C-212-400 MAINTENANCE MANUAL
TO HOLDERS OF MAINTENANCE MANUAL
ORIGINAL ISSUE JANUARY 01/98
REVISION NO. 25 DATED JUN. 15/18
HIGHLIGHTS
1. General.
This revision is only applicable to the chapters:
06 - DIMENSIONS AND AREAS
22 - AUTO-FLIGHT
23 - COMMUNICATIONS
27 - FLIGHT CONTROL SYSTEM
31 - INDICATING AND RECORDING SYSTEM
32 - LANDING GEAR
34 - NAVIGATION
38 - WATER/WASTE
52 - DOORS
53 - FUSELAGE
55 - STABILIZERS
57 - WINGS
61 - PROPELLERS
71 - POWERPLANT
73 - ENGINE FUEL AND CONTROL
79 - OIL SYSTEM
2. Description of the Revision.
N, R or D, in the STATUS column, gives the pages or the section or the
chapters which are New, Revised or Deleted, respectively.
Insert, replace or remove the indicated pages, sections or chapters and
make an entry of Revision No. 25 dated Jun. 15/18 in the Record of Revision
Sheet.
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
TITLE PAGE R To include Rev.25
SERVICE BULLETIN LIST R To include Service Bulletins
(SBL)
06 LEP R To include Rev.25
Effectivity: EE92
HIGHLIGHTS Pag. 1 of 7
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
06 TOC R To include Rev.25
06-41-51 1 001 R Amendment
06-41-53 001 R Amendment
22 LEP R To include Rev.25
22 TOC R To include Rev.25
22-15-51 30 401 N To include a new
Removal/Installation procedure
for the EE92 aircraft version
22-15-53 30 401 N To include a new
Removal/Installation procedure
for the EE92 aircraft version
22-15-55 30 401 N To include a new
Removal/Installation procedure
for the EE92 aircraft version
22-15-57 30 401 N To include a new
Removal/Installation procedure
for the EE92 aircraft version
23 LEP R To include Rev.25
23 TOC R To include Rev.25
23-12-00 30 501 N To include a new Adjustment/Test
Configuration for the EE92
aircraft version
23-31-00 30 501 R Improvement
23-51-00 30 501 R Improvement
23-71-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
27 LEP R To include Rev.25
27 TOC R To include Rev.25
27-51-55 30 401 N To include a new
Removal/Installation procedure
for the EE92 aircraft version
Effectivity: EE92
HIGHLIGHTS Pag. 2 of 7
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
31 LEP R To include Rev.25
31 TOC R To include Rev.25
31-00-00 001 R Amendment
31-31-00 30 001 N To include a new System
Configuration for the EE92
aircraft version
31-31-00 30 101 N To include a new System
Configuration for the EE92
aircraft version
31-51-00 101 R Amendment
32 LEP R To include Rev.25
32 TOC R To include Rev.25
32-20-00 401 R Amendment. To include the RFC
30-844BB-2017-MR-00079
32-44-00 101 R Amendment
32-50-00 101 R Amendment
34 LEP R To include Rev.25
34 TOC R To include Rev.25
34-22-20 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
34-26-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
34-27-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
34-41-00 30 501 R Improvement
34-42-00 30 501 N To include a new Adjustment/Test
for the EE92 aircraft version
34-45-00 30 301 N To include a new System
Effectivity: EE92
HIGHLIGHTS Pag. 3 of 7
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
Configuration for the EE92
aircraft Version
34-45-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
34-46-00 30 001 N To include a new
Description/Operation procedure
for the EE92 aircraft version
34-46-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
34-51-10 30 501 R Improvement
34-52-00 30 501 R Improvement
34-53-00 30 501 R Improvement
34-54-10 30 501 R Improvement
34-61-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
38 LEP R To include Rev.25
38 TOC R To include Rev.25
38-30-00 701 R Amendment
52 LEP R To include Rev.25
52 TOC R To include Rev.25
