Rosemount Aerospace Inc.

14300 Judicial Road

Burnsville, MN 55306-4898
Tel: 952 892 4000
Fax: 952 892 4800
www.goodrich.com

SUPPLEMENTAL INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

FOR

ROSEMOUNT AEROSPACE INC.

COCKPIT DOOR SURVEILLANCE SYSTEM

INSTALLED IN

BOEING 737-300/-400/-500 SERIES AIRCRAFT

STC ST00971SE-D

D2002-256 Revision E

Prepared by Tim Schreiner, Product Support Date 16 April 2009

Approved by Joe Fanska, Design Engineering

Approved by Tim Schreiner, Product Support

Approved by Configuration Management*

* This document is ONLY valid if the configuration management “APPROVED” stamp is applied.

Controlled electronic approvals are on file and available for review:

Reference Change Order # CO-016907

TRANSMITTAL OF TECHNICAL DATA

THESE COMMODITIES, TECHNOLOGY OR SOFTWARE ARE CONTROLLED
BY THE U.S. EXPORT ADMINISTRATION REGULATIONS (EAR),
DIVERSION CONTRARY TO U.S. LAW IS PROHIBITED.
ECCN: 7E994

The information contained in this report is the sole property of, and is proprietary to Rosemount Aerospace Inc. Disclosure, reproduction,
or use requires permission in writing from Rosemount Aerospace Inc.
 REVISIONS

Rev. Ltr Description Date Approval

NEW Original Release 15Oct02 Tim Hughes
Updated Title Page and corrected typo in title.
Updated List of Effective Pages
Updated Table of Contents: Specifically
• Deleted Appendix D because the D2002-247 Supplemental
Maintenance Manual is actually a separate, stand-alone
document.
• Added Appendix E’s page number.
A 17Feb03 Tim Hughes
Updated References Page: Specifically
• Re-formatted table.
• Update D2002-267 IPC Supplement to revision dated
03Jan03.
• Added NOTE 1 and NOTE 2.
Deleted reference to Appendix D from paragraph 2.1.
Revised paragraph 2.5 to callout D2002-267 IPC supplement.
Changed document title to refer to STC number in lieu of DAS
project number.
Updated List of Effective Pages.
Updated Table of Contents.
Made the following References page changes:
• Added drawing 2003-041
• Added document D2003-098
Added System Active Indicator to paragraph 1.
B Changed basis for ICA in paragraph 2 to Boeing MPD. 16Apr03 Tim Hughes
Added Wire Diagram Manual to paragraph 2.
Changed verbiage throughout from “British Airways” to “the
Operator.”
Added maintenance requirements for CDSS Installation 2002-
180-2 to Appendix C.
Deleted Appendix D - Zone Diagram because CDSS has no
effect on zones. Changed para. 3. text to say the same.
Re-numbered pages.
Re-numbered appendices.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page ii

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or use requires permission in writing from Rosemount Aerospace Inc.
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 REVISIONS

Rev. Ltr Description Date Approval

Revised page numbering.
Updated List of Effective Pages.
Updated Table of Contents.
Made the following References page changes:
C • Updated revision of AMM Suppl D2002-247 from A to B. 12May03 Tim Hughes
Revision due to addition of sleep-mode test.
• Updated revision of WDM Suppl D2003-098 from New to
A. Revision due to addition of –3 Wire Diagram.
Added maintenance requirements for CDSS Installation 2002-
180-2 to Appendix C.
Made the following References page changes:.
D • Updated revision of IPC Suppl D2002-267 from B to C. 09Jul03 Tim Hughes
Revision due to addition of Hinge Cover.
Revised cover sheet title and removed previous document
owner. Added Goodich/Rosemount Aerospace Inc header and
E new electronic signature info. Added EAR text on all pages. 06Mar09 See Title Page
Revised propriety info and update revisions on all pages.
Updated structural repair information contact info.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page iii

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
 LIST OF EFFECTIVE PAGES

Page Rev.
Title Page E
i E
ii E
iii E
iv E
v E
vi E
1 E
2 E
3 E
A.1 E
A.2 E
A.3 E
A.4 E
A.5 E
A.6 E
B.1 E
C.1 E

