) Side−Stays

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 65
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−114 * Detailed Inspection of the Vertical Stabilizer Closing Rib

Rev. F−1 55−31−119A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 2000 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2000 L

A/C 9096 T 8500 L

R 2000 L

RAS−C700−990 55−30−00−115 * Special Detailed Inspection of the Rudder Wishbone

Rev. F−1 55−31−117A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 66
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−116 * Detailed Inspection of the Rudder Wishbone

Rev. F−1 55−31−117B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−30−00−117 * Detailed Inspection of the Vertical Stabilizer Skin/Stringer

Rev. G 55−31−104B (one star) Panels

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7505 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7308 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 67
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−00−118 * Special Detailed Inspection of the Vertical Stabilizer Drag

Rev. G 55−31−116B (one star) Angles

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 7500 L

R 7500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 55−30−01−101 * General Visual Inspection of the Caps of the Rear Spar of
Rev. F−1 55−31−103A (one star) the Vertical Stabilizer

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 68
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−30−01−102 * Detailed Inspection of the Vertical Stabilizer Mid−Spar Cap

Rev. F−1 55−31−109A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 3540 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2587 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3540 L

A/C 9096 T 8500 L

R 3540 L

RAS−C700−990 55−40−00−101 * Special Detailed Inspection of the Rudder Actuator Bracket

Rev. F−1 55−41−101A (one star) Lugs

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 1444 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 1444 L

A/C 9096 T 8500 L

R 1444 L

RAS−C700−990 55−40−00−102 * Detailed Inspection of the Rudder Structure − Composite T 7500 L

Rev. D 55−41−102A (one star) Parts R 7500 L

5−10−30
PART 2
Page 69
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 55−40−00−103 * Special Detailed Inspection of the Rudder Hinge Fittings

Rev. F−1 55−41−101B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 9767 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 70
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−101 * Special Detailed Inspection of the Center−Wing

Rev. F−1 57−11−101A (one star) Lower−Panel Access−Holes

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 6173 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5523 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5820 L

A/C 9096 T 8500 L

R 5820 L

RAS−C700−990 57−10−00−102 * Detailed Inspection of the AC Transfer−Pump Lower Panel

Rev. F−1 57−11−102A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 71
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−103 * Special Detailed Inspection of the Main Landing Gear

Rev. F−1 57−11−103A (one star) (MLG) Side−Stay Fitting

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 1353 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1353 L

A/C 9096 T 8500 L

R 1353 L

RAS−C700−990 57−10−00−104 * Special Detailed Inspection of the Center Wing Lower

Rev. G 57−11−104A (one star) Panel Splice, BL47.61

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7847 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7847 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 72
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−106 * Detailed Inspection of the Front Spar Root−Splice

Rev. F−1 57−11−106A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 3670 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3670 L

A/C 9096 T 8500 L

R 3670 L

RAS−C700−990 57−10−00−107 * Detailed Inspection of the Rear Spar Splice of the Center
Rev. G 57−11−107A (one star) Wing

93500 lbs MTOW Pre SB 700−21−034 T 9014 L

R 1412 L

96000 lbs MTOW Pre SB 700−21−034 T 9014 L

R 1412 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 1412 L

A/C 9096 T 8500 L

R 1412 L

5−10−30
PART 2
Page 73
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−108 * Detailed Inspection of the Center−Wing Upper Panel

Rev. G 57−11−109A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 1796 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1796 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1796 L

A/C 9096 T 8500 L

R 1796 L

RAS−C700−990 57−10−00−109 * Detailed Inspection of the Keel Beam Rib, BL4.75

Rev. G 57−11−110A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2722 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 2722 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2722 L

A/C 9096 T 8500 L

R 2722 L

5−10−30
PART 2
Page 74
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−110 * Special Detailed Inspection of the Intermediate Rib,

Rev. E 57−11−111A (one star) BL27.00 Truss Support Plate

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 7047 L

96000 lbs MTOW Pre SB 700−21−034 T 9748 L

R 5414 L

98000 lbs MTOW and any aircraft Post T 7400 L

SB 700−21−034 R 1920 L

RAS−C700−990 57−10−00−111 * Special Detailed Inspection of the Lower−Cap of the

Rev. G 57−11−112A (one star) Center−Wing Front Spar

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1751 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1751 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 1751 L

A/C 9096 T 8500 L

R 1751 L

5−10−30
PART 2
Page 75
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−112 * Detailed Inspection of the Lower Cap of the Center−Wing

Rev. G 57−11−113A (one star) Rear Spar

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 5975 L

RAS−C700−990 57−10−00−113 * Detailed Inspection of the Intermediate Rib, BL27.00 Chord

Rev. F−1 57−11−111B (one star) Flanges

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2226 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1714 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2020 L

A/C 9096 T 8500 L

R 2020 L

5−10−30
PART 2
Page 76
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−114 * Detailed Inspection of the Center−Wing Lower−Panel

Rev. F−1 57−11−101B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 6173 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5523 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2946 L

A/C 9096 T 8500 L

R 2946 L

RAS−C700−990 57−10−00−115 * Detailed Inspection of the Center−Wing Lower−Panel

Rev. G 57−11−104B (one star) Splice, BL47.61

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8514 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 8514 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 77
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−116 * Special Detailed Inspection of the Front Spar Root−Splice

Rev. F−1 57−11−106B (one star) Lower Cap

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 3670 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3670 L

A/C 9096 T 8500 L

R 3670 L

RAS−C700−990 57−10−00−117 * Special Detailed Inspection of the Rear Spar Splice of the
Rev. G1 57−11−107B (one star) Center−Wing

93500 lbs MTOW Pre SB 700−21−034 T 9195 L

R 8515 L

96000 lbs MTOW Pre SB 700−21−034 T 9195 L

R 8515 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 78
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−118 * Special Detailed Inspection of the Keel Beam Rib, BL4.75
Rev. G2 57−11−110B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 6393 L

EFFECTIVITY: ALL
R 4265 L

96000 lbs MTOW Pre SB 700−21−034 T 6393 L

R 4265 L

98000 lbs MTOW and any aircraft Post T 3666 L

SB 700−21−034 R 2273 L

RAS−C700−990 57−10−00−119 * Special Detailed Inspection of the Rear−Spar Lower−Cap,

Rev. G 57−11−113B (one star) BL44.00 to BL47.60

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 79
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−121 * Special Detailed Inspection of the Rear−Spar Lower−Cap

Rev. G 57−11−113C (one star) and Wing Skin Between LBL44.00 and RBL44.00

93500 lbs MTOW Pre SB 700−21−034 T 11335 L

EFFECTIVITY: ALL
R 4063 L

96000 lbs MTOW Pre SB 700−21−034 T 11335 L

R 4063 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4063 L

A/C 9096 T 8500 L

R 4063 L

RAS−C700−990 57−10−00−122 * Detailed Inspection of the Keel Beam Rib Truss−Beam

Rev. G 57−11−110C (one star) Pins, BL4.75

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 80
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−123 * Special Detailed Inspection of the Wing Front−Spar

Rev. G 57−11−112B (one star) Lower−Cap and Web at Keel Beam Attachments, BL4.75

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5042 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5042 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5042 L

A/C 9096 T 8500 L

R 5042 L

RAS−C700−990 57−10−00−124 * Detailed Inspection of the Front Spar Lower Cap of the
Rev. G 57−11−112C (one star) Center Wing from LBL47.60 to RBL47.60

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 81
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−10−00−125 * Special Detailed Inspection of the Center Wing Front−Spar

Rev. G 57−11−112D (one star) Lower−Cap and Web at FS574.50 from LBL47.60 to
RBL47.60

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−20−00−101 * Detailed Inspection of the Splice on the Lower Skin of the
Rev. G 57−21−101A (one star) Wing, WCS537.40

93500 lbs MTOW Pre SB 700−21−034 T 10132 L

R 9080 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 10132 L

R 9080 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

5−10−30
PART 2
R 6500 L

Page 82
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−102 * Detailed Inspection of the Wing Lower Fuel−Access−Holes

Rev. F−1 57−21−102A (one star) − External

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2937 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2705 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1230 L

A/C 9096 T 8500 L

R 1230 L

RAS−C700−990 57−20−00−103 * Detailed Inspection of the Wing Lower−Skin

Rev. F−1 57−21−103A (one star) Fuel−System−Holes

93500 lbs MTOW Pre SB 700−21−034 T 7681 L

R 5088 L

96000 lbs MTOW Pre SB 700−21−034 T 6077 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 3936 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5088 L

A/C 9096 T 7681 L

R 5088 L

5−10−30
PART 2
Page 83
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−104 * Special Detailed Inspection of the Lower Wing−Plank

Rev. G 57−21−104A (one star) Stringer−Runout

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 6347 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6347 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 6347 L

A/C 9096 T 8500 L

R 6347 L

RAS−C700−990 57−20−00−105 * Special Detailed Inspection of the Main Landing Gear

Rev. G 57−21−105A (one star) (MLG) Lower Strap, WS85.50

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7760 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7760 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 84
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−106 * Special Detailed Inspection of the Main Landing Gear

Rev. F−1 57−21−106A (one star) (MLG) Fitting Joint
57−21−106B
57−21−106C

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−20−00−108 * Special Detailed Inspection of the Rear Spar Splice,

Rev. G 57−21−108A (one star) WS178.00

93500 lbs MTOW Pre SB 700−21−034 T 10402 L

R 8154 L

96000 lbs MTOW Pre SB 700−21−034 T 10402 L

R 8154 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 4355 L

5−10−30
PART 2
Page 85
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−109 * Special Detailed Inspection of the Rear Spar Splice,

Rev. G 57−21−109A (one star) WS287.00
57−21−109B

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
R 9779 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 9779 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−20−00−110 * Special Detailed Inspection of the Lower Skin Splice at the
Rev. E 57−21−110A (one star) Front Spar, Canted Rib No. 2 to CWS390.90

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2767 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2632 L

98000 lbs MTOW and any aircraft Post T 3808 L

SB 700−21−034 R 2339 L

5−10−30
PART 2
Page 86
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−111 * Detailed Inspection of the Lower−Skin Spanwise−Splice

Rev. E 57−21−111A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 7958 L

EFFECTIVITY: ALL
R 4069 L

96000 lbs MTOW Pre SB 700−21−034 T 7745 L

R 3973 L

98000 lbs MTOW and any aircraft Post T 6232 L

SB 700−21−034 R 3628 L

RAS−C700−990 57−20−00−112 * Detailed Inspection of the Outer Wing Front and Rear Spar
Rev. E 57−21−112A (one star) Caps and Skin

93500 lbs MTOW Pre SB 700−21−034 T 8273 L

R 3840 L

96000 lbs MTOW Pre SB 700−21−034 T 7864 L

R 3671 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 980 L

5−10−30
PART 2
Page 87
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−113 * General Visual Inspection of the Wing Upper−Skin

Rev. F−1 57−21−113A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−20−00−114 * Detailed Inspection of the Wing Ribs at WS66.00,

Rev. F−1 57−21−114B (one star) WS178.00, WS287.00 and CWS464.20
57−21−116B
57−21−117B
57−21−118B

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 4246 L

A/C 9096 T 8500 L

R 4246 L

5−10−30
PART 2
Page 88
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−115 * Detailed Inspection of the Wing Rib at WS85.50

Rev. F−1 57−21−115A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 1799 L

96000 lbs MTOW Pre SB 700−21−034 T 11298 L

R 960 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1799 L

A/C 9096 T 8500 L

R 1799 L

RAS−C700−990 57−20−00−116 * Special Detailed Inspection of the Wing Rib at WS66.00

Rev. F−1 57−21−114A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 89
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−119 * Special Detailed Inspection of the Main Landing Gear

Rev. F−1 57−21−120A (one star) (MLG) Trunnion−Fitting

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 4397 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1528 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4397 L

A/C 9096 T 8500 L

R 4397 L

RAS−C700−990 57−20−00−120 * Special Detailed Inspection of the Splice on the Lower Skin
Rev. G 57−21−101B (one star) of the Wing, WCS537.40

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 10023 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 10023 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 90
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−121 * Detailed Inspection of the Wing Lower Fuel−Access−Holes

Rev. F−1 57−21−102B (one star) − Internal

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 6646 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 6079 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1100 L

A/C 9096 T 8500 L

R 1100 L

RAS−C700−990 57−20−00−122 * Detailed Inspection of the Lower Skin at the

Rev. E 57−21−111B (one star) Spanwise−Splice

93500 lbs MTOW Pre SB 700−21−034 T 6577 L

R 1543 L

96000 lbs MTOW Pre SB 700−21−034 T 6298 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1460 L

98000 lbs MTOW and any aircraft Post T 4823 L

SB 700−21−034 R 940 L

5−10−30
PART 2
Page 91
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−123 * Detailed Inspection of the Lower Skin at the Front and Rear
Rev. F−1 57−21−112B (one star) Spar Joints

93500 lbs MTOW Pre SB 700−21−034 T 12258 L

EFFECTIVITY: ALL
R 1105 L

96000 lbs MTOW Pre SB 700−21−034 T 11740 L

R 1050 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1030 L

A/C 9096 T 8500 L

R 1030 L

RAS−C700−990 57−20−00−125 * Special Detailed Inspection of the Wing Rib at WS178.00

Rev. F−1 57−21−116A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 5854 L

A/C 9096 T 8500 L

R 5854 L

5−10−30
PART 2
Page 92
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−126 * Special Detailed Inspection of the Wing Rib at WS287.00

Rev. F−1 57−21−117A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−20−00−127 * Special Detailed Inspection of the Wing Rib at CWS464.20

Rev. F−1 57−21−118A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 6500 L

5−10−30
PART 2
Page 93
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−20−00−128 * Detailed Inspection of the Wing Rib at WS85.50

Rev. G 57−21−115B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5548 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3393 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 4730 L

A/C 9096 T 8500 L

R 4730 L

RAS−C700−990 57−20−00−129 * Special Detailed Inspection of the Lower Splice of the Front
Rev. G1 57−21−107A (one star) Spar, WS275.60 and WS549.55

93500 lbs MTOW Pre SB 700−21−034 T 9676 L

R 7073 L

96000 lbs MTOW Pre SB 700−21−034 T 9676 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7073 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7073 L

A/C 9096 T 8500 L

R 5702 L

5−10−30
PART 2
Page 94
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−30−00−101 * Special Detailed Inspection of the Winglet Installation

Rev. G 57−30−101A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 7500 L

EFFECTIVITY: ALL
R 7500 L

96000 lbs MTOW Pre SB 700−21−034 T 7500 L

R 7500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−30−00−102 * Detailed Inspection of the Winglet − External Surfaces

Rev. G 57−30−101B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 7500 L

R 7500 L

96000 lbs MTOW Pre SB 700−21−034 T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 7500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 95
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−00−101 * Special Detailed Inspection of the No. 1 Slat Tracks

Rev. F−1 57−40−101A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2785 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 764 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2785 L

A/C 9096 T 8500 L

R 2785 L

RAS−C700−990 57−42−00−103 * Special Detailed Inspection of the No. 2 Slat Tracks

Rev. F−1 57−40−102A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 96
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−00−104 * Special Detailed Inspection of the No. 3 Slat Tracks

Rev. F−1 57−40−103A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 5663 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4183 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 5663 L

A/C 9096 T 8500 L

R 5663 L

RAS−C700−990 57−42−00−105 * Special Detailed Inspection of the No. 4 Slat Tracks

Rev. F−1 57−40−104A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 12500 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 2593 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 97
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−00−107 * Special Detailed Inspection of the No. 1 Slat to Track

Rev. F−1 57−40−105A (one star) Attachments

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 2657 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1763 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2657 L

A/C 9096 T 8500 L

R 2657 L

RAS−C700−990 57−42−00−108 * Special Detailed Inspection of the No. 2 Slat to Track

Rev. F−1 57−40−106A (one star) Attachments

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 5623 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 5623 L

A/C 9096 T 8500 L

R 5623 L

5−10−30
PART 2
Page 98
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−00−109 * Detailed Inspection of the Slat Track Attachment Lugs, Slat
Rev. F−1 57−40−107B (one star) No. 3 and No. 4
57−40−108A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−42−00−111 * Special Detailed Inspection of the No. 3 Slat to Track

Rev. F−1 57−40−107A (one star) Attachments

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 8276 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2964 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1307 L

A/C 9096 T 8500 L

R 1307 L

5−10−30
PART 2
Page 99
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−02−101 * Detailed Inspection of the Slat Body, Slat No. 1 and No. 2
Rev. F−1 57−40−109A (one star)
57−40−110A

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 12500 L
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−42−02−103 * Detailed Inspection of the Slat Body, Slat No. 3 and No. 4
Rev. F−1 57−40−111A (one star)
57−40−112A

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 2134 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1648 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 2134 L

A/C 9096 T 8500 L

R 2134 L

5−10−30
PART 2
Page 100
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−02−104 * Special Detailed Inspection of the No. 4 Slat Bodies

Rev. F−1 57−40−112B (one star) Interconnect Pin

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 10401 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 4109 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−42−02−105 * Special Detailed Inspection of the Slat No. 1 to No. 4 Roller
Rev. F−1 57−40−113A (one star) Pins

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7766 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 5636 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

5−10−30
PART 2
Page 101
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−42−02−106 * Detailed Inspection of the Slat No. 1 to No. 4 Support Ribs
Rev. F−1 57−40−113B (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−51−00−101 * Special Detailed Inspection of the Flap Track, WS47.80

Rev. F−1 57−50−101A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 1571 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1571 L

A/C 9096 T 8500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1571 L

5−10−30
PART 2
Page 102
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−51−00−102 * Special Detailed Inspection of the Flap Support Structure,

Rev. F−1 57−50−102A (one star) WS178.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 7509 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−51−00−103 * Special Detailed Inspection of the Flap Track, WS287.00

Rev. F−1 57−50−103A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1283 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1246 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 1283 L

A/C 9096 T 8500 L

R 1283 L

5−10−30
PART 2
Page 103
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−51−00−104 * Special Detailed Inspection of the Flap Track, WS404.00

Rev. G 57−50−104A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 956 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 956 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 956 L

A/C 9096 T 8500 L

R 956 L

RAS−C700−990 57−51−00−105 * Special Detailed Inspection of the Flap Carriage, WS47.80,

Rev. G 57−50−105A (one star) WS178.00, WS287.00 and WS404.00.

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3176 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 3176 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3176 L

A/C 9096 T 8500 L

R 3176 L

5−10−30
PART 2
Page 104
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−51−00−106 * Special Detailed Inspection of the Flap Side Fitting,

Rev. F−1 57−50−106A (one star) WS47.80

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−51−00−107 * Special Detailed Inspection of the Flap Rail Forward Fitting,
Rev. G 57−50−107A (one star) WS287.00 and WS404.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5306 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 5306 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 5306 L

A/C 9096 T 8500 L

R 5306 L

5−10−30
PART 2
Page 105
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−51−00−108 * Special Detailed Inspection of the Flap Body Fitting

Rev. F−1 57−50−108A (one star) (Metallic), WS178.00, WS287.00 and WS404.00

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−51−00−109 * Special Detailed Inspection of the Inboard, Mid and

Rev. G 57−50−109A (one star) Outboard Flap (Metallic) End Ribs

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3096 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 3096 L

98000 lbs MTOW and any aircraft Post T 7500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

SB 700−21−034 R 3096 L

A/C 9096 T 8500 L

R 3096 L

RAS−C700−990 57−51−00−110 * Detailed Inspection of the Inboard, Mid and Outboard Flaps T 7500 L
Rev. D 57−50−110A (one star) (Composite) R 7500 L

5−10−30
PART 2
Page 106
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−60−00−101 * Special Detailed Inspection of the Aileron Center−Hinge

Rev. F−1 57−60−101A (one star) Assembly

93500 lbs MTOW Pre SB 700−21−034 T 10150 L

EFFECTIVITY: ALL
R 1757 L

96000 lbs MTOW Pre SB 700−21−034 T 8335 L

R 1395 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1757 L

A/C 9096 T 8500 L

R 1757 L

RAS−C700−990 57−60−00−103 * Special Detailed Inspection of the Aileron Inner−Hinge and

Rev. G 57−60−102A (one star) Outer−Hinge Pins

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

R 1581 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 1581 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 1581 L

A/C 9096 T 8500 L

R 1581 L

5−10−30
PART 2
RAS−C700−990 57−60−00−104 * Detailed Inspection of the Ailerons T 7500 L
Rev. D 57−60−103A (one star) R 7500 L

Page 107
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 57−60−00−105 * Special Detailed Inspection of the Aileron Inner−Hinge and

Rev. G 57−60−102B (one star) Outer−Hinge Fitting Assemblies

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
R 7560 L

96000 lbs MTOW Pre SB 700−21−034 T 12500 L

R 7560 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

A/C 9096 T 8500 L

R 6500 L

RAS−C700−990 57−70−00−101 * Special Detailed Inspection of the Spoilers No. 1 to No. 6

Rev. G 57−70−101A (one star) Hinge Fittings

93500 lbs MTOW Pre SB 700−21−034 T 3066 L

R 763 L

96000 lbs MTOW Pre SB 700−21−034 T 3066 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

R 763 L

98000 lbs MTOW and any aircraft Post T 3066 L

SB 700−21−034 R 763 L

RAS−C700−990 57−70−00−102 * Detailed Inspection of the Spoilers No. 1 to No. 6 T 7500 L

Rev. D 57−70−102A (one star) R 7500 L

5−10−30
PART 2
Page 108
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 71−12−01−101 * Detailed Inspection of the Upper Fan−Cowl−Door

Rev. E 71−10−103A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

RAS−C700−990 71−21−01−101 * Special Detailed Inspection of the Front Mount Beam and
Rev. E 71−20−101A (one star) Links

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 10013 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

RAS−C700−990 71−21−01−102 * Special Detailed Inspection of the Thrust Strut

Rev. E 71−20−102A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 7667 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

5−10−30
PART 2
Page 109
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 71−21−01−103 * Special Detailed Inspection of the Front Mount Link Pins,
Rev. F−1 71−20−103A (one star) Thrust Strut Pins, Thrust Pin and Pylon Attachment Pins
NOTE: Replacement of pin and all associated hardware

EFFECTIVITY: ALL
(e.g.; nut, washers, and cotter pin) restarts the inspection
threshold.

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 12500 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

RAS−C700−990 71−22−01−101 * Special Detailed Inspection of the Rear Mount Beam and
Rev. E 71−20−105A (one star) Links

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

96000 lbs MTOW Pre SB 700−21−034 R 8000 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RAS−C700−990 71−22−01−102 * Special Detailed Inspection of the Rear Mount Link Pins
Rev. F−1 71−20−106A (one star) and Pylon Attachment Pins
NOTE: Replacement of pin and all associated hardware
(e.g.; nut, washers, and cotter pin) restarts the inspection
threshold.

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

5−10−30
PART 2
96000 lbs MTOW Pre SB 700−21−034 R 12333 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 7500 L

Page 110
May 03/2018
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 78−31−01−101 * Detailed Inspection of the Thrust Reverser Upper Door

Rev. E 78−30−104A (one star)

93500 lbs MTOW Pre SB 700−21−034 T 12500 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 3491 L

98000 lbs MTOW and any aircraft Post T 7500 L

SB 700−21−034 R 3491 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−30
PART 2
Page 111
May 03/2018
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−40

CERTIFICATION MAINTENANCE REQUIREMENTS

Tasks by Chapter 5 Task Number

EFFECTIVITY: ALL
PART 2 Cover
5−10−40 Dec 11/2013
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRG700−013 21−31−00−101 ** Operational Test of the Emergency 1500 H 50 H

Rev. N/A 7.1.1.13 (two stars) Depressurization Function NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
RBRG700−013 21−31−00−103 ** Functional Test of the Cabin−Pressure Leakage 120 M 3M
Rev. F 7.1.1.10 (two stars) Rate NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRG700−013 21−31−09−101 * Functional Test of the Safety Valves 3000 H 50 H

Rev. F 7.1.1.5, (one star) NOTE A
NOTE: See section 5−10−05, paragraph 5.
7.1.1.6

RBRG700−121 21−52−00−101 ** Operational Test of the Manual Mode of the Air 1500 H 50 H
Rev. A 7.1.2.1 (two stars) Conditioning System NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRG700−121 21−53−05−101 ** Operational Test of the Ram Air Valve 1500 H 50 H

Rev. A 7.1.1.1 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RBRG700−121 21−60−00−101 ** Operational Test of the Auxiliary Pressurization 1500 H 50 H

Rev. A 7.1.1.3 (two stars) Function NOTE A
NOTE: See section 5−10−05, paragraph 5.

5−10−40
PART 2
Nov 26/2014
Page 1
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RAE−L700−198 24−23−01−101 * Operational Test of the Ram Air Turbine (RAT) 24 M 3M

Rev. A5 3.1.1.1 (one star) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
RBR−L700−158 24−23−01−102 * Functional Test of the Ram Air Turbine (RAT) 24 M 3M
Rev. E 3.1.1.2 (one star) Heater NOTE A
NOTE: See section 5−10−05, paragraph 5.

RAE−L700−158 24−61−00−101 * Operational Test of the Gate Array and Power 1000 H 50 H
Rev. E 3.2.1 (one star) Supplies in the DCPC (A/C 9002 to 9122 Pre SB NOTE A
700−24−045)
NOTE: See section 5−10−05, paragraph 5.
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Dec 11/2013
Page 2
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRT700−230 27−11−13−101 ** Visual Check of the Roll Control Input−Module 1500 H 50 H

Rev. D3 7.1.2.1 (two stars) (A/C 9002 to 9124 Pre SB 700−27−036)

EFFECTIVITY: ALL
RBRC700−103 27−11−25−101 * Functional Test of the Aileron Power−Control 1500 H 50 H
Rev. N/A 7.1.1.17 (one star) Unit (PCU)

RBRC700−103 27−11−25−102 ** Functional Test of the Aileron PCU Bungee 3000 H 50 H

Rev. A1 7.1.1.14 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRC700−103 27−11−35−101 ** Functional Test of the Aileron Cable Tension − 30 M 3M

Rev. A−1 Add. 4 7.1.1.18 (two stars) Flight Compartment Cables NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRC700−103 27−11−35−102 ** Functional Test of the Aileron Cable Tension − 30 M 3M

Rev. A−1 Add. 4 7.1.1.17 (two stars) Fuselage Cables NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRC700−103 27−11−35−103 ** Detailed Inspection of the Aileron Control Cables 30 M

Rev. C−2−1 7.1.1.21 (two stars) in the Main Landing Gear (MLG) Wheel Well
BD−700 TIME LIMITS/MAINTENANCE CHECKS

(Post SB 700−27−086 PART I or PART J or

PART K or PART L or PART M or PART N or
PART O or PART P)

RBRC700−103 27−11−35−104 ** Detailed Inspection of the Aileron Control Cables 15 M

Rev. C−2−1 7.1.1.22 (two stars) in the Wing Trailing Edge, at the Inner, Mid and

5−10−40
PART 2
Outer Flap Areas (Post SB 700−27−086 PART
M or PART N or PART O or PART P)

Page 3
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRC700−102 27−21−09−101 ** Operational Test of the Rudder Power−Control 3000 H 50 H

Rev. A 7.1.1.2 (two stars) Unit (PCU) Input Limiters NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
RBRC700−102 27−21−13−101 ** Functional Test of the Rudder Power−Control 3000 H 50 H
Rev. A 7.1.1.7 (two stars) Units (PCU) NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRC700−102 27−21−27−101 ** Functional Test of the Rudder Cable Tension 30 M 3M

Rev. A−1 Add. 4 7.1.1.7 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRC700−104 27−31−21−101 * Functional Test of the Elevator Power−Control 1500 H 50 H

Rev. N/A 7.1.1.23 (one star) Units (PCU)

RBRT700−230 27−41−09−102 ** Visual Check of the Pitch Trim Actuator (A/C 1500 H 50 H
Rev. D3 7.1.2.3 (two stars) 9002 to 9124 Pre SB 700−27−036)

RBRT700−230 27−41−09−103 * Detailed Inspection of the Pitch Trim Actuator 500 H 50 H

Rev. D5 7.1.1.13 (one star)
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RBRT700−111 27−52−57−101 * Detailed Inspection of the Flap Rollers 3000 H 50 H

Rev. NC 7.1.1.2 (one star) NOTE A
NOTE: See section 5−10−05, paragraph 5.