52-10-11 401 R Amendment
52-10-12 401 R Amendment
52-10-13 401 R Amendment
52-10-20 401 R Amendment
52-10-21 401 R Amendment
52-10-22 401 R Amendment
52-10-23 401 R Amendment
Effectivity: EE92
HIGHLIGHTS Pag. 4 of 7
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
52-20-20 401 R Amendment
52-20-21 401 R Amendment
52-30-10 401 R Amendment
52-30-11 401 R Amendment
52-30-20 401 R Amendment
52-30-40 101 R Amendment
52-30-40 501 R Amendment
52-71-00 30 001 N To include a new
Description/Operation procedure
for the EE92 aircraft version
52-71-00 30 501 N To include a new Adjustment/Test
procedure for the EE92 aircraft
version
52-71-14 30 401 R Amendment
52-71-15 30 401 R Amendment
53 LEP R To include Rev.25
53 TOC R To include Rev.25
53-00-00 001 R Amendment
53-10-00 001 R Amendment
53-50-00 001 R Amendment
55 LEP R To include Rev.25
55 TOC R To include Rev.25
55-10-01 401 R Amendment
55-20-01 401 R Amendment
55-30-01 401 R Amendment
55-40-01 401 R Amendment
57 LEP R To include Rev.25
Effectivity: EE92
HIGHLIGHTS Pag. 5 of 7
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
CHAP./SEC./SUB./CONF./P.B. STATUS REASON FOR CHANGE
57 TOC R To include Rev.25
57-10-00 401 R Amendment
57-20-00 2 401 R Amendment
57-20-10 401 R Amendment
57-30-00 401 R Amendment
57-40-00 601 R Amendment
61 LEP R To include Rev.25
61 TOC R To include Rev.25
61-10-00 601 R Amendment
61-21-00 101 R Amendment
61-40-01 401 R Amendment
71 LEP R To include Rev.25
71 TOC R To include Rev.25
71-00-00 401 R Amendment
71-10-01 401 R Amendment
71-10-02 401 R Amendment
71-20-00 601 R Amendment
71-20-11 401 R Amendment
73 LEP R To include Rev.25
73 TOC R To include Rev.25
73-23-00 101 R Amendment
73-23-01 401 R Amendment
79 LEP R To include Rev.25
79 TOC R To include Rev.25
79-21-00 101 R Amendment
79-21-00 601 R Amendment
Effectivity: EE92
HIGHLIGHTS Pag. 6 of 7
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C-212-400 MAINTENANCE MANUAL
INTENTIONALLY LEFT BLANK
Effectivity: EE92
HIGHLIGHTS Pag. 7 of 7
Jun. 15/18
C-212-400 AIRCRAFT
MAINTENANCE MANUAL
VERSIONS: EE92
The content of this document is the property of AIRBUS DEFENCE AND SPACE, S.A.U.
It is supplied in confidence and commercial security on its contents must be maintained.
This document not be used for any purpose other than for which it is supplied, nor may
information contained in it be disclosed to unauthorized persons. It must not be repro-
duced in whole or in part without permission in writing from the owners of the copyright.
Requests for reproduction of any data in this document and the media authorized for it
must be addressed to AIRBUS DEFENCE AND SPACE, S.A.U.
© AIRBUS DEFENCE AND SPACE, S.A.U. 2017. All rights reserved.
AIRBUS DEFENCE AND SPACE, S.A.U.
Avenida de Aragón 404, 28022 Madrid, SPAIN
System Support Services
Technical Information and Data
Fax (34) 954-59-3623
E-mail = MTA.MSI.Support.Documentation.Services@airbus.com
Original issue: JANUARY 01/98
Revision 25, JUN. 15/18
Printed in Spain
C-212-400 MAINTENANCE MANUAL
RECORD OF REVISIONS
INSERTED INSERTED
REV. ISSUE DATE REV. ISSUE DATE
No. DATE BY No. DATE BY
000 Jan. 01/98 CASA 023 Jun. 15/17 CASA
001 Dec. 15/98 CASA 024 Dec. 15/17 CASA
002 Mar. 30/99 CASA 025 Jun. 15/18 CASA
003 Jul. 31/00 CASA
004 Nov. 15/00 CASA
005 Dec. 15/00 CASA
006 Sep. 15/01 CASA
007 Mar. 31/03 CASA
008 Nov. 01/03 CASA
009 Feb. 29/04 CASA
010 Apr. 30/10 CASA
011 Jul. 15/11 CASA
012 Dec. 15/11 CASA
013 Jun. 15/12 CASA
014 Dec. 15/12 CASA
015 Jun. 15/13 CASA
016 Dec. 15/13 CASA
017 Jun. 15/14 CASA
018 Dec. 15/14 CASA
019 Jun. 15/15 CASA
020 Dec. 15/15 CASA
021 Jun. 15/16 CASA
022 Dec. 15/16 CASA
REC.REV.