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page iv

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 TABLE OF CONTENTS

Item Page
Title Page Title Page
Revisions i - ii
List of Effective Pages iii
Table of Contents Iv
References v
1. Introduction and Description 1
2. Inspection Requirements 2
3. Dimensions and Access 3
4. Lifting and Shoring 3
5. Leveling and Weighing 3
6. Towing and Taxiing 3
7. Parking and Mooring 3
8. Placards and Marking 3
9. Servicing 3
10. Limitations 3
Appendix A - ICAW Checklist A.1 – A.5
Appendix B - MMEL/MEL B.1
Appendix C - Maintenance Schedule C.1

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page v

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 REFERENCES

Number Rev Date Title

Master Data List, Cockpit Door Surveillance System (CDSS),
2002-180 NOTE 1 NOTE 1
Boeing 737-300/-400/-500, DAS STC Project Number DAS90142
2002-190 NOTE 2 NOTE 2 Wiring Diagram
2002-194 NOTE 2 NOTE 2 Wire Routing
2002-195 NOTE 2 NOTE 2 Electrical Installation
2003-041 NOTE 2 NOTE 2 Electrical Installation
British Airways, Maintenance Programme Boeing 737-
ATP No. 2819 n/a 31Aug01
300/400/500
Cockpit Door Surveillance System (CDSS), Supplemental
D2002-247 B 12May03
Maintenance Manual, Boeing 737-300, 400, 500
Cockpit Door Surveillance System (CDSS), Supplemental
D2002-267 C 09Jul03
Illustrated Parts Catalog Boeing 737-300, 400, 500
Cockpit Door Surveillance System (CDSS), Supplemental Wire
A 12May03
D2003-098 Diagram Manual, Boeing 737-300, 400, 500
Boeing 737-300/-400/-500 Maintenance Planning Data
D6-38278 n/a Nov00
Document
D6-54446 n/a 01Aug96 Boeing Standard Wiring Practices Manual
NOTE 1: Revision Level and Date per Supplemental Type Certificate Number ST00971SE-D.
NOTE 2: Revision Level, Date and full Title per Master Data List 2002-180.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page vi

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
1. INTRODUCTION AND DESCRIPTION
1.1. This document presents supplemental Instructions for Continued Airworthiness (ICA) for STC
ST00971SE-D (ref. DAS 9 NM STC project 90142).
1.1.1. The data referenced in this document demonstrates compliance with the requirements of FAR
25.1529, Amendment 25-54 and Appendix H to Part 25 for the components added by this
modification. Revisions to this ICA will be recorded under the Revisions Page and the List of
Effective Pages will be updated accordingly. All revisions of this ICA must be submitted to the
FAA for acceptance prior to being distributed.
1.1.2. Changes to this document or to the data referenced in this document shall be disseminated
within 14 days after acceptance by the FAA to the Operator of the modified aircraft to ensure
continued safe operation and maintenance.
1.2. This Cockpit Door Surveillance System (CDSS) consists of three cameras in the forward cabin near the
flight deck door, one video monitor on the aft bulkhead of the cockpit, a control panel and the
associated wiring to connect these components together (see Figure 1). Some CDSS Systems include
a System Active Indicator, which is mounted in the ceiling panel adjacent to the R1 Door Camera. The
CDSS is directly connected to a non-essential bus (DC2) and isolated by a 2.5 amp circuit breaker. It
is independent from all other aircraft systems.
CAMERAS
SYSTEM ACTIVE
INDICATOR (if installed)

LCD MONITOR

CONTROL PANEL

Figure 1 – General Layout

CAMERA1

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page 1

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
1.3. Interior Modifications:
• Installation of one Camera in the lowered ceiling panel just aft of the flight deck door.
• Installation of one Camera in Door 1 LH over door lining.
• Installation of 1 Camera in Door 1 RH over door lining and, in some CDSS systems, a System
Active Indicator installed in the vicinity of this Camera.
• Installation of 1 Liquid Crystal Display monitor mounted on the inboard corner of the P6 circuit
breaker panel.
• Installation of a control panel in the center aisle stand, consisting of a master power switch and a
camera selection switch. Lighted switches will be installed on the control panel and will be
controlled by the existing lighting system.