RBRT700−111 27−53−09−101 ** Functional Test of the Slat System Actuators 3000 H 50 H

5−10−40
PART 2
Rev. A 7.1.1.1 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

Page 4
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRT700−230 27−60−00−101 ** Operational Test of the Spoiler Power−Control 1500 H 50 H

Rev. D 7.1.1.4 (two stars) Units (PCU) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
RBRT700−230 27−61−17−101 * Operational Test of the Ground Lift Dumping 3000 H 50 H
Rev. D 7.1.1.8 (one star)
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 5
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBR−P700−142 28−41−00−101 ** Functional Test of the Temperature Sensors 120 M 3M

Rev. A4 7.1.1.7 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 6
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRX700−820 29−12−33−101 ** Operational Test of the Firewall Hydraulic 1500 H 50 H

Rev. A 7.1.1.6 (two stars) Shutoff−Valves

EFFECTIVITY: ALL
RBRX700−820 29−13−00−101 * Operational (Internal Leak) Test of the No. 3 1500 H 50 H
Rev. A 7.1.1.5 (one star) Hydraulic System NOTE A
NOTE: See section 5−10−05, paragraph 5.
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 7
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRW700−500 32−31−09−101 ** Visual Check of the Landing−Gear Electronic 3000 H 50 H

Rev. B 7.1.1.1 (two stars) Control Unit (LG ECU) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 8
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RAZ−C700−123 34−11−00−101 * Functional Test of the Air Data Computer, 24 M 3M

Rev. NC−1 7.2.1 (one star) (Post SB 700−34−014, RVSM Qualified A/C) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 9
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRD700−002 52−31−09−101 ** Detailed Inspection of the Baggage Door Seal 15 M 3M

Rev. A 7.1.2.1 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 10
May 19/2021
 Allowable
Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval Extension

RBRB700−124 78−33−05−101 ** Operational Test of the Tertiary Lock 4500 H 50 H

Rev. A 7.1.1.3 (two stars) NOTE A
NOTE: See section 5−10−05, paragraph 5.

EFFECTIVITY: ALL
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−40
PART 2
Page 11
May 19/2021
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

PART 2
SECTION 5−10−50

HASC REQUIREMENTS
Tasks by Chapter 5 Task Number

EFFECTIVITY: ALL
PART 2 Cover
5−10−50 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 52−11−00−105 * General Visual Inspection of the Skin External Surface

Rev. E HASC (one star)

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 52−21−00−103 * General Visual Inspection of the External Skin of the

Rev. E HASC (one star) Overwing Emergency Exit

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 52−30−00−108 * General Visual Inspection of the External Surface of the

Rev. E HASC (one star) Baggage Door Skin Including Door Handle Recess

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 1
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−117 * Detailed Inspection of the Forward Face of Bulkhead,

Rev. E HASC (one star) FS202.75, Above Floor

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−10−00−118 * Detailed Inspection of the Forward Face of

Rev. E HASC (one star) Bulkhead,FS202.75 Web, Below Floor

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−10−00−119 * General Visual Inspection of the External Skin, FS169.00 to

Rev. E HASC (one star) FS280.00

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 2
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−120 * Detailed Inspection of the Longitudinal and Circumferential

Rev. E HASC (one star) Skin Joints, FS202.75 to FS280.00

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−10−00−121 * Detailed Inspection of the NLG and Pressurized Panel

Rev. E HASC (one star) Cutout Surround Structure

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−10−00−122 * Detailed Inspection of the Windshield and Side−Window

Rev. E HASC (one star) Cutout Surround Structure

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 3
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−10−00−123 * Detailed Inspection of the Pressurized Surfaces of the

Rev. E HASC (one star) Nose Landing Gear (NLG) Wheel Well Structure

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−128 * General Visual Inspection of the External Top Skin of the
Rev. E HASC (one star) Fuselage, FS381.00 to FS557.00 and STR6L to STR6R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−129 * General Visual Inspection of the Lower External Skin of the
Rev. E HASC (one star) Fuselage, FS381.00 to FS557.00 and STR6L to STR6R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 4
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−130 * Detailed Inspection of the External Avionics− Compartment

Rev. E HASC (one star) Access Surround Structure

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−131 * Detailed Inspection of the Aft Face of the Pressure

Rev. E HASC (one star) Bulkhead Below WL71.50, FS557.00

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−132 * Detailed Inspection of the Lower Side of the Pressure Floor
Rev. E HASC (one star) FS557.00 to FS574.60 and BL46L to BL46R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 5
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−133 * General Visual Inspection of the External Top Skin of the
Rev. E HASC (one star) Fuselage, FS281.00 to FS381.00 and STR2L to STR7R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−134 * General Visual Inspection of the External Left Side and
Rev. E HASC (one star) Lower Skin, FS281.00 to FS381.00 and STR2L to STR25L

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−135 * Detailed Inspection of the Sills, Frame, Skin and Edge
Rev. E HASC (one star) Members Around the Passenger Door Cutout

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 6
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−136 * General Visual Inspection of the External Right Side and
Rev. E HASC (one star) Lower Skin, FS281.00 to FS381.00 and STR7R to STR25R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−137 * Detailed Inspection of the External Skin Around the

Rev. E HASC (one star) Window Surround Cutouts

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−138 * Detailed Inspection of the Fuselage Longitudinal Joints,

Rev. E HASC (one star) FS281.00 to FS381.00, STR2L, STR7R, STR14L, STR19R
and STR25L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 7
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−20−00−139 * Detailed Inspection of the Fuselage Longitudinal Joints,

Rev. E HASC (one star) FS381.00 to FS557.00, STR6R, STR6L, STR20R and
STR20L

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 6250 L
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−20−00−140 * Detailed Inspection of the External Skin Around the Service
Rev. E HASC (one star) Door Cutout, FS295.00 to FS310.00 and STR22R to
STR24R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−30−00−124 * General Visual Inspection of the External Skin of the

Rev. E HASC (one star) Fuselage Not Behind the Fairing, FS557.00 to FS797.60
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 8
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−125 * General Visual Inspection of the External Skin of the

Rev. E HASC (one star) Fuselage Behind the Fairing, FS557.00 to FS797.60

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−30−00−126 * Detailed Inspection of the Surround Structure for the

Rev. E HASC (one star) Overwing Emergency Exit

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−30−00−127 * Detailed Inspection of the External Skin of Cabin Window

Rev. E HASC (one star) Cutouts, Surround Structure

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

BD−700 TIME LIMITS/MAINTENANCE CHECKS

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 9
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−30−00−128 * Detailed Inspection of the Lower Side of the Pressure Floor
Rev. E HASC (one star) FS719.30 to FS781.00 and BL35L to BL35R

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−30−00−129 * Detailed Inspection of the Pressure Bulkheads, FS719.30

Rev. E HASC (one star) and FS781.00 − External

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−30−00−130 * Detailed Inspection of the Circumferential Skin Joint at

Rev. E HASC (one star) FS557.00 and Longitudinal Skin Joints at STR6 and
STR18, L and R
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 10
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−129 * General Visual Inspection of the External Skin of the

Rev. E HASC (one star) Pressurized Fuselage, FS797.00 to FS861.00

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−40−00−130 * Detailed Inspection of the Circumferential and Logitudinal

Rev. E HASC (one star) Skin Joints of the Pressure Shell not Covered by
Wing−to−Fuselage Fairings

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−40−00−131 * Detailed Inspection of the Baggage Door Cutout Surround

Rev. E HASC (one star) Structure
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 11
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−132 * General Visual Inspection of the External Skin of the

Rev. E HASC (one star) Fuselage Beneath the Wing−to−Fuselage Fairing in the
Pressurized Zone

EFFECTIVITY: ALL
93500 lbs MTOW Pre SB 700−21−034 T 6250 L
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−40−00−133 * Detailed Inspection of the Circumferential and Longitudinal

Rev. E HASC (one star) Skin Joints Beneath the Wing−to−Fuselage Fairing

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

RAS−C700−990 53−40−00−134 * Detailed Inspection of the Pressure Bulkhead Forward Web

Rev. E HASC (one star) Below Floor
BD−700 TIME LIMITS/MAINTENANCE CHECKS

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L

5−10−50
PART 2
Dec 11/2013
Page 12
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 53−40−00−135 * Detailed Inspection of the Pressure Bulkhead Web Above

Rev. E HASC (one star) Floor

93500 lbs MTOW Pre SB 700−21−034 T 6250 L

EFFECTIVITY: ALL
96000 lbs MTOW Pre SB 700−21−034 R 6250 L

98000 lbs MTOW and any aircraft Post T 3750 L

SB 700−21−034 R 3750 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−50
PART 2
Dec 11/2013
Page 13
 BD−700 TIME LIMITS/MAINTENANCE CHECKS

LIFE LIMITS (STRUCTURES)

1. For CIS operators only this section supersedes section 5−10−10.

The structural life limits of the Safe−Life items shown on the pages that follow are taken from
the Structural Airworthiness Control Document. Discard is mandatory at the expiry of the
specified structural life limit for the item. These life limit values may be superseded by the life
limits contained in section 5−10−19, for specific serialized components.

NOTES: [1] Individual Main and Nose Landing Gear component utilization must be
recorded from the time of initial installation.

[2] If no dash number is specified, the life limit is applicable to all the dash
numbers of the part numbers listed.

[3] The non−serialized pin/bolts must be discarded on removal from aircraft and at
intervals not exceeding the discard time presented in this section.

EFFECTIVITY: ALL
PART 2 Page 1
5−10−90 Dec 11/2013
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−11−01−101 * Discard the Main Landing Gear (MLG) Connecting Shock 7500 L
Rev. E4 32−11−105 (one star) Strut/Trailing Arm Pin, Part No. 21115 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−11−01−102 * Discard the Main Landing Gear (MLG) Connecting Shock 7500 L
Rev. E4 32−11−105 (one star) Strut/Main Fitting Pin, Part No. 21260 and 21274−1 COMPONENT

RAS−C700−990 32−11−01−103 * Discard the Main Landing Gear (MLG) Shock Strut 7500 L
Rev. E4 32−11−105 (one star) Cylinder, Part No. 21206 and 21209 COMPONENT

RAS−C700−990 32−11−01−104 * Discard the Main Landing Gear (MLG) Shock Strut Piston, 7500 L
Rev. E4 32−11−105 (one star) Part No. 21216 and 21218 COMPONENT

RAS−C700−990 32−11−01−105 * Discard the Main Landing Gear (MLG) Connecting Shock 5500 L
Rev. E4 32−11−105 (one star) Strut/Trailing Arm Pin, Part No. 21194−1 COMPONENT

RAS−C700−990 32−11−09−101 * Discard the Main Landing Gear (MLG) Trailing Arm/Axle, 7500 L
Rev. E4 32−11−103 (one star) Part No. 21410 COMPONENT
32−11−106

RAS−C700−990 32−11−09−102 * Discard the Main Landing Gear (MLG) Pivot Pin, Part No. 7500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Rev. E4 32−11−103 (one star) 21114 COMPONENT

RAS−C700−990 32−11−17−101 * Discard the Main Landing Gear (MLG) Side−Stay 5584 L
Rev. E4 32−11−104 (one star) Lower−Pin, Part No. 21113 COMPONENT

RAS−C700−990 32−11−17−102 * Discard the Main Landing Gear (MLG) Side Brace Rod 4342 L

5−10−90
PART 2
Rev. E4 32−11−104 (one star) End, Part No. 21510 COMPONENT

RAS−C700−990 32−11−17−103 * Discard the Main Landing Gear (MLG) Side Brace Piston, 4342 L
Rev. E4 32−11−104 (one star) Part No. 21512 COMPONENT

Dec 11/2013
Page 2
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−11−17−104 * Discard the Main Landing Gear (MLG) Side Brace Cylinder, 4342 L
Rev. E4 32−11−104 (one star) Part No. 21521 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−11−29−101 * Discard the Main Landing Gear (MLG) Main Fitting, Part 7500 L
Rev. E4 32−11−102 (one star) No. 21310 COMPONENT

RAS−C700−990 32−11−29−102 * Discard the Main Landing Gear (MLG) Pintle Pin, Part No. 5636 L
Rev. E4 32−11−102 (one star) 21112 COMPONENT

RAS−C700−990 32−11−29−103 * Discard the Main Landing Gear (MLG) Pintle Pin/Cross Pin, 7500 L
Rev. E4 32−11−102 (one star) Part No. 21116−1 COMPONENT

RAS−C700−990 32−21−01−101 * Discard the Nose Landing Gear (NLG) Shock Strut Axle, 7500 L
Rev. E4 32−21−105 (one star) Part No. 1286−0201 and 1286−0203 COMPONENT

RAS−C700−990 32−21−01−102 * Discard the Nose Landing Gear (NLG) Shock Strut Piston 7500 L
Rev. E4 32−21−103 (one star) (Sliding Tube), Part No. 1286−0001 and 1286−0077 COMPONENT

RAS−C700−990 32−21−01−103 * Discard the Nose Landing Gear (NLG) Shock Strut Main 5648 L
Rev. E4 32−21−102 (one star) Fitting, Part No. 1286−0101 COMPONENT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

RAS−C700−990 32−21−05−101 * Discard the Nose Landing Gear (NLG) Upper Drag Brace, 6270 L
Rev. E4 32−21−104 (one star) Part No. 22511 COMPONENT

RAS−C700−990 32−21−05−102 * Discard the Nose Landing Gear (NLG) Lower Drag Brace, 5760 L
Rev. E4 32−21−104 (one star) Part No. 22516 COMPONENT

5−10−90
PART 2
RAS−C700−990 32−21−05−105 * Discard the Nose Landing Gear (NLG) Drag Brace Apex 5595 L
Rev. E4 32−21−104 (one star) Pin, Part No. 22530 COMPONENT

Dec 11/2013
Page 3
 Source Document Ref. No. Chapter 5 Task No. Task Title Task Interval

RAS−C700−990 32−21−05−106 * Discard the Nose Landing Gear (NLG) Drag Brace 5610 L
Rev. E4 32−21−104 (one star) Trunnion Pin, Part No. 22534 COMPONENT

EFFECTIVITY: ALL
RAS−C700−990 32−32−01−105 * Discard the Main Landing Gear (MLG) Retraction Actuator 25000 L
Rev. E4 (one star) Assembly, Part No. 21600 COMPONENT

RAS−C700−990 32−32−05−107 * Discard the Main Landing Gear (MLG) Uplock Assembly, 25000 L
Rev. E4 (one star) Part No. 21900 COMPONENT

RAS−C700−990 32−33−01−105 * Discard the Nose Landing Gear (NLG) Retraction Actuator 20000 L
Rev. E4 (one star) Assembly, Part No. 22400−101/−103 COMPONENT

RAS−C700−990 32−33−05−106 * Discard the Nose Landing Gear (NLG) Uplock Assembly, 25000 L
Rev. E4 (one star) Part No. 22600−101/−103 COMPONENT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−10−90
PART 2
Nov 22/2019
Page 4
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3

MAINTENANCE REVIEW BOARD REPORT

Revision V dated Feb 28/2020

Cover
PART 3 Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

TRANSPORT CANADA APPROVAL PAGE

This report (revision V) outlines the initial minimum scheduled maintenance/inspection

requirements to be used in the development of an approved continuous maintenance program for
the airframe, engines, systems, and components for the Bombardier Global series aircraft that
follow:
Model BD−700−1A10
Market Designation: Global Express (GX)
Global Express XRS (XRS)
Global 6000 (GL6000)
Global 6500 (GL6500)
Model BD−700−1A11
Market Designation: Global 5000 (GL5000)
Global 5000 Featuring Global Vision Flight Deck (GV5000)
Global 5500 (GL5500)

The tasks and their frequencies listed in this report form part of the Instructions for Continued
Airworthiness as required by AWM 525.1529, Appendix H.
The requirements in this MRB report have been developed using the Maintenance Program
Development Document, MSG−3, Revision 2, process and logic.
Transport Canada hereby approves this MRB report for use by Canadian operators of all
Bombardier Global series aircraft shown above.
This MRB report is intended to assist operators in the development process of an initial
maintenance program that is compatible with current regulations/policies.

Signed: (Signed original page on file at Bombardier) Date: May 08/2020

Brad Taylor
Global series MRB Chairperson

Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

EUROPEAN AVIATION SAFETY AGENCY (EASA) APPROVAL PAGE

This MRB Report is approved by Transport Canada as the Competent Authority (CA) under the
provision of the latest applicable revision of the Technical Implementation Procedures for
Airworthiness and Environmental Certification under the agreement on Civil Aviation Safety
between the Government of Canada and the European Union.

May 31/2019
 

 
 
MAINTENANCE REVIEW BOARD REPORT

FEDERAL AVIATION ADMINISTRATION (FAA) APPROVAL PAGE

This report outlines the minimum scheduled tasking/interval requirements to be used in the
development of an airworthiness maintenance/inspection program for the airframe, engines,
systems and components for the Bombardier Global series aircraft that follow:


 
Market Designation: Global Express (GX)
Global Express XRS (XRS)
Global 6000 (GL6000)
Global 6500 (GL6500)



Market Designation: Global 5000 (GL5000)
Global 5000 Featuring Global Vision Flight Deck (GV5000)
Global 5500 (GL5500)

The exception to this approval is, Airworthiness Limitations, which is the responsibility of the
appropriate Aircraft Certification Office (ACO), the CCMR section listed in the ALS with any
reference to the MRBR report task number is not approved by the Aircraft Evaluation Group (AEG).

The requirements in this report have been developed using Maintenance Steerin


!!"#$

The FAA hereby approves that this report MRBR Rev V dated February 28, 2020 be used by U.S.
certificated air carriers (and/or U.S. certificated operators) of the Bombardier Global series aircraft
shown above.

Digitally signed by HARRY P WALKER

HARRY P WALKER 5/8/2020
Signed: Date: 2020.05.06 08:43:39 -07'00'
Date
Harry Paul Walker, FAA Bombardier Global series
MRB Chairperson
Long Beach Aircraft Evaluation Group (AEG)
Federal Aviation Administration
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

LOG OF MRBR REVISIONS

MRBR REV. NO. MRBR REV. DATE PROGRAM TLMC REV. NO. TLMC REV. DATE

A Jun 19/1998 GX NC Dec 21/1998

B Feb 15/1999 GX 1 Apr 30/1999
C Aug 31/1999 GX 2 Nov 03/1999
C Aug 31/1999 GX 3 Feb 14/2000
D Aug 16/2000 GX 4 Oct 23/2000
E Jan 29/2001 GX 5 Oct 01/2001
F Sep 27/2002 GX 6 Jun 02/2003
F Sep 27/2002 GX 7 Dec 12/2003
G Mar 12/2004 GX 8 Mar 12/2004
NC G5000 NC
H Dec 02/2004 GX 9 Aug 12/2005
A Jan 18/2005 G5000 1
I Nov 23/2005 GX 10 Mar 28/2006
B G5000 2
J Feb 28/2007 GX 11 Jul 26/2007
C G5000 3
J Feb 28/2007 GX 12 Jun 24/2008
J XRS NC
C G5000 4
K Mar 28/2008 GX 13 Sep 15/2008
K XRS 1
D G5000 5
L Jun 22/2009 GX 14 May 26/2010
L XRS 2
E G5000 6
L Jun 22/2009 GX 15 Aug 03/2010
L XRS 3
E G5000 7
M Aug 05/2010 GX 16 Nov 09/2010
M XRS 4
F G5000 8
N Jan 21/2011 GX 17 May 24/2011
XRS 5
G5000 9

Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MRBR REV. NO. MRBR REV. DATE PROGRAM TLMC REV. NO. TLMC REV. DATE

O Nov 30/2011 GX 18 Nov 30/2011

XRS 6
GL5000 10
GL6000 NC Dec 12/2011
GV5000 NC
P Feb 16/2012 GX 19 Aug 17/2012
XRS 7
GL5000 11
GL6000 1
GV5000 1
Q Jan 18/2013 GX 20 Aug 22/2013
XRS 8
GL5000 12
GL6000 2
GV5000 2
R Jun 19/2013 GX 21 Dec 11/2013
XRS 9
GL5000 13
GL6000 3
GV5000 3
R Jun 19/2013 GX 22 Nov 26/2014
XRS 10
GL5000 14
GL6000 4
GV5000 4
S Nov 21/2014 GX 23 May 11/2015
XRS 11
GL5000 15
GL6000 5
GV5000 5
S Nov 21/2014 GX 24 Aug 06/2015
XRS 12
GL5000 16
GL6000 6
GV5000 6
S Nov 21/2014 GX 25 Feb 10/2016
XRS 13
GL5000 17
GL6000 7
GV5000 7
T Jan 29/2016 GX 26 Jul 29/2016
XRS 14
GL5000 18
GL6000 8
GV5000 8
T Jan 29/2016 GX 27 Sep 06/2016
T Jan 29/2016 GX 28 Nov 13/2017
XRS 15
GL5000 19
GL6000 9
GV5000 9

May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MRBR REV. NO. MRBR REV. DATE PROGRAM TLMC REV. NO. TLMC REV. DATE

T Jan 29/2016 GX 29 May 03/2018

XRS 16
GL5000 20
GL6000 10
GV5000 10
U May 31/2019 GX 30 Nov 22/2019
XRS 17
GL5000 21
GL6000 11
GV5000 11
GL6500 Basic Sep 16/2019
GL5500 Basic
V Feb 28/2020 GX 31 Aug 17/2020
XRS 18
GL5000 22
GL6000 12
GV5000 12
GL6500 1
GL5500 1

Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3

MAINTENANCE REVIEW BOARD REPORT

LIST OF EFFECTIVE PAGES

Section Effectivity Page Date Section Effectivity Page Date

Title Page Cover Feb 28/2020 20200228 5−20−05 ALL 9 Feb 28/2020 20200228

10 May 31/2019 20190531

TRANSPORT CANADA
APPROVAL PAGE Feb 28/2020 20200228 5−21−00 ALL 1 Jun 19/2013 20130619

2 Jun 19/2013 20130619

EUROPEAN AVIATION 3 Jun 19/2013 20130619

SAFETY AGENCY 4 May 31/2019 20190531

(EASA) APPROVAL 5 May 31/2019 20190531

PAGE Feb 28/2020 20200228 6 May 31/2019 20190531

7 May 31/2019 20190531

FEDERAL AVIATION 8 May 31/2019 20190531

ADMINISTRATION 9 May 31/2019 20190531

(FAA) APPROVAL 10 May 31/2019 20190531

PAGE Feb 28/2020 20200228

5−21−10 Cover Jun 19/2013 20130619

LOG OF MRBR
REVISIONS Feb 28/2020 20200228 5−21−10 ALL 1 May 31/2019 20190531

2 May 31/2019 20190531

Effective Pages 1 Feb 28/2020 20200228 3 May 31/2019 20190531

2 Feb 28/2020 20200228 4 May 31/2019 20190531

3 Feb 28/2020 20200228 5 May 31/2019 20190531

6 May 31/2019 20190531

Effective Temporary 7 May 31/2019 20190531

Revisions 1 Feb 28/2020 20200228 8 Feb 28/2020 20200228

9 May 31/2019 20190531

Contents 1 May 31/2019 20190531 10 May 31/2019 20190531

2 Jan 29/2016 20160129 11 May 31/2019 20190531

12 May 31/2019 20190531

5−20−00 ALL 1 Jun 19/2013 20130619 13 May 31/2019 20190531

14 May 31/2019 20190531

5−20−05 ALL 1 May 31/2019 20190531 15 May 31/2019 20190531

2 May 31/2019 20190531 16 May 31/2019 20190531

3 May 31/2019 20190531 17 May 31/2019 20190531

4 May 31/2019 20190531 18 May 31/2019 20190531

5 May 31/2019 20190531 19 May 31/2019 20190531

6 Jan 29/2016 20160129 20 May 31/2019 20190531

7 Jan 29/2016 20160129 21 May 31/2019 20190531

8 Jan 29/2016 20160129 22 May 31/2019 20190531

EFFECTIVITY: ALL
PART 3 Page 1
EFFECTIVE PAGES Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Section Effectivity Page Date Section Effectivity Page Date

5−21−10 ALL 23 May 31/2019 20190531 5−22−10 ALL 10 May 31/2019 20190531

24 May 31/2019 20190531 11 May 31/2019 20190531

25 May 31/2019 20190531 12 May 31/2019 20190531

26 May 31/2019 20190531 13 May 31/2019 20190531

27 May 31/2019 20190531 14 May 31/2019 20190531

28 May 31/2019 20190531 15 May 31/2019 20190531

29 May 31/2019 20190531 16 May 31/2019 20190531

30 May 31/2019 20190531 17 May 31/2019 20190531

31 May 31/2019 20190531 18 May 31/2019 20190531

32 Feb 28/2020 20200228 19 May 31/2019 20190531

33 Feb 28/2020 20200228 20 May 31/2019 20190531

34 May 31/2019 20190531 21 May 31/2019 20190531

35 May 31/2019 20190531 22 May 31/2019 20190531

36 Feb 28/2020 20200228 23 May 31/2019 20190531

37 Feb 28/2020 20200228 24 May 31/2019 20190531

38 Feb 28/2020 20200228 25 May 31/2019 20190531

39 Feb 28/2020 20200228 26 Feb 28/2020 20200228

40 Feb 28/2020 20200228 27 Feb 28/2020 20200228

41 Feb 28/2020 20200228 28 Feb 28/2020 20200228

42 Feb 28/2020 20200228 29 Feb 28/2020 20200228

43 Feb 28/2020 20200228 30 Feb 28/2020 20200228

31 Feb 28/2020 20200228

5−22−00 ALL 1 Jun 19/2013 20130619

2 Jun 19/2013 20130619 5−23−00 ALL 1 Jun 19/2013 20130619

3 May 31/2019 20190531 2 Jun 19/2013 20130619

4 May 31/2019 20190531 3 May 31/2019 20190531

5 May 31/2019 20190531 4 Jun 19/2013 20130619

6 May 31/2019 20190531 5 Jun 19/2013 20130619

7 May 31/2019 20190531 6 Jun 19/2013 20130619

8 May 31/2019 20190531

9 May 31/2019 20190531 5−23−10 Cover Jun 19/2013 20130619

10 May 31/2019 20190531

11 May 31/2019 20190531 5−23−10 ALL 1 Jun 19/2013 20130619

12 May 31/2019 20190531 2 May 31/2019 20190531

13 May 31/2019 20190531 3 Jun 19/2013 20130619

14 May 31/2019 20190531 4 May 31/2019 20190531

5 May 31/2019 20190531

5−22−10 Cover Jun 19/2013 20130619 6 May 31/2019 20190531

7 May 31/2019 20190531

5−22−10 ALL 1 Jun 19/2013 20130619 8 Jun 19/2013 20130619

2 Jun 19/2013 20130619 9 Jun 19/2013 20130619

3 Jun 19/2013 20130619 10 Jun 19/2013 20130619

4 Jun 19/2013 20130619 11 Jun 19/2013 20130619

5 Jun 19/2013 20130619 12 Jun 19/2013 20130619

6 May 31/2019 20190531 13 Jun 19/2013 20130619

7 May 31/2019 20190531 14 Jun 19/2013 20130619

8 May 31/2019 20190531 15 Jun 19/2013 20130619

9 May 31/2019 20190531 16 Jun 19/2013 20130619

EFFECTIVITY: ALL
PART 3 Page 2
EFFECTIVE PAGES Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Section Effectivity Page Date Section Effectivity Page Date

5−24−00 ALL 1 Jan 29/2016 20160129

2 Jan 29/2016 20160129

3 Jan 29/2016 20160129

4 Jan 29/2016 20160129

5−24−10 Cover Jan 29/2016 20160129

5−24−10 ALL 1 Jan 29/2016 20160129

2 Jan 29/2016 20160129

3 Jan 29/2016 20160129

4 May 31/2019 20190531

5 May 31/2019 20190531

6 May 31/2019 20190531

7 May 31/2019 20190531

8 May 31/2019 20190531

9 May 31/2019 20190531

10 May 31/2019 20190531

EFFECTIVITY: ALL
PART 3 Page 3
EFFECTIVE PAGES Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3

MAINTENANCE REVIEW BOARD REPORT

LIST OF EFFECTIVE TEMPORARY REVISIONS

NO TEMPORARY REVISIONS ARE APPLICABLE AT THIS TIME

TEMPORARY PART, SECTION ISSUE DATE INSERTED DATE REMOVED

REV. NO. AND PAGE NO. DATE INSERTED BY REMOVED BY

NOTE: This list represents only those TRs which are currently in use in Part 3 of this manual.