C-212-400 MAINTENANCE MANUAL
RECORD OF TEMPORARY REVISIONS
REV. CHAP/SECT/SUBJ ISSUE INSERTED REMOVED INCORPORATED
INTO MANUAL
No. P. BLOCK DATE DATE BY DATE BY BY REV. No.
Keep this record at the first pages of the Manual just after the standard
revisions record. When Temporary Revisions are received, insert them into the
Manual and make the appropiate entries in this record.
R.T.REV.
C-212-400 MAINTENANCE MANUAL
SERVICE BULLETINS LIST
SERVICE INCORPORATED SERVICE INCORPORATED
BULLETIN REV. INTO MANUAL BULLETIN REV. INTO MANUAL
No. No. REV.No./DATE No. No. REV.No./DATE
212-11-07 0 NO EFFECT 212-32-19 0 NO EFFECT
212-23-12 0 NO EFFECT 212-32-19 2 NO EFFECT
212-23-12 1 NO EFFECT 212-32-21 2 NO EFFECT
212-24-64 0 NO EFFECT 212-32-22 2 NO EFFECT
212-24-64 1 NO EFFECT 212-32-29 1 NO EFFECT
212-24-64M 1 NO EFFECT 212-32-29M 1 NO EFFECT
212-24-65 1 NO EFFECT 212-32-38 0 NO EFFECT
212-24-65M 0 NO EFFECT 212-32-38M 0 NO EFFECT
212-24-65M 1 NO EFFECT 212-32-40 0 NO EFFECT
212-25-75M 0 Rev. 1, Dec. 15/98 212-32-40M 0 NO EFFECT
212-27-12 3 NO EFFECT 212-33-24 1 NO EFFECT
212-27-13 1 NO EFFECT 212-33-24M 1 NO EFFECT
212-27-14 0 NO EFFECT 212-34-105 0 Rev. 25, Jun. 15/18
212-27-15 1 NO EFFECT 212-34-44 0 NO EFFECT
212-27-19 1 NO EFFECT 212-34-44M 0 NO EFFECT
212-27-21 1 NO EFFECT 212-38-01 2 NO EFFECT
212-27-22 3 NO EFFECT 212-53-30 0 NO EFFECT
212-27-23 1 NO EFFECT 212-53-33 0 NO EFFECT
212-27-24 2 NO EFFECT 212-57-16 1 NO EFFECT
212-27-26 0 NO EFFECT 212-57-19 0 NO EFFECT
212-27-36 0 NO EFFECT 212-57-30 0 NO EFFECT
212-27-47M 0 NO EFFECT 212-57-30 1 NO EFFECT
212-27-47M 1 NO EFFECT 212-57-30M 2 NO EFFECT
212-27-48 0 NO EFFECT 212-61-05M 1 NO EFFECT
212-27-48M 0 NO EFFECT 212-71-06 0 NO EFFECT
212-28-11 3 NO EFFECT 212-72-05 0 NO EFFECT
212-28-18 3 NO EFFECT 212-72-05 1 NO EFFECT
212-28-19 3 NO EFFECT 212-72-05 2 NO EFFECT
212-28-21 0 NO EFFECT 212-72-05 3 NO EFFECT
212-28-22M 1 NO EFFECT 212-72-05 4 NO EFFECT
212-28-22M 2 NO EFFECT 212-79-01 0 NO EFFECT
212-30-22 2 Rev. 19, Jun. 15/15 212-79-03 2 NO EFFECT
212-30-22M 1 Rev. 19, Jun. 15/15 212-79-04 0 NO EFFECT
212-31-07 0 NO EFFECT 212-80-33M 0 NO EFFECT
212-32-17 2 NO EFFECT
S.B.L. Pag. 1
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C-212-400 MAINTENANCE MANUAL
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S.B.L. Pag. 2
Jun. 15/18
C-212-400 MAINTENANCE MANUAL
INTRODUCTION
1. General
This manual has been prepared generally in accordance with ATA
Specification 100.
2. Content
This manual contains information on systems and units of equipment to the
level required to service the aircraft, to understand and maintain the
systems to a safe standard, and to remove and install units of the systems.
Servicing instructions of units removed from the aircraft are contained in
the relevant Component Maintenance Manual.
