SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL FOR …

Rosemount Aerospace Inc. 14300 Judicial Road Burnsville, MN 55306-4898 Tel: 952 892 4000 Fax: 952 892 4800

SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

FOR

ROSEMOUNT AEROSPACE INC.

COCKPIT DOOR SURVEILLANCE SYSTEM

INSTALLED IN

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

STC ST00971SE-D

D2002-247 Revision C

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*

By Noreen Benjegerdes at 1:31 pm, May 12, 2009

* 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.

Page i

BOEING 737-300. 400.500 SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

CHAPTER 23 - COMMUNICATIONS REVISION STATUS

Rev. A B

C

Page All

Paragraph

All

Change Description

Original Release Added 2002-180-3 Installation Reformatted entire document to Goodrich/Rosemount Aerospace Inc. letterhead Added revision status table

Number of Pages

5

5

Effectivity S/N or Date

15 Oct 02

12 May 03

6

See Cover Page

Supplemental Wiring Diagram Manual Cockpit Door Surveillance System, Boeing 737-300/-400/-500 Series, STC ST00971SE-D

No.: D2002-098 Rev.: B Page ii

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.

THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE

BOEING 737-300. 400.500 SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

CHAPTER 23 - COMMUNICATIONS LIST OF EFFECTIVE PAGES

CHAPTER SECTION SUBJECT

LIST OF EFFECTIVE PAGES TABLE OF CONTENTS 23-79-00

23-79-00

23-79-00

23-79-10

23-79-20

PAGE

1 1 1 2 3 4 5 6 401 402 403 404 501 502 503 504 505 506 507 401 402 403 404 401 402 403

DATE

APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09 APR 9/09

EFFECTIVITY

D2002-247

23-79-00

PAGE 1

ALL AIRCRAFT WITH

APR 9/09

CDSS INSTALLED

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.

THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE

TITLE

BOEING 737-300. 400.500 SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

CHAPTER 23 - COMMUNICATIONS TABLE OF CONTENTS

CHAPTER SECTION SUBJECT

COCKPIT DOOR SURVEILLANCE SYSTEM CDSS DESCRIPTION AND OPERATION

COCKPIT DOOR SURVEILLANCE SYSTEM CDSS LCD ASSEMBLY - REMOVAL / INSTALLATION

COCKPIT DOOR SURVEILLANCE SYSTEM CDSS ADJUSTMENT / TEST

COCKPIT DOOR SURVEILLANCE SYSTEM CDSS CAMERA ASSEMBLY - REMOVAL / INSTALLATION

COCKPIT DOOR SURVEILLANCE SYSTEM CDSS CAMERA CONTROL PANEL ASSEMBLY REMOVAL / INSTALLATION

23-79-00 23-79-00 23-79-00 23-79-10 23-79-20

PAGE

1 401 501 401 401

EFFECTIVITY

D2002-247

23-79-00

PAGE 1

ALL AIRCRAFT WITH

APR 9/09

CDSS INSTALLED

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.

THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE

BOEING 737-300. 400.500 SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

COCKPIT DOOR SURVEILANCE SYSTEM (CDSS) - DESCRIPTION AND OPERATION

1. General

A. The Cockpit Surveillance System (CDSS) provides the flight crew with live video images of the control cabin door entrance area, thus enabling the pilots to visually identify persons requesting access to the flight compartment.

B. The CDSS consists of the following major components:

(1) Three video cameras, infrared-illuminated, black-and-white output, located in the cabin as follows:

(a) Camera one is mounted above the control cabin door, (station 297). This camera provides a view of the area just aft of the control cabin, forward cabin, and the galley area.

(b) Camera two is mounted in the ceiling panel above the forward entry door area, (station 341). This camera provides a view looking inboard of the cabin area and the forward entryway.

(c) Camera three is mounted in the ceiling panel above the forward service door, (station 321). This camera provides a view looking inboard, of the galley and the entryway to the control cabin.

(2) A liquid Crystal Display (LDS) Assembly is mounted on the inboard corner of the P6 circuit breaker panel.

(3) The camera control panel located in the center pedestal contains the power and view selector switches.

C. The CDSS is classified as miscellaneous, non-essential electrical equipment. The CDSS is not integrated with existing, essential flight deck display equipment.

D. The System Active Indicator (if installed) is located above camera three (approximately 6 inches), in the ceiling panel above the forward service door.

2. LCD Assembly (Figure 1)

A. The LCD Assembly provides the CDSS display, display control functions for use by the flight crew, and provides a fixed enclosure to contain system components. The LCD Assembly consists of the following:

(1) An LCD Monitor with a thin film resistor display screen (6.4-inch diagonal measure) that shows images from the video cameras.

(2) An enclosure to house the electronics assembly, which includes the following:

(a) A system controller, which contains a video computer circuit card, that provides image selection of up to four NTSC camera inputs. The display electronics include input/output lighting/EMI protection. The computer receives video signals from the cameras and processes the signals for use by the LCD.

(b) A system power supply, which provides power to all cameras connected to the CDSS.

EFFECTIVITY

D2002-247

23-79-00

PAGE 1

ALL AIRCRAFT WITH

APR 9/09

CDSS INSTALLED

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.

THI S DOCUMENT SUBJECT TO THE CONTROLS AND RESTRICTIONS ON THE FIRST PAGE

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