EFFECTIVITY: ALL
PART 3 EFFECTIVE Page 1
TEMPORARY REVISIONS Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3

MAINTENANCE REVIEW BOARD REPORT

TABLE OF CONTENTS

Subject Section Page

MAINTENANCE REVIEW BOARD (MRB) REPORT 5−20−00

Introduction 5−20−05
Scope and Purpose 1
General Program Rules 3
Program Notes 4
Description of the Maintenance Program 8
Task Intervals 9
Airplane Utilization 9
Aircraft Designation 9

AVIONICS, SYSTEMS AND POWERPLANT PROGRAM 5−21−00

General 1
List of Maintenance Significant Items (MSIs) 1
Task and Intervals Table Format 8
Task and Intervals Tables 10
Tasks and Intervals 5−21−10

STRUCTURE PROGRAM 5−22−00

General 1
Program Rules 1
List of Structural Significant Items (SSIs) 2
Task and Intervals Table Format 13
Tasks and Intervals 5−22−10

EFFECTIVITY: ALL
PART 3 Page 1
CONTENTS May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Subject Section Page

ZONAL INSPECTION PROGRAM 5−23−00

General 1
Program Rules 1
List of Zonal Identification Numbers (ZINs) 1
Task and Intervals Table Format 5
Tasks and Intervals 5−23−10

L/HIRF INSPECTION PROGRAM 5−24−00

General 1
Program Rules 1
List of L/HIRF Significant Items 1
Tasks and Intervals Table Format 3
Tasks and Intervals 5−24−10

EFFECTIVITY: ALL
PART 3 Page 2
CONTENTS Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3
SECTION 5−20−00

MAINTENANCE REVIEW BOARD REPORT

EFFECTIVITY: ALL
PART 3 Page 1
5−20−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

INTRODUCTION

1. Scope and Purpose

This Report outlines the initial minimum scheduled maintenance/inspection requirements to

be used in the development of an approved continuous maintenance program for the
airframe, engines (on−wing engines only), systems, and components for the Bombardier
Global series aircraft that follow:

Model BD−700−1A10, market designation:

− Global Express (GX) − with the Rolls−Royce BR710−A2−20 engine

− Global Express XRS (XRS) − with the Rolls−Royce BR710−A2−20 engine
− Global 6000 (GL6000) − with the Rolls−Royce BR710−A2−20 engine
− Global 6500 (GL6500) − with the Rolls−Royce BR710−D5−21 engine

Model BD−700−1A11, market designation:

− Global 5000 (GL5000) − with the Rolls−Royce BR710−A2−20 engine
− Global 5000 featuring Global Vision Flight Deck (GV5000) − with the Rolls−Royce
BR710−A2−20 engine
− Global 5500 (GL5500) − with the Rolls−Royce BR710−D5−21 engine

These MRB requirements are a basis from which each operator develops his/her own
continuous airworthiness maintenance program.

The responsible regulatory inspector shall ascertain that all of the applicable scheduled
maintenance/inspection requirements in this report are included in the operator’s initial
continuous airworthiness maintenance program.

These tasks originate from analysis performed in accordance with Maintenance Program
Development MSG−3 Revision 2 and are approved by the respective Working Groups and
Industry Steering Committee.

The MSG−3 Analysis that produced the maintenance tasks and frequencies of this document
was done on the "Green" aircraft as it leaves Bombardier and before the installation of any
systems, equipment or furnishings at aircraft completion centers.

The MSG−3 Analysis considered the following optional equipment:

− Dual Global Positioning System (GPS)
− Lightning Sensor System (LSS)
− Emergency Locator System (ELS)
− In Flight CAIMS
− SATCOM
− Data Link

EFFECTIVITY: ALL
PART 3 Page 1
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

− Office in the Sky

− Third VHF Unit
− Logo Lights
− Head−Up Display System.

The following is a list of ATA Spec 2200 assigned numbers and titles applicable to this report.
They are provided for information and reference only.

21 Air Conditioning 46 Information Management System

(GL6000, GL6500, GV5000 &
GL5500)

22 Auto Flight 49 Airborne Auxiliary Power

23 Communications 52 Doors

24 Electrical Power 53 Fuselage

25 Equipment/Furnishings 54 Nacelles/Pylons

26 Fire Protection 55 Stabilizers

27 Flight Controls 57 Wings

28 Fuel 71 Powerplant

29 Hydraulic Power 72 Engine

30 Ice and Rain Protection 73 Engine Fuel and Control

31 Indicating/Recording Systems 74 Ignition

32 Landing Gear 75 Air

33 Lights 76 Controls

34 Navigation 77 Indicating

35 Oxygen 78 Exhaust

36 Pneumatic 79 Oil

45 Central Maintenance System (GX, 80 Starting

XRS & GL5000)
Information Management System
(GL6000, GL6500, GV5000 &
GL5500)

EFFECTIVITY: ALL
PART 3 Page 2
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

2. General Program Rules

The purpose of the following general program rules is to provide standard guidelines common
to the avionics, systems, powerplant, structures and zonal maintenance programs.

A. General Visual Inspection cannot be a candidate for transfer to Zonal Working Group if
originated from Route 5 or 8.

B. Performance of the required tasks will be in accordance with the Instructions for
Continued Airworthiness (Maintenance Manual, NDT Manual etc.).

C. It is the responsibility of each operator to adjust their own maintenance program in

accordance with their national requirement.

D. An operator may elect to follow this approved maintenance program or to develop

variations with approval of the operator’s regulatory authority.

This scheduled maintenance program has been developed through careful evaluation of
airworthiness and economic aspects. Before seeking local regulatory authority approval
of changes to the tasks and intervals prescribed, an operator should carefully consider
the potential effect of each change on safety and reliability. When in doubt about the
effect of any change, the operator should seek the advice of Bombardier Business
Aircraft (BBA) Maintenance Engineering.

E. Maintenance requirements of supplemental installations made by agencies other than

the manufacturer must be established by the operator and/or that agency in accordance
with BD700 Completion Center Handbook and with the appropriate regulatory authority.

F. Inspection intervals are given in either Flight Hours (H), Months (M), Landings (L), APU
Cycles, Engine Hours (Eng H), Engine Cycles (Eng C) and also Component Hours (e.g.
APU H).

G. Operators are responsible for maintaining accurate records of all inspection intervals.

H. Revisions to the MRB Report, which introduce new tasks or change existing tasks, must
be evaluated for incorporation into an operator’s maintenance program. Incorporation
(where required) should be at the next suitable point in that program within the frequency
designated for these tasks. However, operational penalties such as withdrawing the
aircraft from service specifically to perform a new or reduced interval MRB Report task
may be avoided by following the guidelines listed in paragraphs 1. and 2. below:

1. Where a new task is introduced to the MRB Report, the task should be introduced
to the operator’s program (where required) at any convenient point, but within 6
months of the date of receipt of the MRB Report revision by the operator. Initial task
accomplishment should be within the interval designated for the task from the date
of introduction to the operator’s program.

2. Where a task interval is revised from a given value to a lower value, the revised

EFFECTIVITY: ALL
PART 3 Page 3
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

task should be introduced into the operator’s program within 6 months of the date of
receipt of the MRB Report revision by the operator. It should be completed within
the new task repeat interval or 6 months from the date of introduction to the
maintenance program by the operator whichever is greater, the exception is if this
rescheduling was to postpone the task beyond the pre−revision task
accomplishment deadline.

The guidelines contained in this Rule H do not apply to the Airworthiness Limitation
Items. Intervals for tasks resulting from Airworthiness Directives or Service Bulletins are
defined solely by the instructions contained in those documents and are not subject to
this Rule H.

I. Task interval parameters expressed in the MRB report may be converted to an individual
operator’s desired units, provided this conversion does not result in the operator
exceeding the initial requirements of the MRB report

J. Within this report, the terms "check" and "inspection" are not intended to imply a level of
skill required to accomplish a task.

K. Life−Limited parts must be retired in accordance with the limits established in the
Airworthiness Limitations section of the Instructions for Continued Airworthiness.

L. Each operator shall comply with existing rules with respect to reporting to their
airworthiness authority and to the manufacturer, events having effects on the continued
airworthiness of the aircraft.

M. Definition of MONTH (M): Equivalent to Calendar Month, i.e., all calendar controlled
intervals are to be mm/yyyy; meaning "anytime within the month it falls due", unless an
item is certified as having a due date in dd/mm/yyyy.

N. Task Intervals identified as “A” Checks or “C” Checks are no longer used on this
program.

References which make use of “A” Check or “C” Check intervals are recommended to
calculate the applicable interval as follows:
− “A” Check Intervals use 500 Hours and multiples
(A = 500 H, 2A = 1000 H, 9A = 4500 H, etc.).
− “C” Check Intervals use 15 Months and multiples
(C = 15 M, 2C = 30 M, 16C = 240 M, etc.).

3. Program Notes

The purpose of the following general program notes is to provide a single source of
information that may be referenced repeatedly throughout the Tasks and Intervals Tables in
the avionics, systems, powerplant, structures and zonal maintenance programs.

EFFECTIVITY: ALL
PART 3 Page 4
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Note 3: Task and interval may be part of the operator’s National Regulations. Whenever a
task has two intervals, one being "Note 3", the most restrictive interval applies. When a
National Regulation does not exist, the MRB Report interval shall be followed.

Note 12: Discard at the expiration date given by the manufacturer.

Note 13: Initial interval is calculated from manufacturing date of item or from the date noted
in the item certification documentation.

Note 14: The intent of this MRB report task is also covered by a CMR, refer to TLMC
section 5−10−40. An operator will have complied with both the CMR and MRB report task
requirement by completing the task with the most restrictive interval.

Note 15: Main Wheel Special Detailed Inspection Interval

Main Wheel Part Number 3−1563 series (Messier−Dowty Part No. 27350−105) and
Main Wheel Part Number 3−1599 (Messier−Dowty Part No. 27350−107)

Penetrant or Eddy Current Penetrant Inspection of the

Tire Change Number
Inspection Entire Wheel Halves

3, 6, 9, 12 X

14, 16, 18 X

21 and thereafter
X
(at every tire change)

10, 15, 20 and thereafter

X
(at every third tire change)

Note 16: Nose Wheel Special Detailed Inspection Interval

Nose Wheel Part Number 3−1560 (Messier−Dowty Part No. 27300−101)

Penetrant or Eddy Current Penetrant Inspection of the

Tire Change Number
Inspection Entire Wheel Halves

3, 6, 9, 12 X

14, 16, 18 X

21 and thereafter X
(at every tire change)

20 and thereafter
X
(at every fifth tire change)

EFFECTIVITY: ALL
PART 3 Page 5
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Note 17: Maximum Approved Lives of the LP Compressor Rotor Blade Assembly

PART NO. GIVEN LIFE (FLIGHT

IPC FIG/ITEM
CYCLES)

BRR20677 72−31−02,01−010
BRR23178
FW33925 7100**
FW34114
FW34776

FW42815
FW42806 7100***
FW42814

BRR24791
FW33513 10000***
FW33980

NOTE: * Denotes Finite Life

** Denotes life dependent upon mandatory refurbishment of the blade root dry film
lubricant coating. Refurbish at intervals of not more than 1000 flight hours ±100
flight hours or 750 flight cycles, whatever comes first, since new or since the
incorporation of the Non−Modification Service Bulletin SB−BR700−72−900266 or
since last refurbishment. To refurbish the dry film lubricant coating, refer to
Engine Maintenance Manual (M−710−2BR), Repair BRG1344, EMM TASK
72−31−02−620−806 (REPAIR−007, PB801) or Engine Manual (E−710−2BR),
Repair BRG1394, EM TASK 72−31−02−300−010 (REPAIR 10, PB901).

*** Denotes life dependent upon mandatory refurbishment of the blade root copper
nickel indium and dry film lubricant coatings. There are two fan blade on−wing
management options for the refurbishment of the root copper nickel indium and
the dry film lubricant coating.

OPTION 1:
Refurbish the root copper nickel indium and dry film lubricant coating at intervals
not more than 4000 flight hours ±400 flight hours or 3000 flight cycles − which
ever occurs first − since new or since last refurbishment of the blade root copper
nickel indium coating. To refurbish the blade root copper nickel indium and the
dry film lubricant coating, refer to Engine Manual (E−710−2BR), Repair
BRG1477, EM TASK 72−31−02−300−015. Before any reinstallation of the LP
compressor rotor blade assembly refurbish the dry film lubricant coating
according to repair BRG1344. Refer to Engine Maintenance Manual
(M−710−2BR), Repair BRG1344, EMM TASK 72−31−02−300−807 or Engine
Manual (E−710−2BR), Repair BRG1394, EM TASK 72−31−02−300−010.

EFFECTIVITY: ALL
PART 3 Page 6
5−20−05 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

OPTION 2:
Refurbish the dry film lubricant at 3000 flight hours ±300 flight hours or 1500 flight
cycles − which ever occurs first − since new or since the refurbishment of the
blade root copper nickel indium coating and at intervals not more than 1000 flight
hours ±100 flight hours or 750 flight cycles − which ever occurs first − there after.
Refurbish the blade root copper nickel indium coating at 8000 flight hours ±400
flight hours or 3000 cycles since new or since the refurbishment of the blade root
copper nickel indium coating, whatever comes first. To refurbish the dry film
lubricant coating, refer to Engine Maintenance Manual (M−710−2BR), Repair
BRG1344, EMM TASK 72−31−02−300−807 or Engine Manual (E−710−2BR),
Repair BRG1394, EM TASK 72−31−02−300−010. To refurbish the blade root
copper nickel indium and the dry film lubricant coating, refer to Engine Manual
(E−710−2BR), Repair BRG1477, EM TASK 72−31−02−300−015. Before any
reinstallation of the LP compressor rotor blade assembly refurbish the dry film
lubricant coating according to repair BRG1344. Refer to Engine Maintenance
Manual (M−710−2BR), Repair BRG1344, EMM TASK 72−31−02−620−806 or
Engine Manual (E−710−2BR), Repair BRG1394, EM TASK 72−31−02−300−010.

Note 18: Functional testing (Hydrostatic) schedules* of the oxygen cylinders with part
numbers 898JT0C50 and 806371−XXX are in accordance with Table 1 for U.S. operators or
Table 2 for Canadian operators (and based on US DOT/Canadian marking) or in accordance
with the operator’s local national regulations but limited to 60 Months maximum. When a
relevant local national regulation does not exist, the testing intervals shown in Table 2 shall
be followed.

The maximum Life Limit (Discard) of the cylinder remains as shown in Table 1 and Table 2 (at
180 Months) if the cylinder passes all inspection criteria.

Restoration (Overhaul) schedule of oxygen cylinder regulators shall be performed as follows:

− A) For cylinder with 60 Months hydrostatic test interval, overhaul of valve/regulator
assemblies should be performed at every 60 Months.
− B) For cylinder with 36 Months hydrostatic test interval, overhaul of valve/regulator
assemblies should be performed at every 72 Months.

EFFECTIVITY: ALL
PART 3 Page 7
5−20−05 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Restoration (Overhaul) schedule of the oxygen cylinder regulators are in accordance with the
two aforementioned conditions (A) or (B) or maximum of 72 Months from the date noted in the
latest certification document, as applicable.

Table 1
Hydrostatic Test Interval (when offered for transport or import in or to the United States)

AVOX Part US DOT Transport Hydrostatic Oxygen Maximum

Number Cylinder Canada Test Interval* Cylinder Cylinder Life
Marking Cylinder Regulators Limit
Marking Overhaul
Interval

898JT0C50 E 8162 SU 4237 60 Months 60 Months 180 Months

806371−XXX SP 8162 SU 4237 60 Months 60 Months 180 Months

806371−XXX SP 8162 SU 9209 60 Months 60 Months 180 Months

Table 2
Hydrostatic Test Interval (when offered for transport or import in or to Canada)

AVOX Part US DOT Transport Hydrostatic Oxygen Maximum

Number Cylinder Canada Test Interval* Cylinder Cylinder Life
Marking Cylinder Regulators Limit
Marking Overhaul
Interval

898JT0C50 E 8162 SU 4237 36 Months 72 Months 180 Months

from latest
retest

806371−XXX SP 8162 SU 4237 36 Months 72 Months 180 Months

from latest
retest

806371−XXX SP 8162 SU 9209 60 Months 60 Months 180 Months

from latest
retest

* From the date marked on the cylinder or from the date noted in the latest certification
documentation.

Reference: Zodiac AVOX Systems, SERVICE INFORMATION LETTER, SIL−35−116, Rev: 1

20080801

4. Description of the Maintenance Program

The Maintenance Program is made up of Systems, Structures and Zonal requirements.

EFFECTIVITY: ALL
PART 3 Page 8
5−20−05 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

The Systems Program gives tasks arising from the MSG−3 Systems and Powerplant/APU
analysis.

The Structures Program lists specific, directed inspections of each Structural Significant Item
developed through the MSG−3 Structures analysis of their fatigue, environment and
accidental damage characteristics.

The Zonal Program lists general visual inspections of system installations and structure on a
zone by zone basis. This program has been developed in conjunction with the other programs
to avoid duplication and to ensure complete coverage of the aircraft systems and structure.

5. Task Intervals

The maintenance program is based on tasks prescribed at specific intervals. Each task is to
be performed at the interval indicated. Future changes to these tasks and intervals are to be
coordinated with the Maintenance Review Board and based on satisfactory maintenance
program results.

6. Airplane Utilization

The MRB Report tasks and intervals are based on an average airplane utilization of 900 flight
hours, 450 flight cycles (landings) within a 12 month time period.

Operators whose airplane utilization exceeds 1750 flight hours within a 12 month period will
need to re−evaluate the recommended intervals in this report with Bombardier.

Operators whose airplane utilization is less than 250 flight hours within a 12 month period
must use the Manufacturer’s Recommended Inspection Program (MRIP) contained within the
Maintenance Planning Document (MPD).

7. Aircraft Designation

The Global series aircraft has market designations as follows:

Model Market Designation Abbreviation

BD700−1A10 Global Express GX

BD700−1A10 Global Express XRS XRS

BD700−1A10 Global 6000 GL6000

BD700−1A10 Global 6500 GL6500

BD700−1A11 Global 5000 GL5000

EFFECTIVITY: ALL
PART 3 Page 9
5−20−05 Feb 28/2020
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Model Market Designation Abbreviation

BD700−1A11 Global 5000 featuring Global Vision Flight Deck GV5000

BD700−1A11 Global 5500 GL5500

EFFECTIVITY: ALL
PART 3 Page 10
5−20−05 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

AVIONICS, SYSTEMS AND POWERPLANT PROGRAM

1. General

This section provides the basic scheduled inspection tasks and frequencies applicable to the
Avionics, Systems and Powerplant.

Maintenance Significant Items (MSI) and task references provided in this section are
presented in sequence by the Air Transport Association (ATA) assigned subject numbers.

MSG−3 (Rev. 2) logic was used to develop an on−wing scheduled maintenance program.
With the exception of life−limited parts, this process does not normally include detailed
off−wing shop maintenance procedures. Off−wing detailed procedures are controlled by
individual operators and are derived from the operator’s reliability program or are in
accordance with the manufacturer’s Instructions for Continued Airworthiness (ICA) which are
required by the Regulations.

The initial maintenance program task intervals for the items that follow have been highlighted
for validation through a data collection process such as reliability data, inspection findings and
sampling findings. When the supporting data has been reviewed, adjustments to the
scheduled maintenance program will be submitted to the ISC and MRB for consideration.
− Recirculation filter
− Ozone filter
− Main and nose landing gear
− Power plant
− Slat/Flap Control System (SFCS).

2. List of Maintenance Significant Items (MSIs)

The following table lists the MSIs identified by BBA that were subjected to MSG−3 Analysis.
The table also describes which Working Group approved the analysis and whether a task was
generated.

MSI TITLE WORKING TASK NO

GROUP TASK

212000 Distribution Systems ALL

213000 Pressurization Control Systems ALL

215000 Cooling Systems ALL

216000 Temperature Control Systems ALL

221000 Automatic Flight Control System (AFCS) Avionics ALL

EFFECTIVITY: ALL
PART 3 Page 1
5−21−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

231100 VHF Communication System Avionics ALL

231300 Satellite Communication System (SATCOM) Avionics ALL

231400 Cabin Communication System Avionics ALL

232200 Selective Calling System Avionics ALL

232300 Airborne Data Link System Avionics ALL

234000 Interphone System Avionics ALL

235100 Audio Integrating System Avionics ALL

236000 Static Dischargers System Avionics ALL

237100 Voice Recorder System Avionics ALL

238100 Radio Management System (RMS) Avionics ALL

242000 AC Generation Avionics ALL

242300 Emergency AC Power Supply Avionics ALL

243000 DC Generation Avionics ALL

245000 AC Electrical Load Distribution Avionics ALL

246000 DC Electrical Load Distribution Avionics ALL

247000 Electrical Management System Avionics ALL

251100 Flight Crew Seats Systems ALL

251300 Heated Floor Mats Systems ALL

256000 Emergency Equipment Systems ALL

256100 Emergency Locator Transmitter (ELT) Avionics ALL

257100 Avionics Compartment Systems ALL

261000 Fire Detection Propulsion ALL

262000 Fire Extinguishing Propulsion ALL

271100 Aileron Control System Systems ALL

EFFECTIVITY: ALL
PART 3 Page 2
5−21−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

271200 Aileron Trim System Systems ALL

272100 Rudder Systems ALL

272200 Rudder Trim System Systems ALL

272300 Travel Limiting Systems ALL

273100 Elevator Control System Systems ALL

273200 Stall Warning System Systems ALL

273300 Pitch Feel System Systems ALL

274000 Horizontal Stabilizer Trim System Systems ALL

275000 Flaps and Slats Systems ALL

276000 Spoilers Systems ALL

281000 Fuel Storage Propulsion ALL

281100 Fuel Storage Propulsion ALL

282100 Fuel Feed Propulsion ALL

282200 Fuel Transfer Propulsion ALL

282300 Refuel/Defuel Propulsion ALL

282400 Fuel Recirculation Propulsion ALL

284000 Indication (FMQGC) Propulsion ALL

291200 Hydraulic System No.1 and No.2 Systems ALL

291300 Hydraulic System No.3 Systems ALL

293000 Indicating Systems ALL

301100 Anti−Icing System Propulsion ALL

302100 Engine Nacelle Anti−Icing System Propulsion ALL

303100 Air Data Probes Anti−Icing Propulsion ALL

EFFECTIVITY: ALL
PART 3 Page 3
5−21−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

304100 Windshields and Windows Ice and Rain Propulsion ALL

Protection

312100 Clock System Avionics ALL

313100 Flight Data Recording System Avionics ALL

314000 Engine Indication and Crew Alerting System Avionics GX GL6000

(EICAS) XRS GL6500
GL5000 GV5000
GL5500

316100 Electronic Flight Instrument System (EFIS) Avionics GX GL6000

XRS GL6500
GL5000 GV5000
GL5500

320000 Main and Nose Gear, Doors, Extension and Systems ALL
retraction

324000 Wheels and Brakes Systems ALL

325000 Steering System Systems ALL

326000 Position and Warning Systems ALL

331000 Flight Compartment Lighting Avionics ALL

331100 Panel Integral Lighting Avionics ALL

334000 Exterior Lighting Avionics ALL

335000 Emergency Lighting Avionics ALL

341100 Air Data Computer System Avionics ALL

341200 Standby Airspeed/Altimeter System Avionics GX

XRS
GL5000

341300 Integrated Electronic Standby Instrument Avionics ALL

342000 Attitude and Direction Avionics ALL

343200 Head−Up Display System Avionics ALL

343300 Enhanced Vision System Avionics ALL

EFFECTIVITY: ALL
PART 3 Page 4
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

343400 Synthetic Vision System Avionics GL6000

GL6500
GV5000
GL5500

343500 Surface Management System Avionics GL6000

GL6500
GV5000
GL5500

344100 Weather Radar System Avionics ALL

Ground Proximity Warning System (GPWS) Avionics GX

XRS
GL5000
344200
Terrain Awareness and Warning System Avionics GL6000
(TAWS) GL6500
GV5000
GL5500

344300 Traffic Alert Collision Avoidance System Avionics ALL

(TCAS)

344400 Radio Altimeter System Avionics ALL

344500 Inertial Reference System (IRS) Avionics ALL

Lightning Sensor System Avionics GX

XRS
GL5000
344700
Lightning Detection System Avionics GL6000
GL6500
GV5000
GL5500

345100 VHF Navigation System Avionics ALL

345400 Air Traffic Control Transponder System Avionics ALL

345500 Global Positioning System (GPS) Avionics ALL

346100 Flight Management System (FMS) Avionics ALL

EFFECTIVITY: ALL
PART 3 Page 5
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

346200 Integrated Processing System Avionics GL6000

GL6500
GV5000
GL5500

351000 Crew Oxygen System Avionics ALL

361100 Bleed Air System Propulsion ALL

361200 Bleed Air Leak Detection System Propulsion ALL

Central Aircraft Information and Maintenance Avionics GX

System (CAIMS) XRS
GL5000
454500
On−board Maintenance System (OMS) Avionics GL6000
GL6500
GV5000
GL5500

461100 Information Management System (IMS) Avionics GL6000

GL6500
GV5000
GL5500

491000 APU Power Plant Propulsion ALL

492100 Engine Power System Propulsion ALL

492200 APU Gearbox Assembly Propulsion ALL

493000 APU Fuel System Propulsion ALL

494000 APU Ignition and Start Propulsion ALL

495000 APU Pneumatic System Propulsion ALL

496000 APU Electronic Control System Propulsion ALL

497000 APU Indicating Propulsion ALL

498000 APU Exhaust Propulsion ALL

499000 APU Oil System Propulsion ALL

521000 Passenger/Crew Systems ALL

EFFECTIVITY: ALL
PART 3 Page 6
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

522000 Emergency exit Systems ALL

523000 Cargo Systems ALL

524000 Service Systems ALL

527000 Door Warning Systems ALL

711000 Cowlings Propulsion ALL

717100 Engine Drains System Propulsion ALL

720300 Core Fairings Propulsion GL6500 GX

GL5500 XRS
GL6000
GL5000
GV5000

723100 Low Pressure Compressor (Fan) System Propulsion ALL

723200 Intermediate Casing Module Propulsion ALL

723300 High Pressure Compressor Module Propulsion ALL

724100 Combustion and High Pressure Turbine Propulsion ALL

Module

725100 Low Pressure Turbine Module Propulsion ALL

725600 Turbine and Rear Support Propulsion ALL

726100 Accessory Gearbox Module Propulsion ALL

727000 Bypass Duct and Engine Fairings Propulsion ALL

731000 Fuel Distribution Propulsion ALL

732000 Fuel Controlling Propulsion ALL

733000 Fuel Indicating Propulsion

740000 Ignition Propulsion ALL

752000 Cooling and Sealing Propulsion ALL

753100 HPC Airflow Control Propulsion ALL

EFFECTIVITY: ALL
PART 3 Page 7
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

MSI TITLE WORKING TASK NO

GROUP TASK

761000 Power Control Propulsion ALL

770000 Engine Indicating Propulsion ALL

781000 Exhaust System Propulsion ALL

783000 Thrust Reverser Propulsion ALL

790000 Oil System Propulsion ALL

791200 Oil Replenishment System Propulsion ALL

793000 Oil Indicating Propulsion ALL

801100 Starting Propulsion ALL

3. Task and Intervals Table Format

Detailed information is given below concerning the format of the table listing the
inspection/maintenance requirements provided on subsequent pages.