3. Using the Manual
A. Chapterization
Chapters are allocated in accordance with ATA Specification 100.
B. Chapter Breakdown
Each chapter is broken down into sections:
Example:
30-00-00 Ice and Rain Protection
30-10-00 Airfoil De-Icing
30-20-00 Air Intakes
30-30-00 Pitot and Static Ice Protection
Each section is broken down into subsections or subsystems:
Example:
30-30-00 Pitot and Static Ice Protection
30-31-00 Pitot-Probe-Ice protection
30-32-00 Angle-of-Attack Sensor-Ice Protection
Effectivity: All
INTRO Pag. 1
Jun. 15/15
C-212-400 MAINTENANCE MANUAL
Each subsection is divided into subjects:
Example:
30-11-11 De-Icer Boots
30-11-12 Water Separator
30-11-13 Regulator Valve
Descriptive and maintenance information for the complete system is
contained in the pages bearing the first element number only
(30-00-00). Where a system is broken down into subsystems, descriptive
and maintenance information for the subsystem will be found on the
pages bearing the first and second element number (30-11-00).
Removal and installation information of units within a system will be
found on the pages bearing all three element numbers (30-11-11).
C. Tab Dividers
The manual is separated into chapters with yellow tab dividers, each
divider indicating the corresponding chapter number and title.
D. Page Numbers
Page numbers blocks are allocated for different topics, the pages being
numbered consecutively:
Pages 1 thru 99 - Description and Operation
Pages 101 thru 199 - Troubleshooting
Pages 201 thru 299 - Maintenance Practices
Pages 301 thru 399 - Servicing
Pages 401 thru 499 - Removal/Installation
Pages 501 thru 599 - Adjustment/Test
Pages 601 thru 699 - Inspection/Check
Pages 701 thru 799 - Cleaning/Painting
Pages 801 thru 899 - Approved Repairs
As no one block of page numbers if fully used, and some page blocks
will not be used at all, the page numbering for a topic will have
unused page block numbers in the sequence.
Effectivity: All
INTRO Pag. 2
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C-212-400 MAINTENANCE MANUAL
E. Figure Numbers
Figures are numbered consecutively within each chapter, the figure
numbers reflecting the topic:
Description and Operation - Figures 1, 2, 3, etc.
Troubleshooting - Figures 101, 102, 103, etc.
Maintenance Practices - Figures 201, 202, 203, etc.
Servicing - Figures 301, 302, 303, etc.
Removal/Installation - Figures 401, 402, 403, etc.
Adjustment/Test - Figures 501, 502, 503, etc.
Inspection/Check - Figures 601, 602, 603, etc.
Cleaning/Painting - Figures 701, 702, 703, etc.
Approved Repairs - Figures 801, 802, 803, etc.
F. List of Effective Pages
The List of Effective Pages located at the front of each chapter can be
used to check the completeness of the chapter and the latest issue of
the pages. The data against each page should correspond to the date on
the relevant page within the chapter.
G. Table of Contents
The Table of Contents located after the List of Effective Pages can be
used to rapidly locate a particular section or subject and to determine
the effectivity of the same against different aircraft types.
H. Effectivity
The system to indicate the effectivity of each topic is as follows:
each page has a "See TOC" indication at its bottom to forward the
reader to the Table of Contents. When a determined page is applicable
to a specific aircraft, the version designation of this aircraft is
indicated at the bottom of the page.
To cover the differences of configuration among aircraft versions in
the topics, the codes CONFIG.1, CONFIG.2, etc, are used.
Refer to the INTRODUCTION ANNEX II, Aircraft Series, for the
cross-reference among the versions designation, CASA serial numbers and
the aircraft serial numbers.
Effectivity: All
INTRO Pag. 3
Jun. 15/15
C-212-400 MAINTENANCE MANUAL
J. Equipment and Materials
The table of "Equipment and Material" of a topic includes:
- The special tools and equipment necessary to do the maintenance task.
When the related tool or equipment is included in the Illustrated
Tools and Equipment Manual, it is identified with the location number
in this manual. The location number is as follows: ITEM xx-xx-xx.
- The consumable materials necessary to do the maintenance task. When
the related consumable material is included in the Consumable Material
List, it is indicated with the identification number in this list. The
identification number is as follows: Z-xx.xxx.
