supplemental aircraft maintenance manual for … · boeing 737-300. 400.500 supplemental aircraft...

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

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

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*

* 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

noreben

Approved

BOEING 737-300. 400.500 SUPPLEMENTAL AIRCRAFT MAINTENANCE MANUAL

CHAPTER 23 - COMMUNICATIONS

REVISION STATUS

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


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

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

Rev. Page Para-graph Change Description Number

of Pages Effectivity S/N

or Date A Original Release 5 15 Oct 02 B Added 2002-180-3 Installation 5 12 May 03

C All All

Reformatted entire document to Goodrich/Rosemount Aerospace Inc. letterhead Added revision status table

6 See Cover Page



LIST OF EFFECTIVE PAGES

EFFECTIVITY 23-79-00

D2002-247 PAGE 1 ALL AIRCRAFT WITH

CDSS INSTALLED APR 9/09



CHAPTER SECTION SUBJECT PAGE DATE LIST OF EFFECTIVE PAGES 1 APR 9/09

TABLE OF CONTENTS 1 APR 9/09

23-79-00 1 APR 9/09

2 APR 9/09

3 APR 9/09

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6 APR 9/09

23-79-00 401 APR 9/09

402 APR 9/09

403 APR 9/09

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23-79-00 501 APR 9/09

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23-79-10 401 APR 9/09

402 APR 9/09

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23-79-20 401 APR 9/09

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403 APR 9/09



TABLE OF CONTENTS






CHAPTER SECTION TITLE SUBJECT PAGE COCKPIT DOOR SURVEILLANCE SYSTEM CDSS - 23-79-00 1 DESCRIPTION AND OPERATION COCKPIT DOOR SURVEILLANCE SYSTEM CDSS - 23-79-00 401 LCD ASSEMBLY - REMOVAL / INSTALLATION COCKPIT DOOR SURVEILLANCE SYSTEM CDSS - 23-79-00 501 ADJUSTMENT / TEST COCKPIT DOOR SURVEILLANCE SYSTEM CDSS - 23-79-10 401 CAMERA ASSEMBLY - REMOVAL / INSTALLATION COCKPIT DOOR SURVEILLANCE SYSTEM CDSS - 23-79-20 401 CAMERA CONTROL PANEL ASSEMBLY REMOVAL / INSTALLATION


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.








CAUTION: REMOVE LCD ASSEMBLY AND BRACKET ASSEMBLY FROM WALL BEHIND CO-PILOT BEFORE LOWERING OVERHEAD CIRCUIT BREAKER PANEL P6-1. DAMAGE COULD RESULT FROM CIRCUIT BREAKER PANEL P6-1 CONTACT WITH LCD ASSEMBLY.

B. The LCD Monitor has the following features:

(1) The LCD Monitor screen has an anti-glare coating and passive backlighting. The backlighting function automatically adjusts screen brightness. A photo-diode on the face of the LCD monitor senses ambient light conditions.

(2) Four controls are located on the front of the LCD Monitor.

(a) Photo-diode light sensor.

(b) Power/Failure LED Indicator, which indicates that the CDSS is powered and operational.

(c) Manual Brightness control knob.

(d) Manual Contrast control knob.

3. Camera Assembly (Figure 1)

A. All three CDSS cameras are interchangeable.

B. The camera assemblies are mounted in housings which allow the camera to swivel (left-right, up-down, and rotate) to achieve the desired field of view.

C. Each camera in this installation has a 105-degree horizontal viewing angle lens.

D. Each camera has an array of infrared-emitting diodes, to illuminate the field of view in all light conditions, including complete darkness.

E. The cameras have a replaceable front lens cover that protects the camera lens and assembly form contamination.

F. The flight crew can toggle between camera views by using the VIEW SELECT switch on the Control Panel.

G. The cameras are supplied with 12 VDC from the LCD assembly.

4. Camera Control Panel (Figure 1)

A. The camera control panel is located on the center console between the captain and first officer.

B. The camera control panel contains two switches.

C. "Camera System Power" controls power to all components in the system.

D. "View Select" switches from one camera view to another.








5. Operation (Figure 2)

A. Power Sources

(1) The CDSS has two sources of power.

(2) The main system power is supplied from 28 VDC. Power is supplied through a circuit breaker, labeled CDSS (2 1/2 Amp), located in the P6-3 circuit breaker panel.

(3) The Camera System Control Panel backlight overlay panel (labeled CDSS) is supplied from the 5 VAC panel lighting circuit.

B. Control

(1) The CDSS has the following primary controls.