2. INSPECTION REQUIREMENTS
2.1. The instructions for inspection and maintenance requirements for this STC are specified in Appendix C.
These requirements have been derived from the inspection and maintenance program detailed in the
Boeing Maintenance Planning Data (MPD) Document D638278.
2.2. Control and Operation Information
2.2.1. Refer to Aircraft Maintenance Manual (AMM) supplement D2002-247.
2.3. Component Maintenance
2.3.1. For servicing of individual components, contact the following:
Rosemount Aerospace Corporation
14300 Judicial Road
Burnsville, MN 55306-4898
USA
Tel. (952) 892-4000
Note: Rosemount Aerospace Corporation is also known as Goodrich Corporation, Sensors and Integrated
Systems Division.
2.3.2. For trouble shooting, remove and replace instructions, see AMM supplement D2002-247.
2.4. Structural Repair Information
2.4.1. Contact Rosemount Aerospace Inc. for any structural repair information associated with this
modification.
Rosemount Aerospace Inc.
14300 Judicial Road
Burnsville. MN 55306-4898
USA
Tel. (952) 892-4000
2.5. Aircraft Maintenance Manuals (AMM)
2.5.1. Refer to AMM supplement D2002-247.
2.6. Illustrated Parts Catalog (IPC)
2.6.1. Refer to IPC supplement D2002-267.
2.7. Wiring Diagram Manual (WDM)
2.7.1. Refer to WDM supplement D2003-098.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page 2

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
3. DIMENSIONS AND ACCESS ZONE DIAGRAMS
3.1. There are no changes to the zone or area descriptions in Boeing MPD D6-38278 as a result of this
modification.

4. LIFTING AND SHORING

4.1. There are no changes to the lifting and shoring procedures or manuals as a result of this modification.

5. LEVELING AND WEIGHING

5.1. Weight and moment change for this installation will be provided to the Operator for incorporation into
their weight and balance loading manifest.

6. TOWING AND TAXIING

6.1. There are no changes to the towing and taxiing procedures or manuals as a result of this modification.

7. PARKING AND MOORING

7.1. There are no changes to the parking and mooring procedures or manuals as a result of this
modification.

8. PLACARDS AND MARKING

8.1. There are no special markings or placards for this installation.

9. SERVICING
9.1. There are no changes to servicing procedures or manuals as a result of this modification.

10. LIMITATIONS
10.1. “The Airworthiness Limitations section is FAA approved and specifies maintenance required under
Secs. 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been
FAA approved”.
10.2. There are no Airworthiness Limitations associated with this STC.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page 3

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
APPENDIX A – INSTRUCTIONS FOR CONTINUED AIRWORTHINESS CHECKLIST

Addressed in
Requirement Regulation
Document/Section
ICAW in the form of a manual or manuals.
H25.2(a) D2002-256
In a practical arrangement.
A description of the: See Below
• aircraft and its systems and installations, N/A
• engines and its systems and installations, H25.3(a)(2) N/A
• propellers and its systems and installations, N/A
• appliances and its systems and installations. AMM
Basic control and operation information describing D2002-256 para. 2
• how the aircraft components and systems
D2002-256 para. 2
are controlled and H25.3(a)(3)
• how the aircraft components and systems
are operated including any special procedure D2002-256 para.2
and limitations.
Servicing information that covers details regarding N/A
• servicing points, N/A
• capacities of tanks, N/A
H25.3(a)(4)
• capacities of reservoirs, N/A
• types of fluids to be used, N/A
• pressures applicable to the various systems. N/A
Location of access panels for inspection and
H25.3 (a)(4) D2002-256 para. 3
servicing.
Servicing information that covers details regarding See Below
• locations of lubrication points, H25.3(a)(4) D2002-256 Appendix C
• the lubricant to be used. N/A
Equipment required for servicing. H25.3(a)(4) N/A
Tow instructions and limitations. H25.3(a)(4) N/A
Mooring information H25.3(a)(4) N/A
Jacking information H25.3(a)(4) N/A
Leveling information H25.3(a)(4) N/A