4. Units of Measurement
The measurements used in the manual are expressed as International System
of Units (SI) units followed by an Imperial Measurement Conversion. Where a
measurement, for example pressure, is read on an instrument installed to
the aircraft, only the units of measurement marked on the instrument face
are given. Some examples and explanation of the abbreviations used are:
Distance: meters (feet) expressed as: m (ft)
centimeters (inches) expressed as: cm (in)
Weight: kilograms (pounds) expressed as: kg (lb)
Volume: liters (U.S. gallons) expressed as: l (US gal)
liters (U.S. pints) expressed as: l (US pt)
cubic centimeters (cubic inches) expressed as: cc
(cu in)
Torque: Newton meters (pounds force inches) expressed as:
Nm (lbf.in)
Meter Deca-Newtons (pounds force feet) expressed
as: mdaN (lbf.ft)
Pressure: Kilograms per square centimeter (pounds per
square inch) expressed as: kg/sq cm (lb/sq in)
5. List of Abbreviations
Refer to the INTRODUCTION ANNEX I for the list of abbreviations used in
this manual, arranged in alphabetic order.
Effectivity: All
INTRO Pag. 4
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C-212-400 MAINTENANCE MANUAL
INTRODUCTION
ANNEX I
LIST OF ABBREVIATIONS
A ...................... AMPERE
AC . . . . . . . . . . . . . . . . . . . . .
Effectivity: All
INTRO ANNEX I
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Effectivity: All
INTRO ANNEX I
Pag. 2
Apr. 30/10
C-212-400 MAINTENANCE MANUAL
INTRODUCTION
ANNEX II
AIRCRAFT SERIES
SERIAL NUMBER VERSION SERIAL NUMBER VERSION
SERIES 400
486 ...................... 0001 ...................... EE92 -01 MILITARY
487 ...................... 0002 ...................... EE92 -02 MILITARY
488 ...................... 0003 ...................... EE92 -03 MILITARY
Effectivity: All
INTRO ANNEX II
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Effectivity: All
INTRO ANNEX II
Pag. 2
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C-212-400 MAINTENANCE MANUAL
GENERAL INFORMATION - LIST OF CHAPTERS
EE92
Date
06 - DIMENSIONS AND AREAS Jun. 15/18
07 - LIFTING AND SHORING Jun. 15/17
08 - LEVELING AND WEIGHING Jul. 31/00
09 - TOWING AND TAXIING Dec. 15/13
10 - PARKING AND MOORING Jul. 31/00
11 - PLACARDS AND MARKINGS Jun. 15/17
12 - SERVICING Jun. 15/17
20 - STANDARD PRACTICES Dec. 15/16
21 - AIR CONDITIONING Jun. 15/17
22 - AUTO-FLIGHT Jun. 15/18
23 - COMMUNICATIONS Jun. 15/18
24 - ELECTRICAL POWER Dec. 15/14
25 - EQUIPMENT/FURNISHING Jun. 15/17
26 - FIRE PROTECTION Jun. 15/17
27 - FLIGHT CONTROL SYSTEM Jun. 15/18
28 - FUEL SYSTEM Jun. 15/17
29 - HYDRAULIC POWER Jun. 15/17
30 - ICE AND RAIN PROTECTION Jun. 15/17
31 - INDICATING AND RECORDING SYSTEM Jun. 15/18
32 - LANDING GEAR Jun. 15/18
33 - LIGHTS Dec. 15/17
34 - NAVIGATION Jun. 15/18
35 - OXYGEN SYSTEM Jun. 15/17
36 - PNEUMATICS Jul. 31/00
38 - WATER/WASTE Jun. 15/18
52 - DOORS Jun. 15/18
53 - FUSELAGE Jun. 15/18
55 - STABILIZERS Jun. 15/18
56 - WINDOWS Nov. 15/00
57 - WINGS Jun. 15/18
61 - PROPELLERS Jun. 15/18
71 - POWERPLANT Jun. 15/18
73 - ENGINE FUEL AND CONTROL Jun. 15/18
74 - IGNITION Feb. 29/04
75 - AIR Jul. 31/00
76 - ENGINE CONTROLS Jul. 15/11
77 - ENGINE INDICATING Dec. 15/14
78 - EXHAUST Jun. 15/17
79 - OIL SYSTEM Jun. 15/18
80 - STARTING Dec. 15/11
L.O.C. Page 1
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