(2) Camera System Power: The Camera System Power switch is located on the Camera System Control Panel. Power to the CDSS is controlled with the power switch.

(3) View Select: The View Select switch is located on the Camera System Control Panel. When activated, this switch toggles the displayed image between the views captured by Camera 1, Camera 2 and Camera 3.

(4) Display Brightness/Contrast: Screen brightness and contrast is automatically controlled by sensing the ambient light conditions present in the flight compartment. Manual adjustment of screen brightness (upper knob) and contrast (lower knob) is possible using the controls provided on the face of the LCD Monitor.

(5) Display Sleep Mode: An automatic sleep mode turns OFF power to the LCD Monitor after 5 minutes of inactivity (if no change in camera image is detected during this period).

(a) To restore the display image, the VIEW SELECT switch must be pressed (LCD Monitor power is restored). The image displayed will be from the last selected camera position, if the restore action is taken within the first 120 seconds of sleep mode.

(b) If the restore action is taken after 120 seconds of sleep mode, the display will present the Camera 1 image. Power to the cameras and a camera infrared illumination function are not interrupted during sleep mode.

C. Annunciation

(1) A power/failure LED (green illumination) provides a system status indication. The LED is located on the face of the LCD Monitor, above the manual display control knob.

Status LED Illumination System Status

Steady ON Power ON and operational

Flashing System failure detected

No Illumination Power OFF to System








D. Flight Operations Requirements

(1) All phases of flight operations.

(a) Camera System Power ON as necessary.

(b) View Select switch momentary push toggle displayed images from Camera 1, to Camera 2, to Camera 3 and then back to Camera 1.








Cockpit Door Surveillance System (Video) Components Figure 1

Control Panel Installation in the Center Pedestal

LCD Assembly on the P6 Panel

RETAINER SNAP RING (2)

CAMERA ASSY (1)

CEILING PANEL

Camera installation above flight compartment entry door








Cockpit Door Surveillance System (Video) Block Diagram Figure 2


COCKPIT DOOR SURVEILANCE SYSTEM (CDSS) - LCD ASSEMBLY - REMOVAL / INSTALLATION






6. General

A. This procedure has these tasks:

(1) A removal of the CDSS, Liquid Crystal Display (LCD) Assembly.

(2) An installation of the CDSS, Liquid Crystal Display (LCD) Assembly.

B. The LCD Assembly is installed on the inboard, forward corner of the P6 circuit breaker panel, in the flight compartment.

7. CDSS LCD Assembly Removal (Figure 401)

A. References

(1) AMM 20-40-12 p201, ESDS Handling for Metal Encased Unit Removal

(2) AMM 20-40-12 p201, Conductive Dust Cap and Connector Cover Installation

B. Access

(1) Location Zones

(a) 101 Flight Compartment - Left

(b) 102 Flight Compartment - Right

C. .Procedure

(1) Open these circuit breakers and attach DO-NOT-CLOSE tags:

(a) Circuit Breaker Panel, P6-3

1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE LCD ASSEMBLY (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE LCD ASSEMBLY (1).

(2) Before you touch the LCD assembly (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to remove the LCD Assembly (1):

(a) Loosen the two screws (4) that secure LCD assembly (1) to mounting bracket (2).

(b) Carefully remove the LCD assembly (1) from the mounting bracket (2).

(c) Disconnect the assembly electrical connector (3).

(d) Install a protective cover on the electrical connector, do this task: Conductive Dust Cap and Connector cover installation (AMM 20-40-42 p201)








LCD Assembly Installation Figure 401

Attaching Screws (4)

LCD MountingBracket (2)

LCD Assembly (1)

P-6 Panel

Electrical Connector (3)








8. CDSS LCD Assembly Installation (Figure 401)

A. References

(1) AMM 20-40-12 p201, ESDS Handling for Metal Encased Unit Installation

(2) AMM 20-40-12 p201, Conductive Dust Cap and Connector Cover Removal

B. Access

(1) Location Zones

(c) 101 Flight Compartment - Left

(d) 102 Flight Compartment - Right

C. .Procedure

(1) Make sure these circuit breakers are open:


1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE LCD ASSEMBLY (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE LCD ASSEMBLY (1).

(2) Before you touch the LCD assembly (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to install the LCD Assembly (1):

(a) To remove the protective cover from the electrical connectors (3), do this task: Conductive Dust Cap and Conductor Cover Removal (AMM 20-40-12 p201).

(b) Examine the electrical connector (3) for bent or broken pins, dirt, and damage.