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.1

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
 Addressed in
Requirement Regulation
Document/Section
Scheduling information for each part of the aircraft
that, provides the recommended periods at which N/A
they should be
• cleaned, N/A
• inspected, H25.3(b)(1) N/A
• adjusted, N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods. N/A
Scheduling information for the aircraft’s engine(s)
that provides the recommended periods at which N/A
they should be
• cleaned, N/A
• inspected, N/A
• adjusted, H25.3(b)(1) N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods.
NOTE: This information may be in the FAA accepted N/A
engine ICA.
Scheduling information for the aircraft’s auxiliary
power unit (APU) that provides the recommended N/A
periods at which they should be
• cleaned, N/A
• inspected, H25.3(b)(1) N/A
• adjusted, N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods. N/A

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.2

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or use requires permission in writing from Rosemount Aerospace Inc.
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 Addressed in
Requirement Regulation
Document/Section
Scheduling information for the aircraft’s propellers
that provides the recommended periods at which N/A
they should be
• cleaned, N/A
• inspected, H25.3(b)(1) N/A
• adjusted, N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods. N/A
Scheduling information for the aircraft’s accessories
that provides the recommended periods at which N/A
they should be
• cleaned, N/A
• inspected, H25.3(b)(1) N/A
• adjusted, N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods. N/A
Scheduling information for the aircraft’s instruments
that provides the recommended periods at which N/A
they should be
• cleaned, N/A
• inspected, H25.3(b)(1) N/A
• adjusted, N/A
• tested, N/A
• lubricated and N/A
• the work recommended at these periods. N/A
Scheduling information for the aircraft’s equipment
that provides the recommended periods at which D2002-256 Appendix C
they should be
• cleaned, D2002-256 Appendix C
• inspected, H25.3(b)(1) D2002-256 Appendix C
• adjusted, D2002-256 Appendix C
• tested, D2002-256 Appendix C
• lubricated and D2002-256 Appendix C
• the work recommended at these periods. D2002-256 Appendix C

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.3

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 Addressed in
Requirement Regulation
Document/Section
The degree of inspection for each part of the aircraft
See Below
and its
• engines N/A
• auxiliary power unit, H25.3(b)(1) N/A
• propellers, N/A
• accessories, N/A
• instruments and equipment D2002-256 Appendix C
The applicable wear tolerances H25.3(b)(1) N/A
The applicant may refer to an See Below
• accessory, N/A
• instrument, or N/A
• equipment manufacturer as the source of this
H25.3(b)(1) Boeing MPD D6-38278
information if the applicant shows
• that the item has an exceptionally high
degree of complexity requiring specialized
N/A
maintenance techniques, test equipment, or
expertise.
The recommended overhaul periods and necessary
cross references to the Airworthiness Limitation H25.3(b)(1) N/A
Section.
An inspection program that includes D2002-256 Appendix C
• the frequency and extent of the inspection H25.3(b)(1)
necessary to provide for the continued D2002-256 Appendix C
airworthiness of the aircraft
Troubleshooting information describing AMM
• problem malfunctions, AMM
H25.3(b)(2)
• how to recognize those malfunctions and AMM
• the remedial action for those malfunctions. AMM
Information describing the order and method of N/A
• removing and H25.3(b)(3) N/A
• replacing engine(s) with any necessary
N/A
precautions to be taken.
Information describing the order and method of AMM
• removing and H25.3(b)(3) AMM
• replacing parts with any necessary
AMM
precautions to be taken.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.4

