(7) in position in the mounting bracket (6).

 (d)
 Make sure that the tab washer (7) engages into the hole of the mounting bracket (6).

 (e)
 Install the castle nut (5) on the lamp body (4).

 (f)
 TORQUE the castle nut (5) with the SPANNER - WRENCH (98F52308330000) to 0.12 m.daN (10.61 lbf.in).

 (2)
 Install the lamp (3) in the lamp body (4) as follows:

 (a)
 Make sure that the lamp body (4) is in the correct condition.

 (b)
 Put the lamp (3) into the lamp body (4).

 (c)
 Install the lamp cover (1) the rubber cap (2) on the lamp body

 (4) and turn it.

 (d)
 Make sure that the rubber cap (2) is installed correctly on the castle nut (5).

 1EFF : ALL 1 52-35-12Page 409 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 Subtask 52-35-12-865-051
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MJ.
 Subtask 52-35-12-710-050
 C. Operational Test
 (1)
 Make sure the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).

 (2)
 Push the lamp cover (1) and examine the indicator light comes on.

 5. Close-up
________ Subtask 52-35-12-410-050
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Close the access panel 134AR. Subtask 52-35-12-862-050
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 1EFF : ALL 1 52-35-12Page 410 1 1 Aug 01/05R 1 1 1CES 1

 TASK 52-35-12-000-002 Removal of the Indicator Light 8MJ
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps No specific circuit breaker(s) safety clip(s) No specific soldering iron 98F52308330000 1 SPANNER - WRENCH
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001  Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 53-42-14-000-001 Removal of the AFT Cargo-Compartment Floor-Panels Zone 150 52-35-12-991-002 Fig. 402
 3. Job Set-up
__________ Subtask 52-35-12-865-053
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
122VU DOORS/CARGO  1MJ T12
 1EFF : ALL 1 52-35-12Page 411 1 1 Aug 01/01R 1 1 1CES 1

 Subtask 52-35-12-010-051
 B. Get Access
 (1)
 Open the access panel 154AR of the door control panel below the fuselage.

 (2)
 To get access to the service panel 2027VU, continues as follows:

 (a)
 Open the AFT cargo compartment door (referred to as cargo door) and install the actuator safety locks (Ref. TASK 52-30-00-860-001).

 (b)
 Remove the floor panel 152AG of the AFT cargo compartment (Ref. TASK 53-42-14-000-001).

 4. Procedure
_________ Subtask 52-35-12-020-051
 A. Removal of the Indicator Light (8MJ)
 (Ref. Fig. 402/TASK 52-35-12-991-002)

 (1)
 Remove the lamp assy (1) and the rubber cap (2) from the lamp body (3).

 (2)
 Remove the service panel (7) from the aft control panel as follows:

 (a)
 Disconnect the connector (8) from the receptacle of the service panel (7).

 (b)
 Put blanking caps on the disconnected electrical connectors.

 (c)
 Remove the srews (4) and the washers (5) from the inner side of the aft control panel.

 (d)
 Remove the service panel (7) and the seal (6) from the aft control panel.

 (3)
 Disassemble the service panel (7) as follows:

 (a)
 Remove the screw (14) from the plate (13).

 (b)
 Carefully remove the plate (13) and the seal (10) from the service panel (7).

 1EFF : ALL 1 52-35-12Page 412 1 1 Aug 01/01R 1 1 1CES 1
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門6(91)