MSG−3 Route Chapter 5 Task Title Program Task Interval

Task No. Task No.

A. MSG−3 Task No. Column

This column shows all MSG−3 tasks from avionics, systems and powerplant. It also
contains the engineering source document number and the revision level as derived
from System Safety Analysis (SSA). Task numbers are as follows:

XXXXXX−YZZ where
− XXXXXX is the MSI number
− Y is 1 for life limited discard tasks
− Y is 2 for all other MSG−3 tasks
− ZZ is the task sequence identifier.

Some MSG−3 tasks requiring General Visual Inspection (GVI) may be absorbed by a
suitable Zonal inspection task. The MSG−3 tasks that are absorbed are not listed in this
section, but are listed beneath the associated Zonal MSG−3 task number in the Zonal
section, 5−23−10.

EFFECTIVITY: ALL
PART 3 Page 8
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

B. Route Column

This column shows the MSG−3 route for the task. The route specifies the effect of the
failure of the system or component. Routes are as follows:
− Route 5: Evident Safety Effects
− Route 6: Evident Operational Effects
− Route 7: Evident Economic Effects
− Route 8: Hidden Safety Effects
− Route 9: Hidden Non−Safety Effects.

Where there are several consequences of failure, the route identifications will be
separated by an oblique line (for example. (6/8).

When applicable, it contains the paragraph number of the engineering source document
referenced in the first column.

C. Chapter 5 Task No. Column

This column snows the chapter 5 task number that corresponds to the MSG−3 task
number in column 1. Chapter 5 task number are XX−XX−XX−YZZ where
− XX−XX−XX is the ATA number
− Y is 2 if the source data was MSG−3 analysis
− ZZ is number that starts at 01 for all different ATA numbers.

D. Task Title Column

This column shows the title of the task. This title includes the inspection level and a brief
description of the area or items to be inspected.

E. Program Column

This column shows the Global model variant to which the task applies, refer to section
5−20−05, paragraph 7.

F. Task Interval Column

This column shows the intervals for the task. “T” indicates inspection threshold and “R”
indicates inspection repeat interval. The interval is measured from the last time that the
task was done. The task interval is measured in flight hours (H), months (M), in landings
(L), APU cycles, engine hours (Eng H), engine cycles (Eng C) or component hours (for
example, APU H).

If two intervals are shown, for example; 750 H or 15 M, the task is next due at whichever
interval occurs first.

EFFECTIVITY: ALL
PART 3 Page 9
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

4. Task and Intervals Tables

The table in section 5−21−10 provides a list of the Avionics, Systems and Powerplant
Program tasks.

EFFECTIVITY: ALL
PART 3 Page 10
5−21−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3
SECTION 5−21−10

AVIONICS, SYSTEMS AND POWERPLANT PROGRAM

Tasks and Intervals

EFFECTIVITY: ALL
PART 3 Cover
5−21−10 Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

212000−203 8 21−21−00−201 Operational Test of the RECIRC Switch ALL 1000 H

212000−202 8 21−21−17−201 Operational Test of the Bulkhead Check Valves ALL 3000 H

EFFECTIVITY: ALL
212000−201 9 21−21−25−201 Discard the Recirculation Filters ALL 1000 H

213000−201 8/9 21−31−00−201 Operational Test of the Manual Mode ALL 2250 H

213000−204 8 21−31−00−101 ** Operational Test of the Emergency ALL 1500 H

(two stars) Depressurization Function
NOTE 14

213000−205 8 21−31−00−203 Operational Test of the Ditching Function ALL 3000 H

213000−202 9 21−31−09−101 * Functional Test of the Safety Valves ALL 3000 H

(one star)
NOTE 14

213000−203 9 21−31−11−201 Discard the Safety Valve Filters ALL 3000 H

MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

215000−201 9 21−51−09−201 Restoration of the Ozone Converter ALL 3000 H

216000−203 9 21−52−00−101 ** Operational Test of the Manual Mode of the Air ALL 1500 H
(two stars) Conditioning System
NOTE 14

5−21−10
PART 3
215000−202 9 21−53−05−101 ** Operational Test of the Ram Air Valve ALL 1500 H
(two stars)
NOTE 14

Page 1
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

212000−205 9 21−54−00−101 ** Operational Test of the Avionics Exhaust−Fan GL5000 1500 H

(two stars) Converter GV5000
NOTE 14
GL5500

EFFECTIVITY: ALL
212000−206 9 21−54−00−101 ** Operational Test of the Avionics Rack GL5000 1500 H
(two stars) Supply−Fan GV5000
NOTE 14
GL5500

212000−207 9 21−54−61−101 ** Visual Check of the Avionics Rack Ducts GL5000 1500 H
(two stars) GV5000
NOTE 14
GL5500

212000−204 9 21−54−69−201 Discard the Avionics Rack Filter GL5000 1500 H

GV5000
GL5500

216000−202 9 21−60−00−101 ** Operational Test of the Auxiliary Pressurization ALL 1500 H

(two stars) Function
NOTE 14
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 2
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

236000−201 9 23−61−01−201 Functional Test of the Static Dischargers ALL 60 M

237100−201 9 23−71−00−201 Operational Test of the Voice Recorder System ALL 3000 H

EFFECTIVITY: ALL
NOTE 3

237100−202 9 23−71−21−201 Discard of the Cockpit− Voice−Recorder (CVR) ALL NOTE 12

Underwater−Locating− Device (ULD) Battery

237100−203 9 23−71−21−202 Operational Test of the Cockpit−Voice−Recorder ALL 30 M

(CVR) Underwater− Locating Device (ULD)
NOTE 3

238100−201 8 23−81−00−201 Operational Test of the Reversion Switch Panel GL6000 30 M

(RSP) TUNE Switch, Emergency 121.5 Position GV5000
GL6500
GL5500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 3
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

242000−201 6 24−21−01−201 Detailed Inspection of the Variable Frequency ALL 1000 H

Generator (VFG) Oil Supply

EFFECTIVITY: ALL
242300−201 8 24−23−01−101 * Operational Test of the Ram Air Turbine ALL 24 M
291300−203 (one star)
NOTE 14

242300−202 8 24−23−01−102 * Functional Test of the Ram Air Turbine (RAT) ALL 24 M
(one star) Heater
NOTE 14

242000−203 9 24−25−00−201 Discard of the Variable Frequency Generator ALL 3000 H

(VFG) Oil Filter COMPONENT

242000−202 9 24−25−00−202 Visual Check of the Differential Pressure ALL 1000 H

Indicator

243000−205 6/8 24−32−01−203 Restoration of the Avionics Battery ALL 8 M

MAINTENANCE REVIEW BOARD REPORT

243000−206 6/8 24−32−09−203 Restoration of the APU Battery ALL 8 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

246000−201 8 24−64−00−201 Operational Test of the DC Override System ALL 500 H

5−21−10
PART 3
Page 4
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

251100−201 8/9 25−11−05−201 Operational Test of the Inertia Reels and the ALL 1000 H
Inertia Reels Control

EFFECTIVITY: ALL
251100−202 8 25−11−09−201 General Visual Inspection of the Safety Straps ALL 1000 H

256000−201 8 25−60−00−201 Restoration of the Crew Life Vests ALL

P/N P0723E105PWC 60 M
NOTE 13

P/N P01074−201WC 120 M

NOTE 13

256000−202 8 25−60−00−202 Restoration of the Crew Protective Breathing GX

Equipment GL5000
XRS

P/N 119003−11 120 M

MAINTENANCE REVIEW BOARD REPORT

NOTE 13
BD−700 TIME LIMITS/MAINTENANCE CHECKS

P/N 119003−21 120 M

NOTE 13

5−21−10
PART 3
Page 5
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

256000−203 8 25−60−00−203 Discard of the Crew Protective Breathing ALL

Equipment

P/N 119003 120 M

EFFECTIVITY: ALL
NOTE 13

P/N 119003−11 240 M

NOTE 13

P/N 119003−21 240 M

NOTE 13

P/N MR10042N (DP3113) 120 M

NOTE 13

P/N MR10037N 120 M

NOTE 13
MAINTENANCE REVIEW BOARD REPORT

256000−209 8 25−60−00−208 Detailed Inspection of the Crew Life Vests ALL 1000 H
BD−700 TIME LIMITS/MAINTENANCE CHECKS

256000−210 8 25−60−00−209 Detailed Inspection of the Crew Protective ALL 1000 H

Breathing Equipment (PBE)

256000−211 8 25−60−00−210 Restoration of the Crew Flashlights ALL 30 M

5−21−10
PART 3
256100−201 8 25−61−00−201 Operational Test of the Emergency Locator ALL 45 M
System
NOTE 3

Page 6
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

256100−202 8 25−61−01−201 Discard of the Emergency Locator Transmitter ALL NOTE 12

(ELT) Battery

EFFECTIVITY: ALL
257100−201 8 25−72−01−201 General Visual Inspection of the Avionics Rack GL5000 2000 H
Inboard Smoke Sealing Provisions GV5000
GL5500

257100−202 8 25−72−01−202 General Visual Inspection of the Avionics Rack GL5000 180 M
Surround Smoke Sealing Provisions GV5000
GL5500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 7
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

262000−205 8 26−10−01−201 Operational Test of the Fire−Detection−and− ALL 60 M

Extinguishing (FIDEEX) Control−Circuits, Arm
and Discharge Circuits

EFFECTIVITY: ALL
261000−201 8 26−12−00−201 Functional Test of the APU Fire Detection ALL 30 M
System

261000−202 8 26−13−00−201 Functional Test of the Main Landing Gear ALL 30 M

(MLG) Overheat−Detection System

262000−207 8 26−21−00−201 General Visual Inspection of the Single−Path ALL 3000 H

Discharge Lines

262000−201 6 26−21−01−201 Functional Test (Hydrostatic Test) of the Fire ALL 120 M
Bottle
NOTE 3
NOTE 13

262000−204 8 26−21−01−202 Functional Test of the Fire −Extinguisher ALL 120 M

MAINTENANCE REVIEW BOARD REPORT

Container Pressure−Switch
NOTE 13
BD−700 TIME LIMITS/MAINTENANCE CHECKS

262000−210 6 26−21−01−203 Functional Test of the Fire Extinguisher ALL 60 M

Contents Weight
NOTE 13

262000−202 8 26−21−05−201 Discard of the Discharge Cartridge ALL 120 M

5−21−10
PART 3
NOTE 13

262000−203 8 26−21−13−201 Operational Test of the Engine Fire−Handle ALL 3000 H

Circuit, Related Circuits and Relays

Feb 28/2020
Page 8
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

262000−206 8 26−21−13−202 Operational Test of the APU Fire−Handle ALL 3000 H

Circuit, Related Circuits and Relays

EFFECTIVITY: ALL
262000−208 8 26−21−45−201 Operational Test of the Discharge Check Valves ALL 60 M

256000−205 8 26−23−00−201 Functional Test of the Flight Compartment ALL 15 M

Extinguisher (Weight Test)
NOTE 13
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 9
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

271100−201 6 27−00−00−201 Detailed Inspection of the Aileron, Elevator and ALL 60 M

272100−201 6 Rudder Control Cables in the Forward Avionics
273100−201 6 Compartment,

EFFECTIVITY: ALL
FS202.75 to FS280.00, GX
XRS
GL6000
GL6500

FS202.75+32.00 to FS280.00+32.00 GL5000

GV5000
GL5500

271100−202 6 27−00−00−202 Detailed Inspection of the Aileron, Elevator and ALL 60 M

272100−202 6 Rudder Control Cables in the Main Avionics
273100−202 6 Compartment,

FS280.00 to FS557.00, GX
XRS
GL6000
GL6500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

FS280.00+32.00 to FS557.00 GL5000

GV5000
GL5500

271100−203 6 27−00−00−203 Detailed Inspection of the Aileron, Elevator and ALL 120 M
272100−203 6 Rudder Control Cables in the Mid− Lower
273100−203 6 Fuselage Compartment, FS557.00 to FS781.00

5−21−10
PART 3
271100−204 6/7 27−00−00−204 Detailed Inspection of the Aileron Control Cables ALL 60 M
in the Main Landing Gear (MLG) Wheel Well
and Mid Wing−to−Fuselage Fairing

Page 10
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

271100−205 6 27−00−00−205 Detailed Inspection of the Aileron Control Cables ALL 60 M

in the Flight Compartment,

FS202.75 to FS280.00, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS202.75+32.00 to FS280.00+32.00 GL5000

GV5000
GL5500

271100−206 6 27−00−00−206 Detailed Inspection of the Aileron Control Cables ALL 60 M

in the Mid and Outboard Wing Box, WS178.00
to WS536.50

271100−207 6 27−00−00−207 Detailed Inspection of the Aileron Control Cables ALL 30 M

in the Inboard Wing Trailing Edge, WS47.62 to
WS178.00
MAINTENANCE REVIEW BOARD REPORT

272100−204 6 27−00−00−208 Detailed Inspection of the Elevator and Rudder ALL 60 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

273100−204 6 Control Cables in the Aft Power Distribution/ECS

Compartment, FS781.00 to FS861.00

272100−205 6/9 27−00−00−209 Detailed Inspection of the Elevator and Rudder ALL 60 M
273100−205 6/9 Control Cables in the Aft Equipment
Compartment, FS861.00 to FS987.55

5−21−10
PART 3
272100−206 9 27−00−00−210 Detailed Inspection of the Elevator and Rudder ALL 60 M
273100−206 9 Control Cables in the Fuselage/Stabilizer
Section, FS987.55 to Rear Spar

Page 11
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

273100−207 6/7 27−00−00−211 Detailed Inspection of the Elevator Control ALL 60 M

Cables in the Vertical Stabilizer, Front Spar to
Rear Spar

EFFECTIVITY: ALL
271100−212 8/9 27−00−00−212 Operational Test of the Aileron, Elevator and ALL 1000 H
272100−210 8/9 Rudder Control Power− Control Units (PCU)
273100−211 8/9

271100−213 6 27−10−00−201 Lubrication of the Aileron Power−Control Unit ALL 60 M

(PCU) Toggle−Link Slotted Bearings

271100−208 8 27−11−05−201 Functional Test of the Roll Disconnect ALL 3000 H

Mechanism

271100−209 8 27−11−05−202 Operational Test of the Roll Disconnect ALL 1000 H

276000−201 8 Mechanism

271100−210 9 27−11−25−102 ** Functional Test of the Aileron PCU Bungee ALL 3000 H
(two stars)
MAINTENANCE REVIEW BOARD REPORT

NOTE 14
BD−700 TIME LIMITS/MAINTENANCE CHECKS

271100−213 8 27−11−35−101 ** Functional Test of the Aileron Cable Tension − ALL 30 M

(two stars) Flight Compartment Cables
NOTE 14

271100−214 8 27−11−35−102 ** Functional Test of the Aileron Cable Tension − ALL 30 M

(two stars) Fuselage Cables
NOTE 14

5−21−10
PART 3
271100−215 8 27−11−35−201 Functional Test of the Aileron Cable Tension − ALL 60 M
Wing Cables

Page 12
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

272100−213 6 27−20−00−201 Lubrication of the Rudder Power−Control Unit ALL 60 M

(PCU) Slotted Bearings

EFFECTIVITY: ALL
272100−207 5/8/9 27−21−00−201 General Visual Inspection of the Single−Rudder ALL 4500 H
Control−Path and PCU Linkage
Centering−Springs

272100−209 8 27−21−05−201 Operational Test of the Rudder Load Limiter ALL 4500 H

272100−212 8 27−21−09−101 ** Operational Test of the Rudder Power−Control ALL 3000 H

(two stars) Unit (PCU) Input Limiters
NOTE 14

272100−214 8 27−21−27−101 ** Functional Test of the Rudder Cable Tension ALL 30 M

(two stars)
NOTE 14

272300−201 8 27−23−00−201 Visual Check of the Rudder Travel−Limiting ALL 4500 H

System
MAINTENANCE REVIEW BOARD REPORT

273100−212 6 27−30−00−201 Lubrication of the Elevator Power−Control Unit ALL 60 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

(PCU) Slotted Bearings

273100−209 8 27−31−05−201 Functional Test of the Pitch Disconnect ALL 3000 H

Mechanism

273100−210 8 27−31−05−202 Operational Test of the Pitch Disconnect ALL 1000 H

5−21−10
PART 3
Mechanism

273100−208 8 27−31−17−201 Operational Test of the Elevator Power−Control ALL 3000 H

Unit (PCU) Load Limiters

Page 13
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

273100−213 8 27−31−35−201 Functional Test of the Elevator Cable Tension ALL 60 M

274000−201 6 27−41−00−201 Lubrication of the Horizontal Stabilizer Trim ALL 500 H

EFFECTIVITY: ALL
Actuator or 15 M

275000−202 6 27−50−00−201 Lubrication of the Flap Drive Torque−Tube ALL 60 M

Splines

275000−203 6 27−50−00−202 Lubrication of the Slat Drive Torque−Tube ALL 60 M

Splines

275000−204 6 27−50−00−203 Lubrication of the Flap Actuator Ballscrews and ALL 15 M

Ballnuts

275000−205 6/8 27−50−00−204 Lubrication of the Slat Actuator Ballscrews ALL 15 M

275000−206 6/8 27−50−00−205 Lubrication of the Flap Rollers ALL 1500 H

MAINTENANCE REVIEW BOARD REPORT

275000−207 6 27−50−00−206 Lubrication of the Slat Rollers ALL 60 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

275000−210 6 27−50−00−207 Lubrication of the Flap Skew Sensor No. 1 (A/C ALL 450 L
9001 and Subs),

and Flap Skew Sensors No. 2, 3 and 4 (A/C GX

9002 to 9126 and 9128 to 9178, Pre SB XRS
700−27−049),

5−21−10
PART 3
and Flap Skew Sensors No. 2, 3 and 4 (A/C GL5000
9128 to 9178, Pre SB 700−1A11−27−006)

Page 14
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

275000−209 8 27−52−57−101 * Detailed Inspection of the Flap Rollers ALL 3000 H

(one star)
NOTE 14

EFFECTIVITY: ALL
275000−208 9 27−53−09−101 ** Functional Test of the Slat Actuators and ALL 3000 H
(two stars) Interconnect Pin
NOTE 14

276000−202 8 27−61−05−201 Operational Test of the Flight−Control Unit ALL 3000 H

(FCU) Back−Up Modules
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 15
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

281000−204 8 28−10−00−201 Detailed Inspection of the Vent Tubing ALL 180 M

Vapor−Barrier Coating

EFFECTIVITY: ALL
281000−205 8 28−10−00−202 Detailed Inspection of the Center−Tank ALL 120 M
Vapor−Barrier Coating

281100−201 9 28−11−00−201 General Visual Inspection of the Wing−Tank ALL 1000 H

External Surfaces

281100−202 9 28−11−00−202 General Visual Inspection of the Wing−Tank ALL 1000 H

External Components

281000−201 9 28−11−05−201 Detailed Inspection of the Water Drain Valves ALL 60 M

281100−203 8 28−12−00−201 General Visual Inspection of the Aft Fuel−Tank GX 1000 H

Drain−Mast XRS
GL6000
GL6500
MAINTENANCE REVIEW BOARD REPORT

281100−204 8 28−12−00−202 Functional Test of the Aft Fuel−Tank GX 120 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

Compartment XRS
GL6000
GL6500

281000−203 8 28−13−00−201 Functional Test of the Fuel Vent Tubing ALL 120 M

5−21−10
PART 3
281000−206 8 28−13−00−202 Operational Test of the Vent System ALL 1000 H

281000−202 8 28−21−00−201 Functional Test of the Fuel−Feed Tubing ALL 120 M

Shrouds

Page 16
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

281000−207 8 28−21−00−202 Visual Check of the Shroud Drains ALL 1000 H

262000−209 8 28−21−29−201 Operational (Internal Leak) Test of the Engine ALL 3000 H

EFFECTIVITY: ALL
Feed Shutoff−Valves

282200−201 9 28−22−00−201 Operational Test of the Aft−Tank GX 3000 H

Manual−Transfer System XRS
GL6000
GL6500

282200−202 8 28−22−00−202 Operational Test of the Wing to Wing ALL 3000 H

Manual−Transfer System

282400−201 8 28−24−00−201 Operational Test of the Fuel Return to Tank ALL 120 M
(FRTT) Check Valves,

Post SB 700−28−034 and A/C 9111 and Subs

MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 17
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

291200−201 9 29−12−00−201 Visual Check of the No. 1 and No. 2 Hydraulic ALL 1000 H
Filter Differential−Pressure Indicators

EFFECTIVITY: ALL
291200−204 9 29−12−01−101 ** Operational Test of the Depressurization GL6500 6000 H
(two stars) Solenoid of the Engine−Driven Hydraulic Pump GL5500 or 72 M
(EDP) 1A and 2A
NOTE 14

291200−202 9 29−12−33−101 ** Operational Test of the Hydraulic Firewall ALL 1500 H

(two stars) Shutoff Valve
NOTE 14

291300−201 9 29−13−00−201 Visual Check of the No. 3 Hydraulic Filter ALL 1000 H
Differential−Pressure Indicators

291300−204 6/8 29−13−21−201 Functional Test of the No. 3 Hydraulic System ALL 1000 H
Accumulator

291300−202 8 29−14−00−201 Functional Test of the Ram Air Turbine (RAT) ALL 3000 H
Hydraulic Fluid−Heating System
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 18
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

301100−202 8 30−11−09−202 Operational Test of the WING XBLEED System ALL 2250 H

302100−201 9 30−21−05−201 General Visual Inspection of the Cowl ALL 3000 H

EFFECTIVITY: ALL
Anti−Icing−Valve Ducts

304100−201 8 30−41−00−202 Functional Test of the Windshield ALL 750 H

Rain−Repellant Layer or 12 M

301100−201 8 30−81−01−201 Operational Test of the Ice Detectors ALL 1500 H

MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 19
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

313100−203 9 31−31−00−201 Operational Test of the Flight Data Recorder ALL 4500 H
(Control Column and Rudder Pedal
Parameters),

EFFECTIVITY: ALL
(A/C 9002, 9025 and 9066 to 9089 Post SB GX
700−31−014 and A/C 9003, 9090 and Subs)

313100−204 9 31−31−00−203 Functional Test of the Flight Data Recorder ALL 90 M

(FDR) Force Sensors,

(Post SB 700−31−020), GX
XRS

(Post SB 700−31−6002), GL6000

(Post SB 700−1A11−31−001), GL5000

(Post SB 700−31−5002), GV5000

(Post SB 700−31−6503), GL6500

MAINTENANCE REVIEW BOARD REPORT

(Post SB 700−31−5503) GL5500

BD−700 TIME LIMITS/MAINTENANCE CHECKS

313100−201 9 31−31−09−201 Operational Test of the Flight−Data−Recorder ALL 30 M

(FDR) Underwater−Locating−Device (ULD)
NOTE 3

313100−202 9 31−31−09−202 Discard of the Flight−Data−Recorder (FDR) ALL NOTE 12

Underwater−Locating−Device (ULD) Battery

5−21−10
PART 3
314000−201 8 31−61−00−201 Operational Test of the EICAS Display GX 30 M
Reversion GL5000
XRS

Page 20
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

316100−201 9 31−61−00−202 Operational Test of the Primary Flight Display GX 30 M

Reversion GL5000
XRS

EFFECTIVITY: ALL
316100−202 9 31−61−00−203 Operational Test of the IRS Reversion GX 30 M
GL5000
XRS

316100−203 9 31−61−00−204 Operational Test of the ADC Reversion GX 30 M

GL5000
XRS

316100−204 6/7/9 31−61−00−205 Discard of the Adaptive Flight Display (AFD) GL6000 1000 H
Outside Fan Filters (No. 1 and 3) and Inside Fan GV5000
Filters (No. 2 and 4) GL6500
GL5500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 21
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

320000−215 8 32−10−00−201 Restoration of the Main Landing Gear ALL 240 M

320000−201 6/8 32−11−00−201 Lubrication of the Main Landing Gear (MLG) and ALL 250 H

EFFECTIVITY: ALL
Components

320000−202 6 32−11−01−201 Detailed Inspection of the Main Landing Gear ALL 750 H
(MLG) Shock Strut Extension

320000−205 6/8/9 32−12−00−201 Lubrication of the Main Landing Gear (MLG) ALL 250 H
Doors

320000−213 6 32−12−00−202 Lubrication of the Main Landing Gear (MLG) ALL 30 M

Door Actuator

320000−217 8 32−20−00−201 Restoration of the Nose Landing Gear ALL 240 M

320000−203 6/8 32−21−00−201 Lubrication of the Nose Landing Gear (NLG) and ALL 250 H
325000−201 6/8 Components
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

320000−204 6 32−21−01−201 Detailed Inspection of the Nose Landing Gear ALL 750 H
(NLG) Shock Strut Extension

320000−206 6/8 32−22−00−201 Lubrication of the Nose Landing Gear (NLG) ALL 250 H
Doors

5−21−10
PART 3
320000−207 8 32−34−00−201 Functional Test of the Landing−Gear Emergency ALL 1500 H
Extension

Page 22
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

320000−208 8 32−34−00−202 Detailed Inspection of the Landing−Gear ALL 450 L

Emergency−Extension Control Path in the Nose
Landing−Gear Wheel−Well,

EFFECTIVITY: ALL
FS202.75 to FS280.00, GX
XRS
GL6000
GL6500

FS202.75+32.00 to FS280.00+32.00 GL5000

GV5000
GL5500

320000−209 8 32−34−00−203 Detailed Inspection of the Landing−Gear ALL 60 M

Emergency−Extension Control Path in the
Forward Avionics Compartment,

FS202.75 to FS280.00, GX
XRS
GL6000
GL6500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

FS202.75+32.00 to FS280.00+32.00 GL5000

GV5000
GL5500

5−21−10
PART 3
Page 23
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

320000−210 8 32−34−00−204 Detailed Inspection of the Landing−Gear ALL 60 M

Emergency−Extension Control Path in the Main
Avionics Compartment,

EFFECTIVITY: ALL
FS280.00 to FS557.00, GX
XRS
GL6000
GL6500

FS280.00+32.00 to FS557.00 GL5000

GV5000
GL5500

320000−211 8 32−34−00−205 Detailed Inspection of the Landing−Gear ALL 120 M

Emergency−Extension Control Path in the
Mid−Lower Fuselage Compartment, FS557.00
to FS781.00