(c) Connect the electrical connector (3).

(d) Position the LCD Assembly (1) to the mounting bracket (2).

(e) Install the two screws (4) (Torque 12-18 inch-lbs).








(4) Remove the DO-NOT-CLOSE tags and close these circuit breakers:


1) CDSS

D. .Installation Test

(1) Do this task: Perform all tests that relate to the LCD Assembly (AMM 23-79-00 p501).


COCKPIT DOOR SURVEILANCE SYSTEM (CDSS) - ADJUSTMENT / TEST






1. General


(1) Functional Test, Lighting Function, LCD Assembly

(2) CDSS Functional Test

(3) Camera Operation and Selection

(4) Manual Image Controls

(5) Image Clarity and Image Orientation

(6) Camera Adjustment

B. References

(1) AMM 23-79-00 p801

C. Access

(1) Location Zones



(c) 104 Forward Galley Area - Right

(d) 105 Forward Entry Area - Left

D. Prepare for the test

(1) Do this task: Supply Electrical Power (AMM 24-22-00 p201)


1) CDSS

2) ELECTRONIC PANEL LIGHTS

E. Functional Test, Lighting Function, LCD Assembly (Figure 501)

(1) Turn on the 5 VAC Panel Lighting








(a) Make sure the Camera System overlay panel is illuminated.

(2) Dim the 5 VAC Panel Lighting

(a) Make sure the CDSS "Camera System" overlay panel dims.

F. Power Switch

(1) Move the Power switch to turn on the power to the CDSS.

(a) Make sure an image is present on the LCD monitor. Allow 10 seconds for system turn-on.

(b) Make sure the System Active Indicator (If installed) is illuminated.

(2) Move the Power switch to turn off power to the CDSS.

G. Camera Operation and Selection

(1) Move the Power switch to turn on the power to the CDSS. (If necessary)

(a) Make sure that the LCD monitor displays the view from Camera 1 (Looks aft from flight compartment door).

(2) Push the View Select Switch.

(a) Make sure that the LCD monitor displays the view from Camera 2.

(3) Push the View Select Switch.

(a) Make sure that the LCD monitor displays the view from Camera 3.

(4) Push the View Select Switch a few times.

(a) Make sure that the system display toggles between views of Camera 1, Camera 2, and Camera 3.

H. Manual Image Controls

(1) Rotate the Brightness Control Knob.

(a) Make sure the image brightness increases and decreases.

(2) Rotate the Contrast Control Knob.

(a) Make sure the image contrast increases and decreases.








I. Automatic Gain Control

(1) Press View Select switch until Camera 1 image is displayed on LCD monitor.

(a) Using a flashlight, position the light beam at the auto dim sensor located at the right corner of the CDSS LCD monitor. Make sure the image brightness increases.

(b) Remove the light source from the CDSS LCD Monitor, verify that the image brightness decreases.

J. Image Clarity and Image Orientation


(a) Make sure the Camera 1 image displayed is clear and focused.

1) Use a suitable subject (person) or object in front of the camera to assure image clarity.

2) Image clarity shall be sufficient to determine a person's identity.

(b) Make sure the Camera 1 image is correctly oriented on the LCD monitor.


(a) Repeat the test of image clarity, focus and orientation for Camera 2.


(a) Repeat the test of image clarity, focus and orientation for Camera 3.

K. Camera Adjustment

(1) Prepare the CDSS for use.

(a) Press the View Select switch until the from the desired camera is visible.

NOTE: The following steps are best done with one person in the flight compartment viewing the LCD monitor and a second person a the camera location to position the camera.

(2) Adjust the camera mounting angle.

(a) Grasp the outer ring of the camera and push in the desired direction.








(b) If necessary, the camera housing may be removed from its mounting surface to allow better access to adjust the camera mounting angle.

1) Alternatively, a reading light adjusting tool may be used to position the camera.

2) Image clarity shall be sufficient to determine a person's identity.

CAUTION: USE CAUTION NOT TO DAMAGE THE CAMERA WITH THE TOOL.

(3) Verify the camera image field of view displayed on the LCD monitor.

(a) Position a tall person, or target image, of about 1.88 meters (6 feet, 2 inches) height, located approximately 30 cm (12 inches) form the flight compartment door, and on the center line of the entry way.

1) Make sure the tall person's head or the target image is present on the LCD monitor display in the upper half of the display and is approximately in the display center.

(b) Position a short person, or bend down to simulate a short person, or place a target image, of about 1.52 meters (5 feet) height, located approximately 30 cm (12 inches) form the flight compartment door, and on the center line of the entry way.

