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时间:2011-03-21 08:24来源:蓝天飞行翻译 作者:admin
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 (4)
 Put the door lining (2) in position and attach it with the screws (33), the plugs (32), the screws (10) and the washers (11).

 (5)
 Lift up the cover (30) and install the plate (31) the screw (12) and the nut (13).


 Subtask 25-23-47-420-120
 D. Installation of the Door Lining 843DZ (844DZ) (834DZ) (6)
 (Ref. Fig. 404/TASK 25-23-47-991-015)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Put the door lining (6) in position on the door and engage the attach brackets to the yo-yo rolls.

 (3)
 Install the LWR handle section (25) the screws (28) and the washers (27).

 (4)
 Install the cover (26) to the LWR handle section (25).

 (5)
 Make sure that the lugs (29) of the cover (26) engage correctly and you hear a click.

 (6)
 Install the cover (21) the screws (22) and the washers (23).

 


 Subtask 25-23-47-420-121
 E. Installation of the Door Lining 843EZ (844EZ) (834EZ) (1)
 (Ref. Fig. 404/TASK 25-23-47-991-015)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Put the door lining (1) in position and install it with the screws


 (8) and the washers (9). Subtask 25-23-47-210-075
 F. Visual Inspection
 (1)
 Make sure that all placards of the retained/new components are in the correct position and in good condition.

 (2)
 If necessary install the new placards, refer to (Ref. TASK 11-00-00-400-002) (Ref. AMM 11-32-25 P.Block 001)


 5. Close-up
________ Subtask 25-23-47-865-086
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15WN, 13WN, 48WV.
 Subtask 25-23-47-410-069
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the related emergency exit door. (Ref. TASK 52-22-00-410-001)


 (3) Remove the access platform(s). Subtask 25-23-47-862-059
 C. De-energize the aircraft electrical circuits. (Ref. TASK 24-42-00-862-001) TASK 25-23-47-000-010


 Removal of the Door Frame Linings of the LH/RH AFT Emergency Exit Doors, zones 251/252.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 33-51-11-000-001 Removal of the Cabin Emergency Lights 33-51-13-000-001 Removal of the Cabin Wall-Mounted
 Emergency-Exit-Markers 33-51-16-000-001 Removal of the Emergency Exit Sign 52-22-00-010-001 Opening of the Emergency Exit Doors from the
 Passenger Compartment 25-23-47-991-010 Fig. 405
 3. Job Set-up
__________ Subtask 25-23-47-861-073
 A. Aircraft Maintenance Configuration
 (1) Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

 

 Subtask 25-23-47-010-077
 B. Get Access
 (1)
 Put the access platform in position on the related emergency exit door(s).

 (2)
 Open the related emergency exit door(s) (Ref. TASK 52-22-00-010-001).

 (3)
 Remove the emergency exit sign(s) 43WL (42WL) (Ref. TASK 33-51-16-000-001)

 (4)
 Remove the cabin emergency light(s) 37WL (36WL) (Ref. TASK 33-51-11-000-001)

 (5)
 Remove the cabin-wall mounted emergency-exit-marker(s) 90WL5 (90WL6) (Ref. TASK 33-51-13-000-001)


 Subtask 25-23-47-865-065
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU COM/CIDS/DEU B/ESS 153RH G03 49VU LIGHTING/EMER LT/CABIN 2WL H06 49VU LIGHTING/EMER LT/CABIN 1WL H05
 122VU LIGHTING/CABIN/EMER/LT 3WL V07
 4. Procedure
 
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