320000−212 8 32−34−00−206 Detailed Inspection of the Landing−Gear ALL 60 M

Emergency Extension Control Path in the Main
MAINTENANCE REVIEW BOARD REPORT

Landing−Gear Wheel−Well, FS719.30 to

FS781.00
BD−700 TIME LIMITS/MAINTENANCE CHECKS

324000−201 8/9 32−40−00−201 Functional Test of the Brake Accumulators ALL 500 H

324000−203 6 32−41−01−201 Special Detailed Inspection of the Main Wheels ALL NOTE 15

5−21−10
PART 3
324000−207 6 32−41−01−202 Detailed Inspection of the Main Wheels ALL Tire Change

325000−202 6 32−42−01−201 Special Detailed Inspection of the Nose Wheels ALL NOTE 16

Page 24
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

325000−203 6 32−42−01−202 Detailed Inspection of the Nose Wheels ALL Tire Change

324000−204 6 32−43−00−201 Detailed Inspection of the Brake Wear Indicators ALL 450 L

EFFECTIVITY: ALL
324000−206 8 32−43−07−201 Visual Check of the Brake−Pedal Return Spring ALL 750 H

324000−207 6 32−43−13−201 Functional Test of the Brake Disk for Drive Slot ALL 30 M
Enlargement

324000−205 8 32−43−25−201 Operational Test of the Brake Shutoff Valve ALL 750 H

326000−201 9 32−60−00−201 Visual Check of the Landing Gear Position and ALL 1000 H
Warning System
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 25
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

335000−201 8 33−50−00−201 Functional Test of the Emergency Lights ALL 15 M

Power−Supplies

EFFECTIVITY: ALL
335000−202 8 33−50−00−202 Operational Test of the Emergency Lights ALL 1000 H
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 26
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

341100−202 6 34−11−00−202 Functional Test of the Pitot−Static Systems GX 30 M

GL5000
NOTE 3
XRS

EFFECTIVITY: ALL
341100−202 7 34−11−00−202 Functional Test of the Pitot−Static Systems GL6000 30 M
GV5000
NOTE 3
GL6500
GL5500

341100−204 6 34−11−01−201 Detailed Inspection of the Pitot−Static Probes ALL 30 M

NOTE 3

341100−203 6 34−11−03−201 Servicing of the Visual Drains ALL 15 M

NOTE 3

341200−201 6 34−12−01−201 Functional Test of the Standby Airspeed/ GX 30 M

Altimeter Indicator (A/C 9002 to 9157) GL5000
NOTE 3
MAINTENANCE REVIEW BOARD REPORT

341300−201 6 34−13−00−201 Functional Test of the Integrated Electronic GL5000 30 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

Standby Instrument (A/C 9158 and subs) XRS

GL6000
GV5000
GL6500
GL5500

5−21−10
PART 3
343200−201 7 34−32−00−201 Detailed Inspection of the Electro−Optical Unit GX 1000 H
Hygrometer Sensor (if HUDS installed) GL5000
XRS

Page 27
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

346200−201 9 34−62−00−201 Operational Test of the Onboard Maintenance GL6000 60 M

System for a Digital Switching Module (DSM) GV5000
Failure Message GL6500
GL5500

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 28
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

351000−203 8 35−10−05−201 Restoration of the Crew Oxygen Mask ALL 75 M

NOTE 13

EFFECTIVITY: ALL
351000−101 5 35−11−01−201 Discard of the Oxygen Storage Cylinder ALL NOTE 13
NOTE 18

351000−201 5 35−11−01−202 Functional Test (Hydrostatic) of the Oxygen ALL NOTE 13

Storage Cylinder and the Regulator Assembly
NOTE 18

351000−202 8 35−21−01−201 Functional Test of the PASSENGER OXYGEN ALL 30 M

Control Panel
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 29
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

361100−201 6 36−11−21−201 Discard of the Pneumatic Temperature ALL 2250 H

Thermostat (THC) Filter

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 30
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

291200−203 6/7/9 45−45−00−201 Visual Check of the Engine Maintenance Alerts ALL 500 H
732000−201
733000−201
740000−202

EFFECTIVITY: ALL
753100−201
770000−201
783000−207
793000−201
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Page 31
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

491000−202 9 49−11−00−201 Visual Check of the Support Mountings ALL 30 M

491000−201 9 49−11−01−201 Visual Check of the Mounting Struts ALL 30 M

EFFECTIVITY: ALL
491000−204 9 49−15−00−201 General Visual Inspection of the Oil−Cooler Duct ALL 30 M
and Boot Assembly

491000−203 9 49−15−09−201 General Visual Inspection of the Inlet Duct and ALL 30 M
Boot Assembly

491000−205 9 49−18−00−201 General Visual Inspection of the APU Drain ALL 1000 APU H
Lines

492100−101 7 49−24−00−201 Discard the Compressor Impeller ALL 20000 APU

Cycles

492100−102 7 49−24−00−202 Discard the 1st Stage Axial Turbine Disk ALL 20000 APU
Cycles
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

492100−103 7 49−24−00−203 Discard the 2nd Stage Axial Turbine Disk ALL 20000 APU
Cycles

493000−201 8 49−30−00−204 General Visual Inspection of the APU ALL 1000 APU H
493000−202 Fuel−System Components
493000−203

5−21−10
PART 3
494000−201 7 49−42−01−201 Detailed Inspection of the Starter Motor ALL 1000 APU H

Feb 28/2020
Page 32
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

496000−201 8 49−62−00−201 Operational Test of the APU Emergency ALL 2250 APU H
Shutdown (APU SHUTDOWN SWITCH and Aft
Service Control Panel APU Shut−Off Switch)

EFFECTIVITY: ALL
497000−201 9 49−70−00−201 Visual Check of the APU Indicating System ALL 1000 H

498000−201 9 49−80−05−201 General Visual Inspection of the APU−Exhaust ALL 30 M

Tailpipe−Duct

498000−202 9 49−80−09−201 General Visual Inspection of the APU−Exhaust ALL 30 M

Tailpipe−Duct Seal

499000−201 8 49−90−00−204 General Visual Inspection of the APU ALL 1000 APU H
499000−202 Oil−System Components
499000−203

499000−204 9 49−90−29−201 Discard the APU Oil−Filter Element ALL 1500 APU H
MAINTENANCE REVIEW BOARD REPORT

499000−205 9 49−90−29−202 Discard the APU−Generator Scavenge−Oil ALL 1500 APU H

Filter−Element
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Feb 28/2020
Page 33
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

521000−203 9 52−10−00−207 Lubrication of the Passenger Door ALL 1500 H

521000−201 8/9 52−11−00−201 Functional Test of the Passenger Door ALL 2250 H

EFFECTIVITY: ALL
Mechanism

521000−202 8 52−11−00−205 Visual Check of the Passenger−Door Vent−Flap ALL 750 H

Mechanism

522000−201 8 52−21−00−201 Operational Test of the Over−Wing ALL 15 M

Emergency−Exit

522000−202 8 52−21−00−202 Functional Test of the Over−Wing ALL 30 M

Emergency−Exit EXIT PULL Sign

522000−203 6/8/9 52−21−00−203 Lubrication of the Over−Wing Emergency−Exit ALL 30 M

Door

523000−201 6 52−31−09−101 ** Detailed Inspection of the Baggage Door Seal ALL 15 M

MAINTENANCE REVIEW BOARD REPORT

(two stars)
NOTE 14
BD−700 TIME LIMITS/MAINTENANCE CHECKS

524000−201 8 52−41−00−201 Detailed Inspection of the Aft ALL 30 M

Equipment−Compartment Door Seal

5−21−10
PART 3
Page 34
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

711000−201 9 71−10−00−201 General Visual Inspection of the Cowls ALL 1500 H

711000−204 9 71−10−00−202 General Visual Inspection of the Cowl Door ALL 1500 H

EFFECTIVITY: ALL
Seals

711000−202 9 71−11−01−201 Detailed Inspection of the Inlet− Cowl ALL 3000 H

Aerodynamic Surfaces

711000−203 9 71−11−01−202 Detailed Inspection of the Inlet−Cowl Fasteners ALL 3000 H

7111001−201 and Attachment Ring

711000−206 9 71−11−01−203 General Visual Inspection of the Inlet−Cowl ALL 3000 H

Rear−Bulkhead Firewall−Material (External
Surfaces)

711000−208 8 71−13−01−201 Functional Test of the Lower−Cowl ALL 30 M

Pressure−Relief Doors
MAINTENANCE REVIEW BOARD REPORT

711000−205 9 71−14−01−201 General Visual Inspection of the Fixed Cowl ALL 3000 H
Seals
BD−700 TIME LIMITS/MAINTENANCE CHECKS

711000−207 9 71−14−01−202 Detailed Inspection of the Fixed Cowl ALL 3000 H

5−21−10
PART 3
Page 35
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

720300−201 9 72−03−00−201 General Visual Inspection of the Core Engine GL6500 3000 Eng H
Fairings GL5500

EFFECTIVITY: ALL
723100−201 6 72−30−01−201 General Visual Inspection of the ALL 2000 Eng H
LP−Compressor Case Liners

723100−202 6 72−31−02−201 Detailed Inspection of the LP Compressor ALL 1000 Eng H

Blades

723100−203 6 72−31−02−202 Detailed Inspection of the LP−Compressor ALL 1000 Eng H

Annulus Fillers

723100−206 6 72−31−02−203 Restoration of the LP Compressor Fan Blades ALL NOTE 17

723200−201 9 72−32−02−201 Detailed Inspection of the LP−Compressor ALL 1000 Eng H

Outlet Guide− Vanes

723200−202 6 72−32−02−202 Detailed Inspection of the LP−Compressor ALL 1000 Eng H

MAINTENANCE REVIEW BOARD REPORT

Engine Stator−Vanes
BD−700 TIME LIMITS/MAINTENANCE CHECKS

723100−205 8 72−34−01−201 General Visual Inspection of the ALL 3000 Eng H

LP−Compressor Case Kevlar−Wrap

723100−204 6 72−38−01−201 General Visual Inspection of the Intake Rotating ALL 2000 Eng H
Fairing

5−21−10
PART 3
Feb 28/2020
Page 36
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

724100−201 6/9 72−40−00−203 Special Detailed Inspection of the Combustion ALL

724100−205 Liner

BR710−A2−20 GX T 3000 Eng H

EFFECTIVITY: ALL
GL5000 R 1000 Eng H
NOTE: After engine shop visit for M41 restoration
XRS
(EMP work−package Level 2.5 or Level 3), the first See NOTE
GL6000
inspection is at 2000 Eng H and repeat at
GV5000
1000 Eng H.

BR710−D5−21 GL6500 T 3000 Eng H

GL5500 or 1000 Eng C
R 1000 Eng H
or 400 Eng C

724100−202 6 72−40−00−204 Special Detailed Inspection of the HP Turbine ALL

724100−206 Blades

BR710−A2−20 GX T 3000 Eng H

GL5000 R 1000 Eng H
NOTE: After engine shop visit for M41 restoration
XRS
(EMP work−package Level 2.5 or Level 3), the first See NOTE
MAINTENANCE REVIEW BOARD REPORT

GL6000
inspection is at 2000 Eng H and repeat at
GV5000
BD−700 TIME LIMITS/MAINTENANCE CHECKS

1000 Eng H.

BR710−D5−21 GL6500 T 3000 Eng H

GL5500 or 1000 Eng C
R 1000 Eng H
or 400 Eng C

5−21−10
PART 3
Feb 28/2020
Page 37
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

724100−203 6 72−40−00−205 Special Detailed Inspection of the HP Turbine ALL

724100−207 Stage−1 Nozzle Guide−Vanes

BR710−A2−20 GX T 3000 Eng H

EFFECTIVITY: ALL
GL5000 R 1000 Eng H
NOTE: After engine shop visit for M41 restoration
XRS
(EMP work−package Level 2.5 or Level 3), the first See NOTE
GL6000
inspection is at 2000 Eng H and repeat at
GV5000
1000 Eng H.

BR710−D5−21 GL6500 T 3000 Eng H

GL5500 or 1000 Eng C
R 1000 Eng H
or 400 Eng C

725100−202 8 72−50−00−204 Special Detailed Inspection of the Emergency ALL 5000 Eng H
Shutdown System

725100−203 8 72−50−00−205 Detailed Inspection of the Emergency Shutdown ALL

725600−201 System
MAINTENANCE REVIEW BOARD REPORT

BR710−A2−20 GX 5000 Eng H

BD−700 TIME LIMITS/MAINTENANCE CHECKS

GL5000
PHASE−IN: First compliance of this task
XRS
is to be done in conjunction with the next
GL6000
accomplishment of task 72−50−00−204.
GV5000

BR710−D5−21 GL6500 5000 Eng H

GL5500

5−21−10
PART 3
727000−201 6/9 72−71−00−201 General Visual Inspection of the Bypass Duct ALL 2000 Eng H

Feb 28/2020
Page 38
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

731000−202 9 73−00−00−201 General Visual Inspection of the Fuel System ALL 1000 Eng H
Components

EFFECTIVITY: ALL
731000−201 6 73−12−01−201 Discard the LP Fuel Filter ALL 1000 Eng H
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Feb 28/2020
Page 39
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

740000−201 9 74−30−01−201 Operational Test of the IGNITION Switch ALL 500 H

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Feb 28/2020
Page 40
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

781000−201 6 78−10−01−201 General Visual Inspection of the Exhaust Nozzle ALL 1000 Eng H

781000−202 6 78−10−02−201 General Visual Inspection of the Exhaust Cone ALL 1000 Eng H

EFFECTIVITY: ALL
783000−204 9 78−30−00−201 General Visual Inspection of the ALL 3000 H
Thrust−Reverser Thermal Blanket

783000−208 8 78−30−00−204 Functional Test of the Thrust Reverser ALL 4500 H

783000−202 9 78−30−00−205 General Visual Inspection of the Thrust ALL 30 M

Reverser P−Seals and Seal Depressors/Support

783000−210 9 78−33−03−201 Detailed Inspection of the Thrust Reverser Unit ALL 60 M

(TRU) Primary−Door Actuator−Rod End

783000−206 9 78−33−05−201 General Visual Inspection of the Tertiary Lock ALL 3000 H
Hook
MAINTENANCE REVIEW BOARD REPORT

783000−209 9 78−33−05−203 General Visual Inspection of the Pivoting Door ALL 3000 H
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Keeper Bar

5−21−10
PART 3
Feb 28/2020
Page 41
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

790000−201 6 79−11−00−201 General Visual Inspection of the Engine Oil Tank ALL 2000 Eng H

791200−201 6 79−11−00−202 Functional Test of the Engine Oil Tank ALL 3000 Eng H

EFFECTIVITY: ALL
726100−202 8 79−11−00−204 General Visual Inspection of the Engine Oil Tank GX 750 Eng H
(Post SB BR700−72−100455) GL5000
XRS
GL6000
GV5000
NOTE: This task applies only to gearboxes with fire
blanket installed.

790000−202 9 79−21−02−201 Discard the Pressure Filter Element ALL 1000 Eng H

723200−203 6 79−21−04−201 Detailed Inspection of the ALL 1000 Eng H

Front−Bearing−Chamber Magnetic
Chip−Detector
MAINTENANCE REVIEW BOARD REPORT

724100−204 6 79−21−04−202 Detailed Inspection of the ALL 1000 Eng H

725100−201 6 Rear−Bearing−Chamber Magnetic
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Chip−Detector

726100−201 6 79−21−04−203 Detailed Inspection of the Accessory−Gearbox ALL 1000 Eng H

Magnetic Chip−Detector

5−21−10
PART 3
Feb 28/2020
Page 42
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

801100−203 6/9 80−11−01−203 Discard the Air Turbine Starter Oil ALL 500 Eng H

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−21−10
PART 3
Feb 28/2020
Page 43
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

STRUCTURE PROGRAM

1. General

This section provides the basic scheduled inspection tasks and frequencies applicable to the
aircraft structure.

According to the analysis procedure, for each Structural Significant Item (SSI), various
inspection levels have been considered with the aim of selecting the lowest inspection level
compatible with the type of damage and the expected damage growth. Therefore, the various
inspection levels, General Visual Inspection , Detailed Inspection or Special Detailed
Inspection can be selected for one SSI. Refer to the definitions in Section 5−00−05.

The following types of damage have been considered for establishment of this program:
− Fatigue Damage (FD)
− Environmental Deterioration (ED)
− Accidental Damage (AD)

Corrosion Prevention and Control Programs (CPCP) are required to maintain the aircraft’s
resistance to corrosion. This program is a requirement as part of MSG−3, Rev. 2. The
program includes tasks such as:
− cleaning tasks (of inspected areas, drainage paths, etc.)
− tasks to dry insulation blankets
− reapply corrosion inhibiting compounds
− ensure fleet−wide corrective action when so warranted (i.e. when detected corrosion level
is above 1).

The requirement is to allow control of corrosion on aircraft to Corrosion Level 1 or better. This
program is based on the environmental deterioration analysis. According to Transport
Canada, the environmental deterioration analysis fully meets the requirements of the CPCP.

The internal fuselage structure inspection tasks (between FS202.75 and FS861.00, above
floor) in section 5−22−10 have been highlighted for validation through a data collection
process such as reliability data, inspection findings and sampling findings. Once the
supporting data has been reviewed, adjustments to the scheduled maintenance program will
be submitted to the ISC and MRB for consideration.

The zonal program (section 5−23−10) also has tasks which will be brought in line with the
structure tasks, to avoid interior removal at different intervals.

2. Program Rules

The purpose of the following program rules is to provide standard guidelines to the structures
inspection/maintenance program.

EFFECTIVITY: ALL
PART 3 Page 1
5−22−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

A. The threshold is the time when the first inspection is due. It is indicated with a "T" in the
Task Interval column.

B. For repeat inspection, the interval commences at the time of the last inspection
performed. It is indicated with a "R" in the Task Interval column.

C. Normal cleaning procedures are to be used prior to Detailed Inspections and specified
cleaning procedures prior to Special Detailed Inspections. Sealant and corrosion
protection finishes should be removed only when specified.

D. Operators shall report all structural findings to the manufacturer.

E. Airworthiness Limitation Instructions:

Additional structural tasks for Principal Structural Elements (PSE) and Safe−life structure
are listed in section 5−10−30, Airworthiness Limitation Items (ALI), of this manual. ALI
tasks refer to mandatory fixed intervals resulting from fatigue and damage tolerance
analysis performed by Bombardier Structural Engineering in coordination with Transport
Canada Engineering. The operator must consider both report (MRB/ALI) requirements
when developing and maintaining their maintenance programs and shall not change the
requirements without the approval of their regulatory authority (Engineering/Certification
disciplines).

F. Unless otherwise noted, it is understood that component/installations/liners/sealants are

not required to be removed to perform the inspection.

3. List of Structural Significant Items (SSIs)

This section contains a list of all the SSIs sorted in ATA sequence by SSI number.

SSI No. SSI DESCRIPTION TASK

2740001 Horizontal Stabilizer Trim Actuator ALL

3210001 Main Landing Gear ALL

3220001 Nose Landing Gear ALL

3220002 Nose Landing Gear Forward Door − Hinges and Actuator Fitting ALL

5210001 Passenger Door − Outer Skin ALL

5210002 Passenger Door − Internal Skin/Stiffeners and Mounting Side Frames ALL

5210004 Passenger Door − Stops and Abutments ALL

5210007 Passenger Door − Handrail Attachment to Fuselage ALL

EFFECTIVITY: ALL
PART 3 Page 2
5−22−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5221001 Overwing Emergency Exit Door − External Skin ALL

5221002 Overwing Emergency Exit Door − Latch Fittings and Door Stop Fittings ALL

5221003 Overwing Emergency Exit Door − Internal Structure and Skin ALL

5230001 Baggage Door − External Skin ALL

5230002 Baggage Door Surround Angles and Stops ALL

5230003 Baggage Door External Fittings and Internal Structure ALL

Frame FS169.00 − Forward Side GX

XRS
GL6000
GL6500
5310001
Frame FS169.00+32.00 − Forward Side GL5000
GV5000
GL5500

Internal Structure from FS169.00 to FS202.75 Above Floor GX

XRS
GL6000
GL6500
5310002
Internal Structure from FS169.00+32.00 to FS202.75+32.00 Above GL5000
Floor GV5000
GL5500

Internal Structure from FS169.00 to FS202.75 Below Floor GX

XRS
GL6000
GL6500
5310003
Internal Structure from FS169.00+32.00 to FS202.75+32.00 Below GL5000
Floor GV5000
GL5500

5310004 Flight Compartment Roof − Internal Structure (Including Frames, ALL

Stringers and Skin)

EFFECTIVITY: ALL
PART 3 Page 3
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

Internal Structure from FS202.75 to FS280.00 Above Floor WL79.50 GX

to WL110.00 XRS
GL6000
GL6500
5310005
Internal Structure from FS202.75+32.00 to FS280.00+32.00 Above GL5000
Floor WL79.50 to WL110.00 GV5000
GL5500

Bulkhead FS280.00 − Forward Side Above Floor WL79.50 GX

XRS
GL6000
GL6500
5310006
Bulkhead FS280.00+32.00 − Forward Side Above Floor WL79.50 GL5000
GV5000
GL5500

Floor Structure from FS202.75 to FS280.00 − Accessed from Below GX

Floor XRS
GL6000
GL6500
5310007
Floor Structure from FS202.75+32.00 to FS280.00+32.00 − Accessed GL5000
from Below Floor GV5000
GL5500

External Skin from FS169.00 to FS280.00 (Including Pressurized GX

Access Panels) XRS
GL6000
GL6500
5310008
External Skin from FS169.00+32.00 to FS280.00+32.00 (Including GL5000
Pressurized Access Panels) GV5000
GL5500

Internal and External Surround Structure of Forward Jacking Point − GX

FS278.00 XRS
GL6000
GL6500
5310009
Internal and External Surround Structure of Forward Jacking Point − GL5000
FS278.00+32.00 GV5000
GL5500

5310010 Windshield and Side Window Surround Structure ALL

5310011 NLG Wheel Well Structure − Accessed from Wheel Well ALL

EFFECTIVITY: ALL
PART 3 Page 4
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

Internal Structure from FS202.75 to FS280.00 Below Floor GX

XRS
GL6000
GL6500
5310012
Internal Structure from FS202.75+32.00 to FS280.00+32.00 Below GL5000
Floor GV5000
GL5500

Internal Skin Panels, Frames and Stringers in Upper Fuselage from GX

Floor to Top Centerline FS381.00 to FS557.00 LH and RH XRS
GL6000
GL6500
5320001
Internal Skin Panels, Frames and Stringers in Upper Fuselage from GL5000
Floor to Top Centerline FS381.00+32.00 to FS557.00 LH and RH GV5000
GL5500

Internal Skin Panels, Frames and Stringers in Lower Fuselage from GX

Floor to Bottom Centerline FS381.00 to FS557.00 LH and RH XRS
GL6000
GL6500
5320002
Internal Skin Panels, Frames and Stringers in Lower Fuselage from GL5000
Floor to Bottom Centerline FS381.00+32.00 to FS557.00 LH and RH GV5000
GL5500

External Top Skin Panel from FS381.00 to FS557.00 and from GX

Stringer 6L to 6R XRS
GL6000
GL6500
5320003
External Top Skin Panel from FS381.00+32.00 to FS557.00 and from GL5000
Stringer 6L to 6R GV5000
GL5500

External Side and Lower Skin Panels from FS381.00 to FS557.00 and GX
from Stringer 6L to 6R XRS
GL6000
GL6500
5320004
External Side and Lower Skin Panels from FS381.00+32.00 to GL5000
FS557.00 and from Stringer 6L to 6R GV5000
GL5500

5320005 External Keel Beam − FS501.00 to FS574.00 and BL4.6L to BL4.6R ALL

5320006 External Overwing Longeron − FS525.00 to FS574.00 and Stringer ALL

19L and 19R

EFFECTIVITY: ALL
PART 3 Page 5
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5320007 Pressure Bulkhead FS557.00 − Forward Face Below Floor Level ALL

5320008 Pressure Bulkhead FS557.00 − Aft Face Below Floor Level (including ALL
Bulkhead Web and Frame Cap Members)

5320009 Pressure Floor Skin Panel, FS557.00 to FS574.50 and BL4.6L to ALL
BL4.6R (Top Surface)

5320010 Pressure Floor Skin Panel, FS557.00 to FS574.50 and BL4.6L to ALL
BL4.6R (Lower Surface)

Floor Support Structure from FS381.00 to FS557.00 (including Floor GX

Beams, Struts, Floor Sills and Seat Rails) XRS
GL6000
GL6500
5320011
Floor Support Structure from FS381.00+32.00 to FS557.00 (including GL5000
Floor Beams, Struts, Floor Sills and Seat Rails) GV5000
GL5500

Internal Skin Panels, Frames and Stringers in Upper Fuselage from GX

Floor to Top Centerline − FS281.00 to FS381.00 XRS
GL6000
GL6500
5320012
Internal Skin Panels, Frames and Stringers in Upper Fuselage from GL5000
Floor to Top Centerline − FS281.00+32.00 to FS381.00+32.00 GV5000
GL5500

Internal Skin Panels, Frames and Stringers in Lower Fuselage from GX

Floor to Top Centerline − FS281.00 to FS381.00 XRS
GL6000
GL6500
5320013
Internal Skin Panels, Frames and Stringers in Lower Fuselage from GL5000
Floor to Top Centerline − FS281.00+32.00 to FS381.00+32.00 GV5000
GL5500

External Top Skin Panel − FS281.00 to FS381.00 and Stringer 2L to GX

2R XRS
GL6000
GL6500
5320014
External Top Skin Panel − FS281.00+32.00 to FS381.00+32.00 and GL5000
Stringer 2L to 2R GV5000
GL5500

EFFECTIVITY: ALL
PART 3 Page 6
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

External Left Side and Lower Skin Panel − FS281.00 to FS381.00 and GX
Stringer 2L to 25L XRS
GL6000
GL6500
5320015
External Left Side and Lower Skin Panel − FS281.00+32.00 to GL5000
FS381.00+32.00 and Stringer 2L to 25L GV5000
GL5500

External Right Side and Lower Skin Panel − FS281.00 to FS381.00 GX

and Stringer 2R to 25R XRS
GL6000
GL6500
5320016
External Right Side and Lower Skin Panel − FS281.00+32.00 to GL5000
FS381.00+32.00 and Stringer 2R to 25R GV5000
GL5500

Floor Support Structure from FS281.00 to FS381.00 (including Floor GX

Beams, Struts, Floor Sills and Seat Rails) XRS
GL6000
GL6500
5320017
Floor Support Structure from FS281.00+32.00 to FS381.00+32.00 GL5000
(including Floor Beams, Struts, Floor Sills and Seat Rails) GV5000
GL5500

Floor Structure in Way of Passenger Door Step FS310.00 to FS347.00 GX

XRS
GL6000
GL6500
5320018
Floor Structure in Way of Passenger Door Step FS310.00+32.00 to GL5000
FS347.00+32.00 GV5000
GL5500

5320019 Sills, Frames and Skin Around Passenger Door Cutout ALL

5320020 Fittings and Hinges on Fuselage for Passenger Door ALL

5320021 Skin Assembly at Window Surround ALL

EFFECTIVITY: ALL
PART 3 Page 7
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

Fuselage Longitudinal Joints FS281.00 to FS381.00 GX

XRS
GL6000
GL6500
5320022
Fuselage Longitudinal Joints FS281.00+32.00 to FS381.00+32.00 GL5000
GV5000
GL5500

Fuselage Longitudinal Joints FS381.00 to FS557.00 GX

XRS
GL6000
GL6500
5320023
Fuselage Longitudinal Joints FS381.00+32.00 to FS557.00 GL5000
GV5000
GL5500