1) Make sure the short person's head or the target image is present on the LCD monitor display.

2) Make sure that the image clarity is sufficient to determine a person's identity.

(4) Camera 2 setup and test.

(a) Adjust the up-and-down mounting angle of Camera 2 so that the maximum area can be viewed from the ceiling to the floor in the direction of the cockpit door entry way.

(b) Adjust the side-to-side mounting angle of Camera 2 to point straight ahead, so that the cockpit door entry way is approximately centered in the LCD monitor display.

1) Make sure that a person or persons, in the cabin area and entry way leading to the cockpit, are visible on the LCD monitor.

L. Low Level Light test

(1) Secure the Passenger Cabin

(a) In the Passenger Cain, close all entry and service doors. Secure all ambient lighting and close all window blinds.

(b) With the Cabin in low level light condition prepare the CDSS for use.








1) Press the View Select switch until the image from the desired camera is visible.


(2) Camera 1 test

(a) Position a tall person, or target image, of about 1.88 meters (6 feet 2 inches) height located approximately 30 cm (12 inches) from the flight compartment door, and on the center line of the entry way.


(3) Camera 2 test

(a) Make sure that a person or persons, in the cabin area and entry way leading to the flight compartment, are visible on the LCD monitor.

(4) Camera 3 test


M. High Level Light test

(1) Configure the Passenger Cabin


(a) In the Passenger Cain, turn on all ambient lighting and open all window blinds.

(b) With the Cabin in a high level light condition prepare the CDSS for use.

1) Press the View Select switch until the image from the desired camera is visible.

(2) Camera 1 test

(a) Position a tall person, or target image, of about 1.88 meters (6 feet 2 inches) height located approximately 30 cm (12 inches) from the flight compartment door, and on the center line of the entry way.









(3) Camera 2 test


(4) Camera 3 test


N. Auto Sleep Mode test

(1) 1 Minute Test

(a) With the CDSS activiated, press the, "View Select" Button until Camera 2 is displayed on the LCD monitor.

NOTE: For the LCD display to enter "Sleep Mode", the CDSS must remain inactive. Do not press any buttons on the control panel or LCD monitor during this time.

(b) With the Camera 2 displayed on the LCD monitor, wait 5 minutes for the CDSS to enter "Sleep Mode".

1) During "Sleep Mode" the LCD monitor will remain blank.

(c) Once the CDSS has entered "Sleep Mode", wait 1 minute and then press the "View Select" button.

1) The CDSS should display the view from Camera 2.

(2) 5 Minute Test

(a) With the CDSS activated, press the 'View Select" button until Camera 2 is displayed on the LCD monitor.

NOTE: For the LCD display to enter "Sleep Mode", the CDSS must remain inactive. Do not press any buttons on the control panel or LCD monitor during this time.

(b) With the Camera 2 displayed on the LCD monitor, wait 5 minutes for the CDSS to enter "Sleep Mode".

1) During "Sleep Mode" the LCD monitor will remain blank.








(d) Once the CDSS has entered "Sleep Mode", wait 5 minute and then press the "View Select" button.

1) The CDSS should display the view from Camera 1.

O. Put the Airplane Back to its Usual Condition.

(1) 1 Do this task: Remove Electrical Power (AMM 23-22-00 p201).


COCKPIT DOOR SURVEILANCE SYSTEM (CDSS) CAMERA ASSEMBLY - REMOVAL / INSTALLATION






2. General


(1) A removal of the CDSS, Camera Assembly.

(2) An installation of the CDSS, Camera Assembly.

B. The Camera Assemblies are installed on the ceilings above the flight compartment, forward entry, forward service doors.

3. CDSS Camera Assembly Removal (Figure 401)

A. References


(2) AMM 20-40-12 p201, Conductive Dust Cap and Connector Cover Installlation

B. Access

(1) Location Zones

(a) 104 Forward Galley Area - Right

(b) 105 Forward Entry Area - Left

C. Procedure



1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE CAMERA ASSEMBLY (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CAMERA ASSEMBLY (1).

(2) Before you touch the Camera assembly (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to remove the Camera Assembly (1):

(a) Remove the camera mounting plate by the removal of four screws.

(b) Remove the camera retaining snap ring (2).

(c) Carefully remove the Camera Assembly (1) from the mounting bracket.

(d) Disconnect the assembly electrical connector.

(e) Install a protective cover on the electrical connector, do this task: Conductive Dust Cap and Connector Cover Installation (AMM 20-40-42 p201).