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or use requires permission in writing from Rosemount Aerospace Inc.
THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE
 Addressed in
Requirement Regulation
Document/Section
Other general procedural instructions including See Below
• storage limitations and procedures for N/A
D2002-256 para. 2
• testing system during ground running,
AMM
• making symmetry checks, H25.3(b)(4) N/A
• weighing and determining the center of
D2002-256 para. 5
gravity,
• lifting, N/A
• shoring. N/A
Diagrams of structural access plates and information
needed to gain access for inspections when access H25.3(c) D2002-256 para. 3
plates are not provided.
Details for the application of special inspection
techniques including radiographic and ultrasonic H25.3(d) N/A
testing where such processes are specified.
Information needed to apply protective treatment to
H25.3(e) Boeing MPD D6-38278
structure after inspection.
All data relative to structural fasteners such as AMM
• identification, AMM
H25.3(f)
• discarded recommendations, and AMM
• torque values. AMM
A list of special tools needed H25.3(g) N/A
The Instructions for Continued Airworthiness must
contain a section, titled Airworthiness Limitations that D2002-256 para. 10
is:
• segregated and D2002-256 para. 10
• clearly distinguishable from the rest of the H25.4
document.
NOTE: The appropriate Aircraft Certification Office D2002-256 para. 10
will evaluate the Airworthiness Limitations
Section in the applicant’s ICA.
The Airworthiness Limitations Section must set forth
each mandatory replacement time, structural
H25.4 N/A
inspection interval, and related structural inspection
procedure approved under § 25.571.
If the Instructions for Continued Airworthiness consist
of multiple documents, the Airworthiness Limitations
H25.4 N/A
Section required by this paragraph must be included
in the principal manual.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.5

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 Addressed in
Requirement Regulation
Document/Section
The Airworthiness Limitations Section must contain a
legible statement in a prominent location that reads:
“The Airworthiness Limitations Section is FAA
H25.4 for FAR
approved and specifies maintenance required and D2002-256 para. 10
Part 25 Aircraft
under §§ 43.16 and 91.403 of the Federal Aviation
Regulations (FAR) unless an alternative program has
been FAA approved.

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page A.6

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APPENDIX B – MMEL/MEL
A Master Minimum Equipment List (MMEL) has been developed and approved by the FAA and other National
Regulatory for Operators of the B737-300/-400/-500 airplanes. Operators of this equipment should review
their approved MMEL list for applicable items and submit their request for use, and incorporation into their
MEL, to the appropriate regulatory authority.

NOTE: The current FAA MMEL for the B737-300/-400/-500 may be electronically obtained at
www.opspecs.com

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page B.1

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APPENDIX C – MAINTENANCE SCHEDULE
1.1. The maintenance tasks and intervals within the Boeing MPD D6-38278 have been found to provide
adequate scheduled maintenance for the CDSS alteration. See below for specific task detail.
1.1.1. Table 1.1 lists maintenance tasks for CDSS Installation Number 2002-180-1.
1.1.2. Table 1.2 lists maintenance tasks for CDSS Installation Number 2002-180-2 and 2002-180-3.
1.1.3. In conjunction with the tasks specified in Table 1, check the CDSS wiring harnesses for cracked,
chafing or broken wires. Check for excessive buildup of dust, dirt and liquid contaminates.
Clean excessive dust, dirt and other contaminants from the wiring by vacuum or by wiping with a
clean cloth as required. Refer to the drawings noted in Table 1 for locations and routing paths.
Repair or replace broken, cracked, or chafed wires in accordance with Boeing Standard Wiring
Practices Manual D6-54446 and the drawings noted in Table 1.
CAUTION: DO NOT use solvents, such as Methyl Ethyl Ketone (MEK) or Trichlorethylene when
cleaning wires.

Applicable Reference from Applicable Reference from British

Equipment
Boeing MPD D6-38278 Airways MPD ATP 2819
Camera Units Z53-107-02-Z 0124002H
Z53-101-01-Z
LCD Monitor Assembly 0124002H
Z53-101-02-Z
Z53-101-01-Z
Control Panel 0124002H
Z53-101-02-Z
2002-190
Reference Drawings 2002-194 n/a
2002-195

LE 1.1 –Maintenance Tasks and Intervals, CDSS Installation 2002-180-1

Applicable Reference from

Equipment
Boeing MPD D6-38278
Camera Units and
Z53-107-02-Z
System Active Indicator
Z53-101-01-Z
LCD Monitor Assembly
Z53-101-02-Z
Z53-101-01-Z
Control Panel
Z53-101-02-Z
2002-190
Reference Drawings 2002-194
2003-041

TABLE 1.2 –Maintenance Tasks and Intervals, CDSS Installation 2002-180-2 and 2002-180-3

Supplemental Instructions for Continued Airworthiness, Cockpit Door Surveillance No.: D2002-256
System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D Rev.: E
Page C.1

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