Fuselage Barrel Joint FS381.00 GX

XRS
GL6000
GL6500
5320024
Fuselage Barrel Joint FS381.00+32.00 GL5000
GV5000
GL5500

5320025 Fuselage Barrel Joint FS557.00 ALL

Sills, Frame and Skin Around Service Door FS295.00 to FS310.00 and GX
Stringer 21R to 23R XRS
GL6000
GL6500
5320026
Sills, Frame and Skin Around Service Door FS295.00+32.00 to GL5000
FS310.00+32.00 and Stringer 21R to 23R GV5000
GL5500

5330001 Front Spar Frame ALL

5330002 Rear Spar Frame ALL

5330003 Skin Panels − External FS557.00 to FS797.60 ALL

5330004 Sills, Frames and Skin Around Overwing Emergency Door Cutout ALL

5330005 Overwing Emergency Exit Door Cutout − Latch Fittings, Hinge Fittings ALL
and Door Stop Fittings

EFFECTIVITY: ALL
PART 3 Page 8
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5330006 Skin Panels Around Window Cutouts − External FS557.00 to ALL

FS797.60

5330007 Frame, Stringers, Side Beams and Skin Panels − Internal FS557.00 to ALL
FS797.60

5330008 Pressure Floor Panel − Upper Side FS719.30 to FS781.00 ALL

5330009 Pressure Floor Panel − Lower Side FS719.30 to FS781.00 ALL

5330010 Pressure Floor Beams − FS713.10 to FS781.00, BL0.0, BL9, BL19, ALL
BL27 and BL35

5330012 MLG Uplock Fittings ALL

5330013 Aft Keel Beam − FS719.30 to FS781.00 ALL

5330014 Pressure Bulkheads FS719.30 Aft Face and FS781.00 Forward Face ALL

5340001 Exterior Fuselage Skin, FS797.00 to Vertical Stabilizer Rear Spar ALL
Datum (excluding Skin Upper Wing−to−Fuselage Fairing)

5340002 Exterior Skin Around Baggage Door Cutout ALL

5340003 Exterior Skin Underneath Wing−to−Fuselage Fairing − FS781.00 to ALL

FS945.00. Aft Keel Beam Structure, FS781.00 to FS885.00

5340004 Baggage Door Stops on the Fuselage ALL

5340005 Baggage Door Cutout Interior Surround Structure Forward of Pressure ALL
Bulkhead

5340006 Interior Fuselage Shell Structure Above Floor in Baggage ALL

Compartment − FS797.00 to FS861.00, Stringer 0 to 18L/R

5340007 Interior Fuselage Shell Structure Below Floor − FS781.00 to ALL

FS861.00, Floor Structure in Baggage Compartment, Rear Pressure
Bulkhead Forward Face Below Floor

5340008 Rear Pressure Bulkhead Forward Face Above Floor ALL

5340009 Rear Pressure Bulkhead Web Aft Face including Vertical Stiffeners ALL
and Horizontal Beam

5340010 Baggage Door Sills and Stops Backup Structure Aft of Pressure ALL
Bulkhead

5340011 Auxiliary Fuel Tank Support Structure ALL

EFFECTIVITY: ALL
PART 3 Page 9
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5340012 Aft Equipment Bay Door Hinges and Door Cutout Surround Structure ALL

5340013 Interior Fuselage Shell Structure in Aft Equipment Bay and Barrel ALL
Section − FS861.00 to Vertical Stabilizer Rear Spar Frame

5340014 Interior Fuselage Shell Structure in Aft Equipment Bay − FS861.00 to ALL
FS893.50, WL80.25 to WL137.00

5340015 Forward Engine Mount Frame Assembly (including Engine Mount to ALL
Frame Joint)

5340016 Inner Flap Inboard Track Support Structure ALL

5350001 Aft Engine Mount Frame Assembly (including Engine Mount to Frame ALL
Joint)

5350002 Mid Spar Frame (including Mid Spar to Frame Joint) ALL

5350003 Rear Spar Frame (including Rear Spar to Frame Joint) ALL

5350004 APU Mount Strut Attach Fittings on Rear Spar Frame and Backup ALL
Fittings

5450001 Exterior Skins of the Pylon Center Box ALL

5450002 Pylon Drag Angles ALL

5450003 Pylon Center Box Internal Structure ALL

5510001 Screw−Jack Fitting, Pivot Fitting, External Buttstraps, Rear Spar Joint ALL
Fitting, Upper/Lower External Support Fittings

5510002 Center Box Ribs, Bracing Rib, Forward/Rear Internal Fittings ALL

5510003 Horizontal Stabilizer − External Hinge Fittings, Support Fittings and ALL
Internal Backup Fittings

5510004 Horizontal Stabilizer − Upper and Lower Skins (Composite) − External ALL

5510005 Horizontal Stabilizer − Spars (External and Internal), Ribs and Internal ALL
Skin Surfaces

5520001 Elevator − Upper and Lower Skins (Composite) − External ALL

5520002 Elevator External Hinge Fittings and Internal Backup Fittings ALL

5520003 Elevator − Spars (External and Internal) Ribs and Internal Skin ALL
Surfaces

EFFECTIVITY: ALL
PART 3 Page 10
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5530001 Exterior Vertical Stabilizer Skins ALL

5530002 Vertical Stabilizer Drag Angles ALL

5530003 Vertical Stabilizer Front Spar Forward and Aft Face from Fuselage to ALL
Tip

5530004 Front Spar to Fuselage Skin Joint ALL

5530005 Vertical Stabilizer Rear Spar Forward and Aft Face from Fuselage to ALL
Tip and Rudder Hinge Fittings on Rear Spar

5530006 Tip Rib, Trim Actuator Support/Backup Fittings, Pivot Fitting and ALL
Support Structure, and Lateral Steady

5530007 Interior Skins, Ribs Stringers and Mid Spar ALL

5530008 Wishbone Fittings and their Attachments ALL

5530009 Pitch Trim Actuator Lower Attachment Pins ALL

5530010 Rudder Hinge Pins ALL

5540001 Rudder Skins − External ALL

5540002 Rudder Hinge Fittings and Internal Backup Fittings ALL

5540003 Rudder − Spars (External and Internal), Ribs and Internal Skin ALL
Surfaces

5610001 Windshield and Side Window ALL

5711001 Center Wing Front Spar − Forward Side, FS574.50 Between LBL47.6 ALL
and RBL47.6

5711002 Center Wing Front Spar − Aft Side, FS574.50 Between LBL47.6 and ALL
RBL47.6

5711003 Center Wing Rear Spar − Forward Side, FS719.00 Between LBL47.6 ALL
and RBL47.6

5711004 Center Wing Rear Spar − Aft Side, FS719.00 Between LBL47.6 and ALL
RBL47.6

5711005 Center Wing Upper Panel − Upper Between FS574.50 and FS719.00, ALL
Between LBL47.6 and RBL47.6

EFFECTIVITY: ALL
PART 3 Page 11
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5711006 Center Wing Lower Panel − Lower Between FS574.50 and FS719.00, ALL
Between LBL47.6 and RBL47.6

5711007 Center Wing Upper Panel − Lower Panel and Ribs − Internal Between ALL
FS574.50 and FS719.00, Between LBL47.6 and RBL47.6

5711008 Root Rib Outboard Side − LBL47.6 and RBL47.6 Between FS574.50 ALL
and FS719.00

5711009 MLG Side Stay Fitting ALL

5720001 Wing Front Spar − Forward Side ALL

5720002 Wing Front Spar − Aft Side BL47.61 to CWS537.4 ALL

5720003 Wing Rear Spar − Forward Side BL47.61 to CWS537.4 ALL

5720004 Wing Rear Spar − Aft Side ALL

5720005 Wing Upper Panel − External ALL

5720006 Wing Lower Panel − External ALL

5720007 Wing Upper Panel, Lower Panel, Stringers and Ribs − Internal ALL
BL47.61 to CWS537.4

5720008 Wing Tip Dry Bay − Internal CWS537.4 to WS536.50 ALL

5720009 Auxiliary Spar Assembly ALL

5720010 MLG Trunnion Fitting ALL

5720012 No. 1 Slat Support Fittings ALL

5720013 No. 2, 3, 4 Slat Support Fittings ALL

5720016 Flap Support Fitting ALL

5720020 Ground Spoiler Support Fittings ALL

5720021 Multifunction Spoiler Support Fittings ALL

5720023 Aileron Support Fitting ALL

5730001 Winglet Internal Structure ALL

5730002 Winglet Attachment Fittings ALL

EFFECTIVITY: ALL
PART 3 Page 12
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

SSI No. SSI DESCRIPTION TASK

5730003 Winglet External Structure ALL

5740001 No. 1 Slat Body ALL

5740002 No. 2, 3, 4 Slat Body ALL

5750001 Inboard, Mid, Outboard Flaps − Wing Trailing Edge Between BL47.6 ALL
and WS404.00

5760001 Aileron − Wing Trailing Edge Between Aileron Station 477.3 ALL
WS544.80

5770001 Ground Spoiler − Wing Trailing Edge Between BL47.6 and WS178.00 ALL

5770002 Multifunction Spoiler − Wing Trailing Edge Between WS178.00 and ALL
WS404.00

7110001 Upper Fan Cowl Doors ALL

7111001 Inlet Cowl Attachment Ring ALL

7120001 Engine Front and Rear Mounts ALL

7830001 Thrust Reverser Upper Pivot Door ALL

4. Task and Intervals Table Format

Data about the tables used in section 5−22−10 are given below:

MSG−3 Route Chapter 5 Task Title Program Task Interval

Task No. Task No.

A. MSG−3 Task No. Column

This column lists all MSG−3 task numbers from the structures analysis. It also includes
tasks at the request of the MRB.

The task numbers are of the form XXXXXXX−YZZ for structures tasks, where
− XXXXXXX is the SSI number
− Y = 2 for MSG−3 items
− ZZ is the task sequence identifier.

EFFECTIVITY: ALL
PART 3 Page 13
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Some MSG−3 tasks requiring General Visual Inspection (GVI) may be absorbed by a
suitable Zonal inspection task. Whenever an MSG−3 task is absorbed by a Zonal
inspection task, the absorbing Zonal task is listed below it in parenthesis. Refer to the
absorbing Zonal task in the Zonal section, since this is the task which requires
accomplishment. The format for Structures tasks and Zonal tasks is defined in 5−21−00
and 5−23−00, respectively.

B. Route Column

This column shows the type of damage analysis that was used to make the MSG−3 task
shown in column 1. This column also shows tasks where the application of corrosion
inhibiting compound (CIC) is necessary. The letters used in this column are as follows:
− AD: Accidental Damage
− ED: Environmental Deterioration
− CPCP: Application of CIC is necessary

C. Chapter 5 Task No. Column

This column shows the chapter 5 task number that corresponds to the MSG−3 task
number in column 1. Chapter 5 task numbers are XX−XX−XX−YZZ where
− XX−XX−XX is the ATA number
− Y = 2 shows that the source data was the MRB report
− ZZ is the number that starts at 01 for all different ATA numbers.

D. Task Title Column

This column shows the title of the task. This title includes the inspection level and a brief
description of the area or items to be inspected.

E. Program Column

This column shows the Global model variant to which the task applies.

F. Task Interval Column

This column shows the intervals for the task (T − Threshold, R − Repeat). The interval is
measured from the last time that the task was done. The task interval is measured in
flight hours (H), months (M), or landings (L).

EFFECTIVITY: ALL
PART 3 Page 14
5−22−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3
SECTION 5−22−10

STRUCTURE PROGRAM
Tasks and Intervals

EFFECTIVITY: ALL
PART 3 Cover
5−22−10 Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

2740001−201 ED 27−41−00−202 Detailed Inspection of the Horizontal Stabilizer ALL T 60 M

Trim Actuator R 60 M

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Page 1
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

3210001−202 ED−CPCP 32−10−00−202 Detailed Inspection of the Main Landing Gear ALL T 120 M
(MLG) Pintle Pin R 120 M

EFFECTIVITY: ALL
3210001−204 ED−CPCP 32−10−00−203 Detailed Inspection of the Main Landing Gear ALL T 120 M
(MLG) (Attachment Pins and Lugs) R 120 M

3210001−209 ED−CPCP 32−10−00−204 Special Detailed Inspection of the Main Landing ALL T 240 M
Gear (MLG) Shock−Strut Assembly (Internal) R 120 M

3210001−203 ED 32−10−00−206 Special Detailed Inspection of the Main Landing ALL T 240 M
Gear (MLG) Pintle Pins R 120 M

3210001−205 ED 32−10−00−207 Special Detailed Inspection of the Main Landing ALL T 240 M
Gear (MLG) (Attachment Pins and Lugs) R 120 M

3210001−206 ED−CPCP 32−10−00−208 Detailed Inspection of the Trailing Arm/Axle ALL T 120 M
Assembly R 120 M
MAINTENANCE REVIEW BOARD REPORT

3210001−207 ED 32−10−00−209 Special Detailed Inspection of the Trailing ALL T 240 M

Arm/Axle Assembly R 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

3210001−208 ED−CPCP 32−10−00−210 Detailed Inspection of the Shock Strut Assembly ALL T 120 M
(Internal) R 120 M

3210001−210 ED 32−10−00−211 Detailed Inspection of the Side Brace Actuator ALL T 120 M
(Internal) R 120 M

5−22−10
PART 3
3210001−211 ED 32−10−00−212 Special Detailed Inspection of the Side Brace ALL T 240 M
Actuator (Internal) R 120 M

Page 2
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

3210001−212 ED−CPCP 32−10−00−213 Detailed Inspection of the Retraction Actuator ALL T 120 M
(Internal) R 120 M

EFFECTIVITY: ALL
3210001−213 ED 32−10−00−214 Special Detailed Inspection of the Retraction ALL T 240 M
Actuator (Internal) R 120 M

3220001−202 ED−CPCP 32−20−00−204 Detailed Inspection of the Nose Landing Gear ALL T 120 M
(NLG) Pintle Pins R 120 M

3220001−203 ED 32−20−00−205 Special Detailed Inspection of the Nose Landing ALL T 240 M
Gear (NLG) Pintle Pins R 120 M

3220001−204 ED−CPCP 32−20−00−206 Detailed Inspection of the Nose Landing Gear ALL T 120 M
(NLG) (Attachment Pins and Lugs) R 120 M

3220001−205 ED 32−20−00−207 Special Detailed Inspection of the Nose Landing ALL T 240 M
Gear (NLG) (Attachment Pins and Lugs) R 120 M
MAINTENANCE REVIEW BOARD REPORT

3220001−206 ED−CPCP 32−20−00−208 Detailed Inspection of the Sliding Tube ALL T 120 M
(Internal), Steering and Axle Assembly R 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

3220001−207 ED 32−20−00−209 Special Detailed Inspection of the Sliding Tube ALL T 240 M
(Internal), Steering and Axle Assembly R 120 M

3220001−208 ED 32−20−00−210 Detailed Inspection of the Nose Landing Gear ALL T 120 M
Retraction Actuator (Internal) R 120 M

5−22−10
PART 3
3220001−209 ED 32−20−00−211 Special Detailed Inspection of the Nose Landing ALL T 240 M
Gear Retraction Actuator (Internal) R 120 M

Page 3
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

3220002−201 ED 32−22−00−202 Detailed Inspection of the Nose−Gear−Door ALL T 120 M

Hinges and Actuator Attachment Fitting R 120 M

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Page 4
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5210002−201 ED−CPCP 52−11−00−202 Detailed Inspection of the Internal Structure of ALL T 120 M
the Passenger Door R 120 M

EFFECTIVITY: ALL
5210004−201 ED 52−11−00−203 Detailed Inspection of the Stops and Abutments ALL T 120 M
of the Passenger Door R 120 M

5210007−201 ED 52−11−21−201 Detailed Inspection of the Handrails Attachment ALL T 120 M

to the Fuselage R 120 M

5221002−201 ED−AD 52−21−00−204 Detailed Inspection of the Latch Fittings and ALL T 60 M
Door Stop Fittings of the Over− Wing R 60 M
Emergency Exit

5221003−201 ED−CPCP 52−21−00−205 Detailed Inspection of the Internal Skin and ALL T 120 M
Structure of the Over−Wing Emergency Exit R 120 M

5230002−201 ED−CPCP 52−30−00−201 Detailed Inspection of the Surround Angles and ALL T 120 M
Stop Fittings of the Baggage Door R 120 M
MAINTENANCE REVIEW BOARD REPORT

5230003−201 ED−CPCP 52−30−00−202 Detailed Inspection of the Internal Support ALL T 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Structure of the Baggage Door R 120 M

5−22−10
PART 3
Page 5
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310002−201 ED 53−10−00−201 Detailed Inspection of the Internal Structure, ALL T 120 M

R 60 M
FS169.00 to FS202.75, Above Floor, GX
XRS

EFFECTIVITY: ALL
GL6000
GL6500

FS169.00+32.00 to FS202.75+32.00, Above GL5000

Floor GV5000
GL5500

5310003−201 ED 53−10−00−202 Detailed Inspection of the Internal Structure, ALL T 120 M

R 60 M
FS169.00 to FS202.75, Below Floor, GX
XRS
GL6000
GL6500

FS169.00+32.00 to FS202.75+32.00, Below GL5000

Floor GV5000
GL5500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5310004−201 ED−CPCP 53−10−00−203 Detailed Inspection of the Internal Forward ALL T 180 M
5310005−201 Fuselage Skin/Structure and FS280.00 R 60 M
5310006−201 Bulkhead Forward Face,

FS202.75 to FS280.00, Above WL79.50, GX

XRS
GL6000

5−22−10
PART 3
GL6500

FS202.75 to FS280.00+32.00, Above WL79.50 GL5000

GV5000
GL5500

Page 6
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310005−202 ED 53−10−00−205 Detailed Inspection of the Pilot and Copilot Seat ALL T 120 M
Tracks R 60 M

EFFECTIVITY: ALL
5310007−201 ED−CPCP 53−10−00−207 Detailed Inspection of the Floor Structure, ALL T 120 M
R 120 M
FS202.75 to FS280.00, GX
XRS
GL6000
GL6500

FS202.75+32.00 to FS280.00+32.00 GL5000

GV5000
GL5500

5310009−201 ED−CPCP 53−10−00−208 Detailed Inspection of the Forward Jacking ALL T 120 M
Point, R 120 M

FS278.00, GX
XRS
GL6000
MAINTENANCE REVIEW BOARD REPORT

GL6500
BD−700 TIME LIMITS/MAINTENANCE CHECKS

FS278.00+32.00 GL5000
GV5000
GL5500

5310010−201 ED 53−10−00−209 Detailed Inspection of the Windshield and ALL T 180 M

Side−Window Surround Structure and Retainers R 120 M

5−22−10
PART 3
5310011−201 ED 53−10−00−210 Detailed Inspection of the Nose Landing Gear ALL T 60 M
(NLG) Wheel Well Structure R 60 M

Page 7
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310012−201 ED−CPCP 53−10−00−211 Detailed Inspection of the Internal Structure, ALL T 120 M
R 120 M
FS202.75 to FS280.00, Below Floor, GX
XRS

EFFECTIVITY: ALL
GL6000
GL6500

FS202.75+32.00 to FS280.00+32.00, Below GL5000

Floor GV5000
GL5500

5320001−201 ED−CPCP 53−20−00−201 Detailed Inspection of the Internal Fuselage Skin ALL T 240 M
5320012−201 and Structure, R 120 M
5320021−201
5320022−202 FS281.00 to FS861.00, Above WL71.50, GX
5320023−202 XRS
5320024−202 GL6000
5320025−202 GL6500
5330007−201
5340006−201 FS281.00+32.00 to FS861.00, Above WL71.50 GL5000
GV5000
MAINTENANCE REVIEW BOARD REPORT

GL5500
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320002−201 ED−CPCP 53−20−00−202 Detailed Inspection of the Lower Internal Skin ALL T 120 M
and Structure, R 120 M

FS381.00 to FS557.00, Below WL71.50, GX

XRS
GL6000

5−22−10
PART 3
GL6500

FS381.00+32.00 to FS557.00, Below WL71.50 GL5000

GV5000
GL5500

Page 8
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320002−202 ED 53−20−00−203 Detailed Inspection of the Lower Internal Skin ALL T 60 M

and Structure, R 60 M

FS381.00 to FS557.00 As Visible From the GX

EFFECTIVITY: ALL
Crawlway, XRS
GL6000
GL6500

FS381.00+32.00 to FS557.00 As Visible From GL5000

the Crawlway GV5000
GL5500

5320005−201 ED 53−20−00−204 Detailed Inspection of the Keel Beam, FS501.00 ALL T 120 M
to FS574.00 and BL4.6L to BL4.6R R 120 M

5320006−201 ED 53−20−00−205 Detailed Inspection of the Over−Wing Longeron, ALL T 120 M

FS525.00 to FS574.00 and STR19L and R 120 M
STR19R

5320007−201 ED−CPCP 53−20−00−206 Detailed Inspection of the Forward Face of the ALL T 120 M
MAINTENANCE REVIEW BOARD REPORT

Pressure Bulkhead Below WL71.50, FS557.00 R 120 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320008−201 ED 53−20−00−207 Detailed Inspection of the Aft Face of the ALL T 120 M
Pressure Bulkhead Below WL71.50, FS557.00 R 120 M

5320009−201 ED−CPCP 53−20−00−208 Detailed Inspection of the Top Side of the ALL T 120 M
Pressure Floor, FS557.00 to FS574.50 and R 120 M

5−22−10
PART 3
BL46L to BL46R

Page 9
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320011−201 ED−CPCP 53−20−00−209 Detailed Inspection of the Floor Support ALL T 120 M
Structure, R 120 M

FS381.00 to FS557.00, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS381.00+32.00 to FS557.00 GL5000

GV5000
GL5500

5320011−202 ED−CPCP 53−20−00−210 Detailed Inspection of the Floor Support ALL T 120 M
Structure, R 60 M

FS381.00 to FS557.00 As Visible From the GX

Crawlway, XRS
GL6000
GL6500

FS381.00+32.00 to FS557.00 As Visible From GL5000

MAINTENANCE REVIEW BOARD REPORT

the Crawlway GV5000

BD−700 TIME LIMITS/MAINTENANCE CHECKS

GL5500

5−22−10
PART 3
Page 10
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320013−201 ED−CPCP 53−20−00−212 Detailed Inspection of the Internal Structure ALL T 120 M
Below WL71.50, R 60 M

FS281.00 to FS381.00, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS281.00+32.00 to FS381.00+32.00 GL5000

GV5000
GL5500

5320013−202 ED 53−20−00−213 Detailed Inspection of the Internal Structure ALL T 60 M

Below WL71.50, R 60 M

FS281.00 to FS381.00, As Visible with the Floor GX

Panels Installed, XRS
GL6000
GL6500

FS281.00+32.00 to FS381.00+32.00, As Visible GL5000

MAINTENANCE REVIEW BOARD REPORT

with the Floor Panels Installed GV5000

BD−700 TIME LIMITS/MAINTENANCE CHECKS

GL5500

5−22−10
PART 3
Page 11
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320017−201 ED−CPCP 53−20−00−214 Detailed Inspection of the Floor Support ALL T 120 M
Structure, R 120 M

FS281.00 to FS381.00, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS281.00+32.00 toFS381.00+32.00 GL5000

GV5000
GL5500

5320017−202 ED−CPCP 53−20−00−215 Detailed Inspection of the Floor Support ALL T 120 M
Structure, R 60 M

FS281.00 to FS381.00 As Visible From the GX

Crawlway, XRS
GL6000
GL6500

FS281.00+32.00 to FS381.00+32.00 As Visible GL5000

MAINTENANCE REVIEW BOARD REPORT

From the Crawlway GV5000

BD−700 TIME LIMITS/MAINTENANCE CHECKS

GL5500

5−22−10
PART 3
Page 12
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320018−201 ED AD 53−20−00−216 Detailed Inspection of the Floor Structure in the ALL T 60 M

CPCP Way of the Passenger Door Step, R 60 M

FS310.00 to FS347.00, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS310.00+32.00 to FS347.00+32.00 GL5000

GV5000
GL5500

5320019−201 ED−AD 53−20−00−217 Detailed Inspection of the Sills, Frames, Skin ALL T 60 M
and Edge Members around the Passenger Door R 60 M
Cutout

5320019−202 ED−CPCP 53−20−00−218 Detailed Inspection of the Internal Skin around ALL T 120 M
the Passenger Door Cutout R 120 M

5320020−201 ED−CPCP 53−20−00−219 Detailed Inspection of the Fittings and Hinges on ALL T 120 M
MAINTENANCE REVIEW BOARD REPORT

the Fuselage for the Passenger Door R 120 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320022−201 ED−CPCP 53−20−00−221 Detailed Inspection of the Fuselage Longitudinal ALL T 120 M
Joints, R 120 M

FS281.00 to FS381.00, STR19R and STR25L, GX

XRS
GL6000

5−22−10
PART 3
GL6500

FS281.00+32.00 to FS381.00+32.00, STR19R GL5000

and STR25 GV5000
GL5500

Page 13
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320023−201 ED−CPCP 53−20−00−223 Detailed Inspection of the Fuselage Longitudinal ALL T 120 M
Joints, R 120 M

FS381.00 to FS557.00 − STR20L and STR20R, GX

EFFECTIVITY: ALL
XRS
GL6000
GL6500

FS381.00+32.00 to FS557.00 − STR20L and GL5000

STR20R GV5000
GL5500

5320024−201 ED−CPCP 53−20−00−225 Detailed Inspection of the Fuselage Barrel Joint, ALL T 120 M
R 120 M
FS381.00, Below WL71.50, GX
XRS
GL6000
GL6500

FS381.00+32.00, Below WL71.50 GL5000

GV5000
MAINTENANCE REVIEW BOARD REPORT

GL5500
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320025−201 ED−CPCP 53−20−00−227 Detailed Inspection of the Fuselage Barrel Joint, ALL T 120 M
FS557.00, Below WL71.50 R 120 M

5−22−10
PART 3
Page 14
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320026−201 ED AD 53−20−00−229 Detailed Inspection of the Machined Fitting and ALL T 60 M

CPCP Skin around the Service Door, R 60 M

FS295.00 to FS310.00 and STR22R to GX

EFFECTIVITY: ALL
STR24R, XRS
GL6000
GL6500

FS295.00+32.00 to FS310.00+32.00 and GL5000

STR22R to STR24R GV5000
GL5500

5320026−202 ED−CPCP 53−20−00−230 Detailed Inspection of the Machined Fitting and ALL T 120 M
Skin around the Service Door, R 120 M

FS295.00 to FS310.00 and STR22R to GX

STR24R As Visible From the Crawlway, XRS
GL6000
GL6500

FS295.00+32.00 to FS310.00+32.00 and GL5000

MAINTENANCE REVIEW BOARD REPORT

STR22R to STR24R As Visible From the GV5000

BD−700 TIME LIMITS/MAINTENANCE CHECKS

Crawlway GL5500

5320004−205 ED 53−20−00−244 Detailed Inspection of the Lower External Skin of GX T 120 M

the Fuselage, FS381.00 to FS557.00 and XRS R 120 M
STR6L to STR6R Covered by the Forward Fuel GL6000
Tank (A/C 9003, 9096, 9159 and Subs) GL6500

5−22−10
PART 3
5330001−201 ED−CPCP 53−30−00−201 Detailed Inspection of the Front Spar Frame ALL T 180 M
Above WL71.50, FS574.50 R 120 M

Page 15
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5330001−202 ED−CPCP 53−30−00−202 Detailed Inspection of the Front Spar Frame ALL T 120 M
Below WL71.50, FS574.50 R 120 M