Camera Assembly Installation Figure 401


CAMERA ASSY (1)

CEILING PANEL

Camera installation above flight compartment entry door


MOUNTING PLATE SCREWS (4 PLACES)

CAMERA ASSY (1)

MOUNTING PLATE

CEILING PANEL (REF)

Camera Installation Above Forward Entry Door

MOUNTING PLATE SCREWS (4 PLACES)

CAMERA ASSY (1)

MOUNTING PLATE

CEILING PANEL (REF)


Camera Installation Above Forward Service Door








4. CDSS Camera Assembly Installation (Figure 401)

A. References



(3) AMM 23-79-00 p501, Cockpit Door Surveillance System (CDSS) - Functional Test

B. Access

(1) Location Zones

(a) 104 Forward Galley Area - Right

(b) 105 Forward Entry Area - Left

C. Procedure

(1) Make sure these circuit breakers are open:


1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE CAMERA ASSEMBLY (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CAMERA ASSEMBLY (1).

(2) Before you touch the Camera assembly (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to install the Camera Assembly (1):

(a) To remove the protective cover from the electrical connector, do this task: Conductive Dust Cap and Conductor Cover Removal (AMM 20-40-12 p201).

(b) Examine the electrical connector for bent or broken pins, dirt, and damage.

(c) Connect the electrical connector.

(d) Position the Camera Assembly (1) in the mounting bracket.








(e) Install the retaining snap ring (2).

(f) Install the camera mounting plate by the installation of four screws.



1) CDSS

D. Installation Test

(1) Do this task: Perform all (AMM 23-79-00 p501) tests that relate to the Camera Assembly


COCKPIT DOOR SURVEILANCE SYSTEM (CDSS) CAMERA CONTROL PANEL ASSEMBLY - REMOVAL / INSTALLATION






1. General


(1) A removal of the CDSS, Camera Control Panel Assembly.

(2) An installation of the CDSS, Camera Control Panel Assembly.

B. The Camera Control Panel are installed in the center pedestal in the flight compartment.

2. CDSS Camera Control Panel Assembly Removal (Figure 401)

A. References


(2) AMM 20-40-12 p201, Conductive Dust Cap and Connector Cover Installation

B. Access

(1) Location Zones



C. Procedure



1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE CAMERA CONTROL PANEL (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CAMERA CONTROL PANEL (1).

(2) Before you touch the Camera Control Panel (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to remove the Camera Control Panel (1):

(a) Loosen the four quarter turn fasten (4) that secure the Camera Control Panel (1) to the Center Pedestal (2).

(b) Carefully remove the Camera Control Panel (1).

(c) Disconnect the Camera Control Panel Electrical Connector (3).

(d) Install a protective cover on the electrical connector, do this task: Conductive Dust Cap and Connector Cover Installation (AMM 20-40-42 p201).








Camera Control Panel Installation Figure 401

CAMERA CONTROL PANEL ASSEMBLY (1)

QUARTER TURN FASTENERS (4) (4 PLACES)

CENTER PEDESTAL (2)

CAMERA CONTROL PANEL ASSEMBLY ELECTRICAL CONNETOR (3) (ON BACK OF PANEL- NOT SHOWN)








3. CDSS Camera Control Panel Assembly Installation (Figure 401)

A. References



(3) AMM23-79-00 p501, Cockpit Door Surveillance System (CDSS) - Functional Test

B. Access

(1) Location Zones



C. Procedure

(1) Open these circuit breakers are open:


1) CDSS

CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE CAMERA CONTROL PANEL (1). IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE CAMERA CONTROL PANEL (1).

(2) Before you touch the Camera Control Panel (1), do this task: ESDS Handling for Metal Encased Unit Removal (AMM 20-40-12 p 201)

(3) Do these steps to install the Camera Control Panel (1):

(a) To remove the protective cover from the electrical connector (3) do this task: Conductive Dust Cap and Connector Cover Removal (AMM 20-40-12 p201).

(b) Examine the Electrical Connector (3) for bent or broken pins, dirt, and damage.

(c) Connect the Electrical Connector (3).

(d) Position the Camera Control Panel Assembly (1) in the Center Pedestal (2).

(e) Secure the four quarter turn fasteners (4) that secure the Camera Control Panel (1) to the Center Pedestal (2).



1) CDSS

D. Installation Test

(1) Do this task: Perform all (AMM 23-79-00 p501) tests that relate to the Camera Control Panel Assembly.

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