EFFECTIVITY: ALL
5330002−201 ED−CPCP 53−30−00−203 Detailed Inspection of the Rear Spar Frame ALL T 180 M
Above WL71.50, FS719.30 R 120 M

5330002−202 ED−CPCP 53−30−00−204 Detailed Inspection of the Rear Spar Frame ALL T 120 M
Below WL71.50, FS719.30 R 120 M

5330004−201 ED−AD 53−30−00−205 Detailed Inspection of the Surround Structure for ALL T 60 M
the Over−Wing Emergency Exit −External R 60 M

5330004−203 ED−CPCP 53−30−00−206 Detailed Inspection of the Surround Structure for ALL T 180 M
the Over−Wing Emergency Exit − Internal R 120 M

5330005−201 ED 53−30−00−207 Detailed Inspection of the Fittings on the Frame ALL T 60 M

of the Over−Wing Emergency Exit R 60 M
MAINTENANCE REVIEW BOARD REPORT

5330006−201 ED 53−30−00−208 Detailed Inspection of the External Skin around ALL T 120 M
the Cabin Window Cutouts R 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5330007−202 ED−CPCP 53−30−00−210 Detailed Inspection of the Internal Structure of ALL T 120 M
the Fuselage Below WL71.50, FS557.00 to R 120 M
FS797.60

5330008−201 ED−CPCP 53−30−00−211 Detailed Inspection of the Top of the Pressure ALL T 120 M

5−22−10
PART 3
Floor, FS719.30 to FS781.00 and BL35L to R 120 M
BL35R

Page 16
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5330009−201 ED 53−30−00−212 Detailed Inspection of the Lower Side of the ALL T 120 M
Pressure Floor, FS719.30 to FS781.00 and R 120 M
BL35L to BL35R

EFFECTIVITY: ALL
5330010−201 ED−CPCP 53−30−00−213 Detailed Inspection of the Pressure Floor ALL T 120 M
Beams, FS713.10 to FS781.00, BL0.0, BL9, R 120 M
BL19, BL27 and BL35

5330013−201 ED 53−30−00−214 Detailed Inspection of the Keel Beam Structure, ALL T 120 M
FS719.30 to FS781.00 R 120 M

5330014−201 ED 53−30−00−215 Detailed Inspection of the Pressure Bulkheads, ALL T 120 M

FS719.30 and FS781.00 − External R 120 M

5340001−203 ED 53−40−00−201 Detailed Inspection of the External Skin of the ALL T 120 M
Fuselage Below the Vertical Stabilizer, R 120 M
FS945.00 to the Rear Spar of the Vertical
Stabilizer
MAINTENANCE REVIEW BOARD REPORT

5340001−204 ED 53−40−00−202 Detailed Inspection of the External Skin of the ALL T 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Fuselage Below the Pylon, FS877.25 to the R 120 M

Rear Spar of the Vertical Stabilizer

5340003−201 ED 53−40−00−203 Detailed Inspection of the External Skin of the ALL T 120 M
Fuselage Below the Wing−to−Fuselage Fairing, R 120 M
and the Aft Keel Beam, FS781.00 to FS945.00

5−22−10
PART 3
5340004−201 ED AD 53−40−00−204 Detailed Inspection of the Stop Fittings of the ALL T 60 M
CPCP Baggage Door on the Fuselage R 60 M

Page 17
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5340005−201 ED−CPCP 53−40−00−205 Detailed Inspection of the Internal Surround ALL T 120 M
Structure of the Baggage Door, Forward of the R 120 M
Pressure Bulkhead

EFFECTIVITY: ALL
5340005−202 ED AD 53−40−00−206 Detailed Inspection of the Baggage Door Cutout ALL T 60 M
CPCP Surround Structure R 60 M

5340007−201 ED AD 53−40−00−208 Detailed Inspection of the Internal Fuselage ALL T 60 M

CPCP Structure and Forward Face of the Rear R 60 M
Pressure Bulkhead Below the Floor, and the
Floor Structure of the Baggage Compartment

5340008−201 ED−CPCP 53−40−00−209 Detailed Inspection of the Forward Face of the ALL T 180 M
Rear Pressure Bulkhead Above the Floor R 60 M

5340009−201 ED 53−40−00−210 Detailed Inspection of the Structure of the Aft ALL T 120 M
Face of the Rear Pressure Bulkhead R 120 M

5340010−201 ED 53−40−00−211 Detailed Inspection of the Upper Sill and Stop ALL T 120 M
MAINTENANCE REVIEW BOARD REPORT

Backup Structure of the Baggage Door, Aft of R 120 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

the Pressure Bulkhead

5340011−201 ED 53−40−00−212 Detailed Inspection of the Auxiliary Fuel Tank GX T 120 M

Floor Structure XRS R 120 M
GL6000
GL6500

5−22−10
PART 3
5340013−201 ED−AD 53−40−00−213 Detailed Inspection of the Aft Equipment ALL T 60 M
Compartment Interior Structure, FS861.00, R 60 M
Vertical−Stabilizer Rear−Spar Frame

Page 18
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5340014−201 ED 53−40−00−214 Detailed Inspection of the Aft Equipment GX T 120 M

Compartment Interior Structure Adjacent to the XRS R 120 M
Auxiliary Fuel Tank, FS861.00 to FS893.50, GL6000
WL80.25 to WL137.00 GL6500

EFFECTIVITY: ALL
5340015−201 ED 53−40−00−215 Detailed Inspection of the Forward ALL T 120 M
Engine−Mount Frame−Assembly R 60 M

5340016−201 ED−CPCP 53−40−00−216 Detailed Inspection of the Support Structure of ALL T 120 M
the Inner Flap Inboard Track R 120 M

5350001−201 ED−AD 53−50−00−201 Detailed Inspection of the Aft Engine−Mount ALL T 60 M

Frame−Assembly R 60 M

5350002−201 ED 53−50−00−202 Detailed Inspection of the Mid Spar Frame ALL T 120 M
R 120 M

5350003−201 ED 53−50−00−203 Detailed Inspection of the Rear Spar Frame ALL T 120 M
R 120 M
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5350004−201 ED 53−50−00−204 Detailed Inspection of the Strut Attach and ALL T 120 M
Backup Fittings of the APU Mount Structure R 120 M

5−22−10
PART 3
Page 19
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5450002−201 ED 54−50−00−201 Detailed Inspection of the Vertical Flange of the ALL T 120 M
Pylon Drag Angles − PS30.00 to PS151.00 R 120 M

EFFECTIVITY: ALL
5450003−201 ED−AD 54−50−00−202 Detailed Inspection of the Pylon Center Box ALL T 60 M
Internal Structure − PS30.00 to PS151.00 R 60 M
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Page 20
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5510001−201 ED 55−10−00−201 Detailed Inspection of the Attachment Fittings ALL T 120 M

and Straps of the Horizontal Stabilizer R 120 M

EFFECTIVITY: ALL
5510002−201 ED 55−10−00−202 Detailed Inspection of the Center Box Ribs and ALL T 120 M
Fittings of the Horizontal Stabilizer R 120 M

5510003−201 ED 55−10−00−203 Detailed Inspection of the Horizontal Stabilizer ALL T 120 M

Hinge, Support, and Backup Fittings at Ribs 4, R 120 M
5, 9 and 12

5510004−201 ED−AD 55−10−00−204 Detailed Inspection of the External Skin of the ALL T 7500 L
Horizontal Stabilizer R 7500 L

5510005−201 ED−AD 55−10−00−205 Detailed Inspection of the Internal Skin and ALL T 3750 L
Structure of the Horizontal Stabilizer R 3750 L

5520001−201 ED−AD 55−20−00−201 Special Detailed Inspection of the Upper and ALL T 1875 L
Lower Skins of the Elevator R 1875 L
MAINTENANCE REVIEW BOARD REPORT

5520003−201 ED−AD 55−20−00−202 Detailed Inspection of the Ribs and Spar of the ALL T 7500 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Elevator R 7500 L

5520002−201 ED 55−20−05−201 Detailed Inspection of the Fittings of the Elevator ALL T 120 M
R 120 M

5530002−201 ED 55−30−00−202 Detailed Inspection of the Stabilizer Drag Angles ALL T 120 M

5−22−10
PART 3
− Front Spar Datum to Rear Spar Datum R 120 M

5530003−201 ED 55−30−00−203 Detailed Inspection of the Front Spar, Web and ALL T 120 M
Straps of the Vertical Stabilizer R 120 M

Page 21
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5530001−202 ED 55−30−00−205 General Visual Inspection of the ALL T 120 M

Vertical−Stabilizer Skin Outer−Surfaces R 60 M
Covered by Access Panels and Rudder Seal

EFFECTIVITY: ALL
5530001−203 ED 55−30−00−206 General Visual Inspection of the ALL T 60 M
Vertical−Stabilizer Skin Outer−Surfaces R 60 M
Covered by the Dorsal and Bullet Fairings

5530004−201 ED 55−30−01−201 Detailed Inspection of the Horizontal Legs, ALL T 60 M

Front−Spar Joint Legs, and Shear Angle of the R 60 M
Vertical−Stabilizer Front Spar−to−Fuselage
Interface−Fittings

5530005−201 ED 55−30−01−203 Detailed Inspection of the Fittings and Wishbone ALL T 120 M
5530008−202 ED Attachments of the Rudder and Rear Spar Aft R 120 M
5540002−201 ED Face and Rudder Hinge of the Vertical Stabilizer

5530006−201 ED 55−30−01−204 Detailed Inspection of the Tip Canted Rib and ALL T 120 M
the Rib Fittings of the Vertical Stabilizer R 60 M
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5530007−201 ED 55−30−01−205 Detailed Inspection of the Internal Structure and ALL T 120 M
5530005−202 ED Rear Spar Forward Face of the Vertical R 60 M
5530008−201 ED Stabilizer and Wishbone Attachments to the
Vertical Stabilizer

5530008−201 ED 55−30−01−206 Detailed Inspection of the Attachments and ALL T 120 M

Fittings of the Wishbone to the Vertical Stabilizer R 120 M

5−22−10
PART 3
5530009−201 ED 55−30−01−207 Detailed Inspection of the Lower Attachment ALL T 120 M
Pins of the Pitch Trim Actuator R 120 M

Page 22
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5530009−202 ED 55−30−01−208 Detailed Inspection of the Lower Attachment ALL T 60 M

Bolts of the Pitch Trim Actuator R 60 M

EFFECTIVITY: ALL
5530010−201 ED 55−30−01−209 Detailed Inspection of the Rudder Hinge Pins ALL T 120 M
R 120 M

5540001−201 ED−AD 55−40−00−201 Special Detailed Inspection of the Skins of the ALL T 1875 L
Rudder, External R 1875 L

5540003−201 ED−AD 55−40−00−203 Detailed Inspection of the Ribs and Spar of the ALL T 7500 L
Rudder R 7500 L

5540002−202 ED 55−40−00−205 Detailed Inspection of the Backup Fittings of the ALL T 120 M
Rudder R 120 M
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Page 23
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5711001−201 ED 57−10−00−201 Detailed Inspection of the Forward Face of the ALL T 120 M
Front Spar of the Center Wing − LBL47.6 to R 120 M
RBL47.6

EFFECTIVITY: ALL
5711002−201 ED 57−10−00−202 Detailed Inspection of the Center Wing Front ALL T 120 M
5711007−201 ED Spar Aft Face, and Center Wing Upper Panel, R 60 M
Lower Panel and Ribs − Internal LBL47.6 to
RBL47.6

5711003−201 ED 57−10−00−203 Detailed Inspection of the Forward Face of the ALL T 120 M
Rear Spar of the Center Wing − LBL47.6 to R 120 M
RBL47.6

5711004−201 ED 57−10−00−204 Detailed Inspection of the Aft Face of the Rear ALL T 120 M
Spar of the Center Wing − LBL47.6 to RBL47.6 R 120 M

5711005−201 ED 57−10−00−205 Detailed Inspection of the Upper Face of the ALL T 120 M
Center Wing Upper Panel R 120 M
MAINTENANCE REVIEW BOARD REPORT

5711006−201 ED 57−10−00−206 Detailed Inspection of the Lower Face of the ALL T 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Center Wing Lower Panel R 60 M

5711008−201 ED 57−10−00−208 Detailed Inspection of the Outer Face of the ALL T 120 M
Center Wing Root Rib R 60 M

5711009−201 ED 57−10−00−209 Detailed Inspection of the Main Landing Gear ALL T 120 M

5−22−10
PART 3
(MLG) Side Stay Fitting R 60 M

5720001−201 ED−CPCP 57−20−00−201 Detailed Inspection of the Forward Face of the ALL T 120 M
Front Spar of the Wing R 120 M

Page 24
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5720002−201 ED 57−20−00−202 Detailed Inspection of the Aft Face of the Front ALL T 120 M
Spar of the Wing − BL47.61 to CWS537.40 R 120 M

EFFECTIVITY: ALL
5720003−201 ED 57−20−00−203 Detailed Inspection of the Forward Face of the ALL T 120 M
Rear Spar of the Wing − BL47.61 to CWS537.40 R 120 M

5720004−201 ED−AD 57−20−00−204 Detailed Inspection of the Aft Face of the Rear ALL T 60 M
5720009−201 Spar and Auxiliary Spar of the Wing R 60 M

5720006−202 ED 57−20−00−205 Detailed Inspection of the Lower Wing Surface ALL T 120 M
Covered by the Fuel Access Panels R 60 M

5720007−201 ED 57−20−00−206 Detailed Inspection of the Internal Skin and ALL T 120 M
Structure of the Wing − BL47.61 to CWS537.40 R 60 M

5720008−201 ED 57−20−00−207 Detailed Inspection of the Internal Skin and ALL T 120 M
Structure of the Wing − CWS537.40 to R 60 M
WS536.50
MAINTENANCE REVIEW BOARD REPORT

5720010−201 ED 57−20−00−210 Detailed Inspection of the Main Landing Gear ALL T 120 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5720004−202 (MLG) Trunnion Fitting and Bay R 120 M

5720009−202
5720007−202

5720023−201 ED 57−20−00−212 Detailed Inspection of the Aileron Support ALL T 120 M

Fittings R 120 M

5−22−10
PART 3
5720004−203 ED−AD 57−20−00−213 Detailed Inspection of the Internal Wing ALL T 120 M
5720009−203 Structure between the Rear Spar and Auxiliary R 60 M
5720007−203 Spar, WS85.00 to WS178.00

Page 25
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5730002−201 ED 57−30−00−202 Detailed Inspection of the Winglet Attachment ALL T 120 M

Fittings R 120 M

EFFECTIVITY: ALL
5720012−201 ED 57−42−00−201 Detailed Inspection of the No. 1 Slat Support ALL T 120 M
Fittings R 120 M

5720013−201 ED 57−42−00−202 Detailed Inspection of the No. 2, No. 3 and No. 4 ALL T 120 M
Slat Support Fittings R 120 M

5740001−201 ED 57−42−02−201 Detailed Inspection of the No. 1 Slat Track Rails ALL T 60 M
R 60 M

5740001−202 ED 57−42−02−202 Detailed Inspection of the No. 1 Slat Rail ALL T 120 M
Support Fittings R 120 M

5740001−203 ED 57−42−02−203 Detailed Inspection of the No. 1 Slat Body ALL T 120 M
R 120 M
MAINTENANCE REVIEW BOARD REPORT

5740002−201 ED 57−42−02−204 Detailed Inspection of the No. 2, No. 3 and No. 4 ALL T 60 M
Slat Track Rails R 60 M
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5740002−202 ED 57−42−02−205 Detailed Inspection of the No. 2, No. 3 and No. 4 ALL T 120 M
Slat Rail Support Fittings R 120 M

5740002−203 ED 57−42−02−206 Detailed Inspection of the No. 2, No. 3 and No. 4 ALL T 120 M
Slat Bodies R 120 M

5−22−10
PART 3
5750001−209 ED 57−51−00−201 Special Detailed Inspection of the Inboard−Flap ALL T 60 M
Internal Ribs R 60 M

Feb 28/2020
Page 26
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5720016−201 ED 57−51−05−201 Detailed Inspection of the Flap Track Rails − ALL T 60 M

WS47.80, WS178.00, WS287.00 and WS404.00 R 60 M

EFFECTIVITY: ALL
5720016−202 ED 57−51−05−202 Detailed Inspection of the Flap Support Fittings ALL T 120 M
− WS47.80, WS178.00, WS287.00 and R 120 M
WS404.00

5750001−201 ED 57−51−05−203 Detailed Inspection of the Inner−Flap ALL T 60 M

Inner−Fittings and End Ribs R 60 M

5750001−202 ED 57−51−05−204 Detailed Inspection of the Inner−Flap ALL T 60 M

Outer−Fittings and the Middle−Flap R 60 M
Inner−Fittings and End Ribs

5750001−203 ED 57−51−05−205 Detailed Inspection of the Middle−Flap ALL T 60 M

Outer−Fittings and the Outer−Flap Inner−Fittings R 60 M
and End Ribs

5750001−204 ED 57−51−05−206 Detailed Inspection of the Outer−Flap ALL T 60 M

MAINTENANCE REVIEW BOARD REPORT

Outer−Fittings and End Ribs R 60 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

5750001−205 ED−AD 57−51−05−207 Detailed Inspection of the Inner Flaps Upper and ALL T 1875 L
Lower Skin R 1875 L

5750001−206 ED−AD 57−51−05−208 Special Detailed Inspection of the Inner Flaps ALL T 950 L
Trailing Edge Upper and Lower Skin and Core R 950 L

5−22−10
PART 3
5750001−207 ED−AD 57−51−05−209 Detailed Inspection of the Middle/Outboard ALL T 3750 L
Upper and Lower Flaps Skin R 3750 L

Feb 28/2020
Page 27
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5750001−208 ED−AD 57−51−05−210 Special Detailed Inspection of the Middle/Outer ALL T 1875 L
Flap Panel Trailing Edge Upper and Lower Skin R 1875 L
and Core

EFFECTIVITY: ALL
5760001−201 ED 57−60−00−201 Detailed Inspection of the Aileron Hinge Fittings ALL T 120 M
R 120 M

5760001−202 ED−AD 57−60−00−202 Special Detailed Inspection of the Aileron Skin ALL T 1875 L
R 1875 L

5760001−203 ED−AD 57−60−00−203 Detailed Inspection of the Aileron Spar ALL T 7500 L
R 7500 L

5720020−201 ED 57−71−00−201 Detailed Inspection of the Ground−Spoiler ALL T 120 M

Support−Fittings R 120 M

5770001−201 ED 57−71−00−202 Detailed Inspection of the Ground−Spoiler ALL T 120 M

Support−Fittings − BL47.61 and WS178.00 R 120 M
MAINTENANCE REVIEW BOARD REPORT

5770001−202 ED−AD 57−71−00−203 Special Detailed Inspection of the Ground ALL T 3750 L
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Spoiler Skin R 3750 L

5720021−201 ED 57−72−00−201 Detailed Inspection of the Multi−Function Spoiler ALL T 120 M

Support−Fittings R 120 M

5770002−201 ED 57−72−00−202 Detailed Inspection of the Multi−Function Spoiler ALL T 120 M

5−22−10
PART 3
Hinge Fittings − WS178.00 and WS404.00 R 120 M

Feb 28/2020
Page 28
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5770002−202 ED−AD 57−72−00−203 Special Detailed Inspection of the ALL T 3750 L

Multi−Function Spoiler Skin − WS178.00 and R 3750 L
WS404.00

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Feb 28/2020
Page 29
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

7110001−201 ED 71−12−01−201 Detailed Inspection of the Upper Cowls ALL T 120 M

R 120 M

EFFECTIVITY: ALL
7110001−202 ED−AD 71−12−01−202 Special Detailed Inspection of the Upper Cowls ALL T 1875 L
R 1875 L

7120001−201 ED 71−20−00−201 Detailed Inspection of the Mounts ALL T 120 M

R 120 M

7120001−202 ED 71−20−00−202 Detailed Inspection of the Casing Lugs for the ALL T 60 M
Front Mounts R 60 M
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Feb 28/2020
Page 30
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

7830001−201 ED 78−31−01−201 Detailed Inspection of the Upper Pivoting Doors ALL T 120 M
(Metallic) R 120 M

EFFECTIVITY: ALL
7830001−202 ED−AD 78−31−01−202 Special Detailed Inspection of the Upper ALL T 1875 L
Pivoting Doors (Composite) R 1875 L
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−22−10
PART 3
Feb 28/2020
Page 31
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

ZONAL INSPECTION PROGRAM

1. General

This section provides the general visual inspection (GVI) and Visual Checks (VCK)
requirements for each aircraft zone to check system and powerplant installations and
structure for security and general condition.

There are zones which will require more than one inspection at different intervals, because
the depth at which the zone is to be examined can necessitate differing levels of accessibility.

2. Program Rules

The purpose of the following program rules is to provide standard guidelines to the zonal
maintenance program.

A. Zones which contain systems/components/installations are assigned a zonal GVI task to

be performed at specified intervals. Zones which contain no systems installations or
which received adequate coverage from other maintenance or structural inspection tasks
will not require the additional zonal inspection task. Detailed and Special Detailed
Inspection tasks shall not be contained in the Zonal Inspection Program.

B. When necessary, seats, carpets, ceiling and wall trim panels including insulation are to
be removed to access and complete an adequate GVI.

3. List of Zonal Identification Numbers (ZINs)

This section contains a list of all the ZIN items sorted in ATA/zone sequence by ZIN number.
Each ZIN is covered by at least one MSG−3 task.

ZONE ID No. DESCRIPTION TASK

3270000001 Nose Landing Gear Assembly ALL

3270000002 LH/RH Main Landing Gear Assembly ALL

3270000003 LH/RH/AFT Nose Landing Gear Doors ALL

3270000004 LH/RH Main Landing Gear Inboard Doors ALL

3270000005 LH/RH Main Landing Gear Outboard Doors ALL

5280000001 External RH Overwing Emergency Exit Door ALL

5280000003 Baggage Compartment Door ALL

5280000011 External Passenger Door ALL

EFFECTIVITY: ALL
PART 3 Page 1
5−23−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

ZONE ID No. DESCRIPTION TASK

5310000002 Internal Nose Radome ALL

5310000004 Internal LH Lower Nose Compartment ALL

5310000005 Internal RH Lower Nose Compartment ALL

5310000006 Internal Nose Wheel Well ALL

5310000009 Mid−Lower Fuselage/Slat Drive Compartment ALL

5310000020 Internal Underfloor Baggage Compartment ALL

5310000021 Internal Aft Wing to Fuselage Fairing ALL

5310000032 External Lower Mid Fuselage Under Fairing ALL

5310000033 Main Landing Gear Wheel Well ALL

5310000034 Internal Lower Mid Fuselage Between Center Wing and Cabin ALL
Floor

5310000036 External Underside of the Center Wing Box ALL

5310000037 Internal Center Wing Box ALL

5310000081 External Lower Forward Fuselage, Including Internal ALL

Wing−to−Fuselage Fairing

5310000082 Internal Lower Forward Fuselage ALL

5310000083 External wing−to−Fuselage Fairing ALL

5310020001 External Forward Fuselage ALL

5320000002 Internal Forward Equipment Compartment ALL

5320000004 Internal Flight Compartment ALL

5320000020 External Baggage Compartment ALL

5320000021 Internal Baggage Compartment ALL

5320000031 External Mid−Fuselage ALL

5320000035 Internal Mid−Fuselage Compartment Above the Cabin Floor ALL

5320000081 External Upper Forward Fuselage ALL

EFFECTIVITY: ALL
PART 3 Page 2
5−23−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

ZONE ID No. DESCRIPTION TASK

5320000082 Internal Upper Forward Fuselage ALL

5320000083 Avionics Rack GL5000

GV5000
GL5500

5330000020 External Aft Fuselage/Vertical Stabilizer Section ALL

5330000021 Internal Aft Fuselage ALL

5330000022 External Tail Cone ALL

5330000023 Internal Tail Cone ALL

5330000024 External Fuselage/Vertical Stabilizer Section ALL

5440000001 External LH/RH Pylon ALL

5530000001 External Ram Air Inlet fairing ALL

5530000002 Internal Ram Air fairing and External Vertical Stabilizer Leading ALL
Edge

5530000003 External Vertical Stabilizer ALL

5530000004 Internal Vertical Stabilizer ALL

5530000005 External Vertical Stabilizer Bullet Fairing ALL

5530000006 Internal Vertical Stabilizer Bullet Fairing ALL

5530000007 Internal Vertical Stabilizer Leading Edge ALL

5530000008 Internal Rudder Leading Edge ALL

5530000009 External Rudder ALL

5530000010 External LH/RH Horizontal Stabilizer ALL

5530000011 Internal Horizontal Stabilizer Leading Edges ALL

5530000013 External LH/RH Horizontal Stabilizer Rear Spar ALL

5750060003 External LH/RH Leading Edge and Slats ALL

5750060004 Internal LH/RH Leading Edge and Slats ALL

5750060007 External LH/RH Inboard Wing ALL

EFFECTIVITY: ALL
PART 3 Page 3
5−23−00 May 31/2019
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

ZONE ID No. DESCRIPTION TASK

5750060008 Internal LH/RH Inboard Wing ALL

5750060009 External LH/RH Inboard Wing Between Auxiliary Spar and Rear ALL
Spar Between WS85.50 and WS178.00

5750060010 External LH/RH Mid Wing Box ALL

5750060011 Internal LH/RH Mid Wing Box ALL

5750060012 External LH/RH Outboard Wing Box ALL

5750060013 Internal LH/RH Outboard Wing ALL

5750060014 External LH/RH Inboard Wing Between Auxiliary Spar and Rear ALL
Spar Between BL47.60 and WS85.50

5750060015 External LH/RH Winglet ALL

5730003

5750060017 Internal LH/RH Inboard Flap ALL

5750060018 Inboard Flap Actuator Attachment Fitting ALL

5750060019 External LH/RH Mid Flap, Outboard Flap and Aileron ALL

5750060020 Aileron Hinge Fittings ALL

7140000001 External LH/RH Engine Nacelles ALL

7140000023 Internal LH/RH Engines (Fan Cowl Door Open) ALL

7840000022 LH/RH Thrust Reversers (Thrust Reversers Deployed) ALL

The following ZINs did not produce any MSG−3 zonal tasks. The details on how these ZINs
are inspected are in the following table.

Zone ID No. Description Coverage

5280000002 Internal Emergency Covered by SSI 5221003

Over−Wing Exit Door

5280000012 Internal Passenger Door Covered by SSI 5210002 and MSI 521000

5310000020 Internal Underfloor Baggage Covered by SSI 5340007 and MSIs 212000,
Compartment 213000, 271100, 272100, 273100

EFFECTIVITY: ALL
PART 3 Page 4
5−23−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

Zone ID No. Description Coverage

5320000008 Internal Forward Avionics, Covered by SSI 5310012 and MSIs 271100,
Power Distribution and 272100, 273100, 320000, 341100, 351000
Flight Controls
Compartment

5440000002 Internal Pylons Covered by SSI 5450003

5530000012 Internal Horizontal Stabilizer External Inspection of Horizontal Stabilizer

(ZIN 5530000010) includes looking for signs
of internal damage

5750060016 Internal Winglet External Inspection of the Winglets (ZIN

5750060015) includes looking for signs of
internal damage

7140000021 Internal Nose Cowlings External Inspection of the Engine Nacelles

(ZIN 7140000001) includes looking at the
internal nose cowlings for signs of damage
such as discoloration and deformation

4. Task and Intervals Table Format

Data about the tables used in section 5−23−10 are given below:

MSG−3 Route Chapter 5 Task Title Program Task Interval

Task No. Task No.

A. MSG−3 Task No. Column

This column shows all MSG−3 tasks from the zonal analysis. The task numbers are in
the form XXXXXXXXXX−YZ for zonal tasks. XXXXXXXXXX is the ZIN number. Y is 0 for
MSG−3. Z is the task sequence identifier. Whenever a MSG−3 task precludes (absorbs)
other tasks, the other tasks are listed beneath it. The format for avionics, systems,
powerplant tasks and structures tasks are defined in section 5−21−00 and 5−22−00,
respectively.

B. Route Column

This column shows the working group from which the MSG−3 task was transferred
(when applicable).

EFFECTIVITY: ALL
PART 3 Page 5
5−23−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

C. Chapter 5 Task No. Column

This column shows the Chapter 5 task number that corresponds to the MSG−3 task
number in column 1. Chapter 5 task numbers are XX−XX−XX−YZZ, where
− XX−XX−XX is the ATA number
− Y=2 shows that the source data was the MRB report
− ZZ is a number that starts at 01 for all different ATA numbers.

D. Task Title Column

This column contains the task title. This title includes the inspection level and a brief
description of the area or items to be inspected.

E. Program Column

This column shows the Global model variant to which the task applies.

F. Task Interval Column

This column contains the task intervals. The interval is defined from the last time that
particular task was carried out. The intervals in this column are in flight hours (H),
months (M) or in landings (L).

EFFECTIVITY: ALL
PART 3 Page 6
5−23−00 Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3
SECTION 5−23−10

ZONAL INSPECTION PROGRAM

Tasks and Intervals

EFFECTIVITY: ALL
PART 3 Cover
5−23−10 Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

3270000001−01 32−ZL−00−201 General Visual Inspection of the Nose Landing ALL 450 L
3220001−201 STRU Gear (NLG) Assembly

EFFECTIVITY: ALL
3270000002−01 32−ZL−00−202 General Visual Inspection of the Main Landing ALL 450 L
3210001−201 STRU Gear Assembly − LH

3270000002−02 32−ZL−00−203 General Visual Inspection of the Main Landing ALL 450 L
3210001−201 STRU Gear Assembly − RH

3270000003−01 32−ZL−00−204 General Visual Inspection of the Nose Landing ALL 900 L
Gear Door − LH

3270000003−02 32−ZL−00−205 General Visual Inspection of the Nose Landing ALL 900 L
Gear Door − RH

3270000003−03 32−ZL−00−206 General Visual Inspection of the Nose Landing ALL 900 L
Gear Door − Aft
MAINTENANCE REVIEW BOARD REPORT

3270000004−01 32−ZL−00−207 General Visual Inspection of the Main Landing ALL 450 L
Gear (MLG) Inboard Door − LH
BD−700 TIME LIMITS/MAINTENANCE CHECKS

3270000004−02 32−ZL−00−208 General Visual Inspection of the Main Landing ALL 450 L
Gear (MLG) Inboard Door − RH

3270000005−01 32−ZL−00−209 General Visual Inspection of the Main Landing ALL 450 L
Gear (MLG) Outboard Door − LH

5−23−10
PART 3
3270000005−02 32−ZL−00−210 General Visual Inspection of the Main Landing ALL 450 L
Gear (MLG) Outboard Door − RH

Page 1
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5280000001−01 52−ZL−00−201 General Visual Inspection of the Over−Wing ALL 60 M

5221001−201 STRU Emergency Exit − External

EFFECTIVITY: ALL
5280000001−02 52−ZL−00−202 General Visual Inspection of the Latch ALL 60 M
Mechanism of the Over−Wing Emergency Exit

5280000003−01 52−ZL−00−203 General Visual Inspection of the Baggage Door ALL 120 M
5230001−201 STRU − Inboard Side

5280000003−02 52−ZL−00−204 General Visual Inspection of the Baggage Door ALL 120 M
5230001−201 STRU − Outboard Side

5280000011−01 52−ZL−00−205 General Visual Inspection of the Passenger ALL 24 M

5210001−201 STRU Door − External
5210002−202 STRU
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 2
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310000002−01 53−ZL−00−201 General Visual Inspection of the Nose Radome ALL 120 M
5310001−201 STRU − Internal

EFFECTIVITY: ALL
5310000004−01 53−ZL−00−202 General Visual Inspection of the Lower Nose ALL 120 M
Compartment − Internal LH

5310000005−01 53−ZL−00−203 General Visual Inspection of the Lower Nose ALL 60 M

Compartment − Internal RH

5310000006−01 53−ZL−00−204 General Visual Inspection of the Nose Wheel ALL 450 L
Well

5310000009−01 53−ZL−00−205 General Visual Inspection of the Mid Lower ALL 60 M

5320010−201 STRU Fuselage, Slat Drive Compartment − Internal

5310000020−01 53−ZL−00−206 General Visual Inspection of the Fuselage from ALL 60 M

FS781.00 to FS861.00, Below WL71.5 − Internal
MAINTENANCE REVIEW BOARD REPORT

5310000021−01 53−ZL−00−207 General Visual Inspection of the Aft ALL 60 M

Wing−to−Fuselage Fairing − Internal
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5310000032−01 53−ZL−00−208 General Visual Inspection of the Lower ALL 120 M

5330003−202 STRU Mid−Fuselage − External

5310000033−01 53−ZL−00−209 General Visual Inspection of the Main Landing ALL 60 M

5330012−201 STRU Gear Wheel Well

5−23−10
PART 3
5310000034−01 53−ZL−00−210 General Visual Inspection of the Lower ALL 120 M
Mid−Fuselage Between the Pressure Floor and
the Cabin Floor − Internal

Page 3
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310000036−01 53−ZL−00−211 General Visual Inspection of the Center Wing ALL 120 M
Box Lower Surface − External

EFFECTIVITY: ALL
5310000037−01 53−ZL−00−212 General Visual Inspection of the Center Wing ALL 120 M
Box − Internal

5310000081−01 53−ZL−00−213 General Visual Inspection of the Lower Forward ALL 60 M

5320004−201 STRU Fuselage,
5320015−201 STRU
5320016−201 STRU Between FS280.00 and FS557.00 − External, GX
XRS
GL6000
GL6500

Between FS280.00+32.00 and FS557.00 − GL5000

External GV5000
GL5500

5310000082−01 53−ZL−00−214 General Visual Inspection of the Lower Forward ALL 60 M

Fuselage,
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

Between FS280.00 and FS557.00, and GX

Between STR22L and STR22R − Internal, XRS
GL6000
GL6500

Between FS280.00+32.00 and FS557.00, and GL5000

Between STR22L and STR22R − Internal GV5000

5−23−10
PART 3
GL5500

Page 4
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5310000082−02 53−ZL−00−215 General Visual Inspection of the Lower Forward ALL 120 M
Fuselage,

Between FS280.00 and FS557.00, and GX

EFFECTIVITY: ALL
Between STR18L and STR22L, and STR18R XRS
and STR22R − Internal, GL6000
GL6500

Between FS280.00+32.00 and FS557.00, and GL5000

Between STR18L and STR22L, and STR18R GV5000
and STR22R − Internal GL5500

5310000083−01 53−ZL−00−216 General Visual Inspection of the ALL 1800 L

Wing−to−Fuselage Fairings − External

5310020001−01 53−ZL−00−217 General Visual Inspection of the Fuselage Nose ALL 3000 H
5310008−201 STRU Section − External

5320000002−01 53−ZL−00−218 General Visual Inspection of the Nose Section of ALL 60 M

the Forward Equipment Compartment − Internal
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320000004−01 53−ZL−00−219 General Visual Inspection of the Flight ALL 30 M

Compartment

5320000020−01 53−ZL−00−220 General Visual Inspection of the Baggage ALL 60 M

5340001−201 STRU Compartment, Excluding the Baggage Door −
5340002−201 STRU External

5−23−10
PART 3
5320000021−01 53−ZL−00−221 General Visual Inspection of the Electrical ALL 60 M
Power Control−Center − External

Page 5
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5320000021−02 53−ZL−00−222 General Visual Inspection of the Baggage ALL 180 M

Compartment − Internal

EFFECTIVITY: ALL
5320000031−01 53−ZL−00−223 General Visual Inspection of the Mid−Fuselage ALL 120 M
5330003−201 STRU − External

5320000035−01 53−ZL−00−224 General Visual Inspection of the Mid−Fuselage ALL 180 M

Compartment Above the Cabin Floor − Internal

5320000081−01 53−ZL−00−225 General Visual Inspection of the Upper Forward ALL 60 M

5320003−201 STRU Fuselage,
5320004−201 STRU
5320014−201 STRU Between FS280.00 and FS557.00, Excluding GX
5320015−201 STRU the Passenger Door − External, XRS
5320016−201 STRU GL6000
GL6500

Between FS280.00+32.00 and FS557.00, GL5000

Excluding the Passenger Door − External GV5000
GL5500
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5320000082−01 53−ZL−00−226 General Visual Inspection of the Upper Forward ALL 180 M
Fuselage,

Between FS280.00 and FS557.00, Above GX

WL71.50, Excluding the Passenger Door − XRS
Internal, GL6000
GL6500

5−23−10
PART 3
Between FS280.00+32.00 and FS557.00, GL5000
Above WL71.50, Excluding the Passenger Door GV5000
− Internal GL5500

Page 6
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5330000020−01 53−ZL−00−227 General Visual Inspection of the Aft Fuselage − ALL 60 M

5340001−201 STRU External
5340012−201 STRU

EFFECTIVITY: ALL
5330000021−01 53−ZL−00−228 General Visual Inspection of the Aft Fuselage − ALL 30 M
5340012−201 STRU Internal

5330000022−01 53−ZL−00−229 General Visual Inspection of the Tailcone − ALL 60 M

External

5330000023−01 53−ZL−00−230 General Visual Inspection of the Tailcone − ALL 60 M

Internal

5330000024−01 53−ZL−00−231 General Visual Inspection of the Fuselage From ALL 60 M

FS987.50 to the Vertical−Stabilizer Rear−Spar
Datum−Line − Internal

5310000008−01 53−ZL−00−232 General Visual Inspection of the Forward ALL 60 M

Avionics Compartment − Internal LH
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5310000008−02 53−ZL−00−233 General Visual Inspection of the Forward ALL 60 M

Avionics Compartment − Internal RH

5320000083−01 53−ZL−00−234 General Visual Inspection of the Above Floor GL5000 120 M
Avionic Rack Located Between FS281.00+32.00 GV5000
and FS319.06+32.00 GL5500

5−23−10
PART 3
Page 7
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5440000001−01 54−ZL−00−201 General Visual Inspection of the Pylon − LH ALL 60 M

5450001−201 STRU External

EFFECTIVITY: ALL
5440000001−02 54−ZL−00−202 General Visual Inspection of the Pylon − RH ALL 60 M
5450001−201 STRU External
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 8
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5530000001−01 55−ZL−00−201 General Visual Inspection of the Ram Air Intake ALL 120 M
and Dorsal Fairing − Internal

EFFECTIVITY: ALL
5530000002−01 55−ZL−00−202 General Visual Inspection of the Ram Air Dorsal ALL 120 M
Fairing and the Leading Edge of the Vertical
Stabilizer − External

5530000003−01 55−ZL−00−203 General Visual Inspection of the Vertical ALL 60 M

5530001−201 STRU Stabilizer − External LH

5530000003−02 55−ZL−00−204 General Visual Inspection of the Vertical ALL 60 M

5530001−201 STRU Stabilizer − External RH

5530000004−01 55−ZL−00−205 General Visual Inspection of the Vertical ALL 120 M

Stabilizer − Internal

5530000005−01 55−ZL−00−206 General Visual Inspection of the ALL 60 M

Horizontal−Stabilizer Bullet Fairing − External
MAINTENANCE REVIEW BOARD REPORT

5530000006−01 55−ZL−00−207 General Visual Inspection of the Horizontal− ALL 120 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

Stabilizer Bullet Fairing − Internal

5530000007−01 55−ZL−00−208 General Visual Inspection of the Vertical ALL 120 M

Stabilizer Leading Edge − Internal

5530000008−01 55−ZL−00−209 General Visual Inspection of the Leading Edge ALL 60 M

5−23−10
PART 3
of the Rudder − Internal

5530000009−01 55−ZL−00−210 General Visual Inspection of the Rudder − ALL 120 M

External

Page 9
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5530000010−01 55−ZL−00−211 General Visual Inspection of the Horizontal ALL 120 M

Stabilizer − External LH

EFFECTIVITY: ALL
5530000010−02 55−ZL−00−212 General Visual Inspection of the Horizontal ALL 120 M
Stabilizer − External RH

5530000011−01 55−ZL−00−213 General Visual Inspection of the Horizontal ALL 3750 L

Stabilizer Leading−Edge − Internal LH

5530000011−02 55−ZL−00−214 General Visual Inspection of the Horizontal ALL 3750 L

Stabilizer Leading−Edge − Internal RH

5530000013−01 55−ZL−00−215 General Visual Inspection of the Rear Spar of ALL 60 M

the Horizontal Stabilizer − External LH

5530000013−02 55−ZL−00−216 General Visual Inspection of the Rear Spar of ALL 60 M

the Horizontal Stabilizer − External RH
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 10
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5750060003−01 57−ZL−00−201 General Visual Inspection of the Wing Leading ALL 30 M

Edge Slats − External LH

EFFECTIVITY: ALL
5750060003−02 57−ZL−00−202 General Visual Inspection of the Wing Leading ALL 30 M
Edge Slats − External RH

5750060004−01 57−ZL−00−203 General Visual Inspection of the Wing ALL 60 M

Leading−Edge and Slats − Internal LH

5750060004−02 57−ZL−00−204 General Visual Inspection of the Wing ALL 60 M

Leading−Edge and Slats − Internal RH

5750060007−01 57−ZL−00−205 General Visual Inspection of the Wing Between ALL 30 M

5720005−201 STRU WS47.60 and WS178.00 − External LH
5720006−201 STRU

5750060007−02 57−ZL−00−206 General Visual Inspection of the Wing Between ALL 30 M

5720005−201 STRU WS47.60 and WS178.00 − External RH
5720006−201 STRU
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5750060008−01 57−ZL−00−207 General Visual Inspection of the Inboard Wing ALL 120 M
Box − Internal LH

5750060008−02 57−ZL−00−208 General Visual Inspection of the Inboard Wing ALL 120 M
Box − Internal RH

5−23−10
PART 3
5750060009−01 57−ZL−00−209 General Visual Inspection of the Inboard Wing ALL 120 M
Box Between the Auxiliary Spar and the Rear
Spar, Between WS85.50 and WS178.00 −
Internal LH

Page 11
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5750060009−02 57−ZL−00−210 General Visual Inspection of the Inboard Wing ALL 120 M
Box Between the Auxiliary Spar and the Rear
Spar, Between WS85.50 and WS178.00 −
Internal RH

EFFECTIVITY: ALL
5750060010−01 57−ZL−00−211 General Visual Inspection of the Wing Between ALL 60 M
5720005−201 STRU WS178.00 and WS287.00 − External LH
5720006−201 STRU

5750060010−02 57−ZL−00−212 General Visual Inspection of the Wing Between ALL 60 M

5720005−201 STRU WS178.00 and WS287.00 − External RH
5720006−201 STRU

5750060011−01 57−ZL−00−213 General Visual Inspection of the Mid−Wing Box ALL 120 M
− Internal LH

5750060011−02 57−ZL−00−214 General Visual Inspection of the Mid−Wing Box ALL 120 M
− Internal RH
MAINTENANCE REVIEW BOARD REPORT

5750060012−01 57−ZL−00−215 General Visual Inspection of the Wing Between ALL 60 M

BD−700 TIME LIMITS/MAINTENANCE CHECKS

5720005−201 STRU WS287.00 and WS544.00 − External LH

5720006−201 STRU

5750060012−02 57−ZL−00−216 General Visual Inspection of the Wing Between ALL 60 M

5720005−201 STRU WS287.00 and WS544.00 − External RH
5720006−201 STRU

5−23−10
PART 3
5750060013−01 57−ZL−00−217 General Visual Inspection of the Outboard Wing ALL 120 M
Box − Internal LH

Page 12
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5750060013−02 57−ZL−00−218 General Visual Inspection of the Outboard Wing ALL 120 M
Box − Internal RH

EFFECTIVITY: ALL
5750060014−01 57−ZL−00−219 General Visual Inspection of the Inboard Wing ALL 900 L
Between the Auxiliary Spar and the Rear Spar,
Between BL47.60 and WS85.50 − Internal LH

5750060014−02 57−ZL−00−220 General Visual Inspection of the Inboard Wing ALL 900 L
Between the Auxiliary Spar and the Rear Spar,
Between BL47.60 and WS85.50 − Internal RH

5750060015−01 57−ZL−00−221 General Visual Inspection of the Winglet − ALL 60 M

5730003−201 External LH

5750060015−02 57−ZL−00−222 General Visual Inspection of the Winglet − ALL 60 M

5730003−201 External RH

5750060017−01 57−ZL−00−223 General Visual Inspection of the Inboard Flaps − ALL 1800 L
External LH
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5750060017−02 57−ZL−00−224 General Visual Inspection of the Inboard Flaps − ALL 1800 L
External RH

5750060018−01 57−ZL−00−225 General Visual Inspection of the Inboard−Flap ALL 60 M

Actuator Support−Fittings − LH

5−23−10
PART 3
5750060018−02 57−ZL−00−226 General Visual Inspection of the Inboard−Flap ALL 60 M
Actuator Support−Fittings − RH

Page 13
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

5750060019−01 57−ZL−00−227 General Visual Inspection of the Middle Flaps, ALL 60 M

Outboard Flaps and Ailerons − External LH

EFFECTIVITY: ALL
5750060019−02 57−ZL−00−228 General Visual Inspection of the Middle Flaps, ALL 60 M
Outboard Flaps and Ailerons − External RH

5750060020−01 57−ZL−00−229 General Visual Inspection of the Aileron Hinge ALL 60 M

Fittings − LH

5750060020−02 57−ZL−00−230 General Visual Inspection of the Aileron Hinge ALL 60 M

Fittings − RH
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 14
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

7140000001−02 71−ZL−00−201 General Visual Inspection of the Nacelle − RH ALL 3000 H

7140000001−01 71−ZL−00−202 General Visual Inspection of the Nacelle − LH ALL 3000 H

EFFECTIVITY: ALL
7140000023−01 71−ZL−00−203 General Visual Inspection of the Engine − ALL 3000 H
Internal LH

7140000023−02 71−ZL−00−204 General Visual Inspection of the Engine − ALL 3000 H

Internal RH
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 15
Jun 19/2013
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

7840000022−01 78−ZL−00−201 General Visual Inspection of the Thrust ALL 1800 L

783000−201 PROP Reverser − LH
783000−203 PROP
783000−205 PROP

EFFECTIVITY: ALL
7840000022−02 78−ZL−00−202 General Visual Inspection of the Thrust ALL 1800 L
783000−201 PROP Reverser − RH
783000−203 PROP
783000−205 PROP
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−23−10
PART 3
Page 16
Jun 19/2013
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

L/HIRF INSPECTION PROGRAM

1. General

This section provides the basic scheduled inspection tasks and frequencies applicable to the
lightning/high intensity radiated field (L/HIRF) protection.

The intent of the L/HIRF protection maintenance program is to ensure the availability of
L/HIRF protection for each line replaceable unit (LRU) and wiring disconnect within a
specified system.

The L/HIRF maintenance program will involve on−aircraft inspection of L/HIRF protection
termination at LRUs and wiring disconnects for unserviceability resulting from accidental or
environmental deterioration. Wiring runs are considered to be covered within the scope of the
normal Zonal Inspection Program.

MSG−3 (Rev. 2001.1) logic was used to develop the on−wing L/HIRF scheduled maintenance
program.

2. Program Rules

The purpose of the following program rules is to provide standard guidelines for the L/HIRF
maintenance program.

A. During the performance of detailed inspection of L/HIRF protective devices, no

connector or equipment is to be removed that would necessitate subsequent functional
testing.

B. For all wiring and termination points installed within heat shrink or other conduits, the
defined detailed inspection will apply only to the heat shrink or conduit for integrity.

C. The L/HIRF maintenance program addresses only on−aircraft inspections of L/HIRF

protective devices. However, specified LRUs may also incorporate, inside the
equipment, additional protective devices. These internal devices will be subject to
off−aircraft inspection and testing, on an opportunity basis, as per instructions contained
within the LRU manufacturer’s component maintenance manual.

3. List of L/HIRF Significant Items

The following is a list of the L/HIRF significant items.

L/HIRF ANALYSIS TITLE

215000 Avionics Cooling System

221000 Automatic Flight Control System

EFFECTIVITY: ALL
PART 3 Page 1
5−24−00 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

L/HIRF ANALYSIS TITLE

242100 Primary AC Power Supply − GCU

242300 Emergency AC Power Supply − RAT GCU

246200 Electrical Management System − EMS CDU and SPDA

270000 Flight Control System − Flight Control Unit

273200 Stall Protection System

274000 Horizontal Stabilizer Control System

275000 Flaps and Slats Control System − SFCU

284000 Fuel Indicating

301100 Anti−Icing System − Ice Detectors

303100 Air Data Probes and Sensors

304100 Windshield and Side Window Temperature Controller

314200 Data Acquisition System

320000 Landing Gear Control System − LG ECU

324000 Brake Control System − BCU

325000 Nosewheel−Steering Control System

331000 PFD Controller

334000 Exterior Lighting

341100 Air Data Computer System

344500 Inertial Reference System

344400 Radio Altimeter System

345100 VHF Navigation System

361100 Bleed Air System − Bleed Management Controller

491000 Engine Fuel and Control − APU FADEC

732000 Engine Fuel and Control − FADEC

EFFECTIVITY: ALL
PART 3 Page 2
5−24−00 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

L/HIRF ANALYSIS TITLE

740000 Engine Ignition

751000 Engine Anti−Icing

761000 Engine Power Control

801100 Engine Starting

4. Tasks and Intervals Table Format

The table in section 5−24−10 provides a list of the L/HIRF program tasks. Data about the
tables used in section 5−24−10 is given below:

MSG−3 Route Chapter 5 Task Title Program Task Interval

Task No. Task No.

A. MSG−3 Task No. Column

This column lists all MSG−3 task numbers from the L/HIRF analysis.

The task numbers are of the form XXXXXXXX−YZZ for L/HIRF tasks.
− XXXXXXXX is the system ATA number.
− YZZ is the task sequence identifier that starts at 201 for all different ATA numbers.

The format for avionics, systems and powerplant tasks, structures tasks and zonal tasks
are defined in sections 5−21−00, 5−22−00 and 5−23−00 respectively.

B. Route Column

Not applicable for L/HIRF tasks.

C. Chapter 5 Task No. Column

This column shows the Chapter 5 task number that corresponds to the MSG−3 task
number in column 1. Chapter 5 task numbers are XX−XX−XX−YZZ where:
− XX−XX−XX is the ATA Chapter number
− Y is 2 if the source data was MSG−3 analysis
− ZZ is the task sequence identifier that starts at 01 for all different ATA numbers.

EFFECTIVITY: ALL
PART 3 Page 3
5−24−00 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

D. Task Title Column

This column shows the task title. This title includes the inspection level and a brief
description of the area or items to be inspected.

E. Program Column

This column shows the Global model variant to which the task applies.

F. Task Interval Column

This column shows the intervals for the task. The interval is measured from the last time
that the task was done. The task interval is measured in months (M).

EFFECTIVITY: ALL
PART 3 Page 4
5−24−00 Jan 29/2016
 BD−700 TIME LIMITS/MAINTENANCE CHECKS
MAINTENANCE REVIEW BOARD REPORT

PART 3
SECTION 5−24−10

L/HIRF INSPECTION PROGRAM

EFFECTIVITY: ALL
PART 3 Cover
5−24−10 Jan 29/2016
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

32730740−201 32−43−53−201 General Visual Inspection of the L/HIRF ALL 120 M

Protection of the Wheel Speed Transducers
Connectors

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 1
Jan 29/2016
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

33540640−201 33−00−00−201 General Visual Inspection of the L/HIRF ALL 120 M

Protection of the Wing Tip Lights and
Components Connectors and Ground Studs

EFFECTIVITY: ALL
33510610−201 33−41−01−201 General Visual Inspection of the L/HIRF ALL 120 M
Protection of the Wing Landing and Taxi Lights
Connectors

33140000−201 33−43−09−201 General Visual Inspection of the L/HIRF ALL 120 M

Protection of the Lower Strobe/Anticollision Light
Connector
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 2
Jan 29/2016
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

34440000−201 34−44−05−201 General Visual Inspection of the L/HIRF ALL 60 M

Protection of the Radio Altimeter Antennas
Connectors

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 3
Jan 29/2016
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

22220000−201 53−10−00−212 General Visual Inspection of the L/HIRF ALL 120 M

24220000−201 Protection of the Flight Compartment
24220000−202 Connectors
27220000−201

EFFECTIVITY: ALL
27220000−202
27220000−203
30220000−201
32220000−201
33220000−201
34220000−201
34220000−202

27210000−201 53−10−00−213 General Visual Inspection of the L/HIRF ALL 180 M

30210000−201 Protection on the Forward Face of the Forward
Pressure Bulkhead Connectors,

FS202.00, GX
XRS
GL6000
GL6500
MAINTENANCE REVIEW BOARD REPORT

FS202.00+32.00 GL5000
BD−700 TIME LIMITS/MAINTENANCE CHECKS

GV5000
GL5500

5−24−10
PART 3
Page 4
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

22230000−201 53−20−00−245 Detailed Inspection of the L/HIRF Protection of GL5000 120 M

27230000−201 the Avionics Racks Connectors GV5000
27230000−202 GL5500
27230000−203

EFFECTIVITY: ALL
28230000−201
31230000−201
32230000−201
34230000−201
34230000−202
34230000−203
34230000−204

27140000−201 53−20−00−246 Detailed Inspection of the Ground Studs for ALL 120 M
L/HIRF Protection in the Lower Forward
Fuselage,

Between FS280.00 and FS557.00, GX

XRS
GL6000
GL6500
MAINTENANCE REVIEW BOARD REPORT

Between FS280.00+32.00 and FS557.00 GL5000

BD−700 TIME LIMITS/MAINTENANCE CHECKS

GV5000
GL5500

5−24−10
PART 3
Page 5
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

22310000−201 53−40−00−217 General Visual Inspection of the L/HIRF ALL 60 M

24310000−201 Protection on the Aft Face of the Aft Pressure
27310000−201 Bulkhead Connectors − FS861.00
27310000−202

EFFECTIVITY: ALL
27310000−203
28310000−201
34310000−201
34310000−202
36310000−201
49310000−201
73310000−201
74310000−201
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 6
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

24410420−201 54−50−01−201 Detailed Inspection of the L/HIRF Protection of ALL 120 M

34410420−201 the Engine Pylons Connectors
36410420−201
73410420−201

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 7
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

73430440−202 71−00−00−201 Detailed Inspection of the L/HIRF Protection of ALL 120 M

the Engine Components Electrical Connectors

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 8
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

73430440−201 73−21−05−201 Detailed Inspection of the L/HIRF Protection of ALL 120 M

the T20/P20 Sensors Connectors

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 9
May 31/2019
 MSG−3 Task No. Route Chapter 5 Task No. Task Title Program Task Interval

73430440−203 78−30−00−206 Detailed Inspection of the L/HIRF Protection of ALL 120 M

the Thrust Reversers Electrical Connectors

EFFECTIVITY: ALL
MAINTENANCE REVIEW BOARD REPORT
BD−700 TIME LIMITS/MAINTENANCE CHECKS

5−24−10
PART 3
Page 10
May 31/2019