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时间:2011-03-21 08:32来源:蓝天飞行翻译 作者:admin
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 (2)
 If necessary, remove damaged tape (4),(7) from the partition panels (1),(2).

 (3)
 Clean the component interface and/or the adjacent area with CLEANING AGENTS (Material No. 11-004) .

 (4)
 If necessary, remove damaged tape (4),(7) from the partition panels (1),(2).

 (5)
 If necessary, remove damaged tape (9) from the valve (8).

 (6)
 Replace the removed tape (4),(7) on the partition panels (1),(2).

 (7)
 Replace the removed tape (9) on the valve (8).

 (8)
 Put the valve (8) in the correct position on the partition panel (2) and fasten them with the studs (10).

 (9)
 Put the grills (6) in the correct position on the partition panels (1),(2) and fasten them with the studs (5).


 Subtask 25-55-12-420-050
 B. Installation of the AFT Cargo-Compartment Partition FR65.
 (1)
 Install the partition panels (1),(2).

 (2)
 Fasten the partition panels (1),(2) with the studs (3).


 5. Close-up
________ Subtask 25-55-12-410-050-A
 A. Put the aircraft back to the serviceable condition.
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 EFF : ALL
25-55-12Page 415
Aug 01/05
R
 CES  **ON A/C 001-049, 051-099, 101-105,


 Subtask 25-55-12-942-054
 B. Close Access
 (1) Close the BULK cargo compartment door.
 (2) Remove the access platform(s). R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 25-55-12-942-054-B
 B. Close Access
 (1)
 Remove the actuator safety lock and close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002).

 (2)
 Remove the access platform(s).


 EFF : ALL
25-55-12Page 416


 **ON A/C ALL
 TASK 25-55-12-000-002
 Removal of the Ceiling Panels in the AFT Cargo Compartment - FR59/FR65

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  access platform 2.1 m (6 ft. 11 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
52-30-00-860-001  Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 25-55-12-991-002  Fig. 402
 **ON A/C 151-199,
 25-55-12-991-002-A Fig. 402A R **ON A/C 401-499,
R 25-55-12-991-002-B Fig. 402B
 EFF : ALL
25-55-12Page 417


 **ON A/C ALL
 3. Job Set-up
__________
 **ON A/C 001-049, 051-099, 101-105,

 Subtask 25-55-12-010-053-B
 A. Get Access
 (1)
 Open the BULK cargo compartment door.

 (2)
 Put the access platform in position at the opening of the BULK cargo compartment door.


R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 25-55-12-010-053-A
 A. Get Access
 (1)
 Open the AFT cargo-compartment door and install the actuator safety lock (Ref. TASK 52-30-00-860-001).

 (2)
 Put the access platform in position at the opening of the AFT cargo-compartment door.


 **ON A/C ALL
 4. Procedure
_________
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,

 (Ref. Fig. 402/TASK 25-55-12-991-002)
 **ON A/C 151-199,

 (Ref. Fig. 402A/TASK 25-55-12-991-002-A)


 Ceiling Panels - AFT Cargo Compartment FR59/FR65 Figure 402/TASK 25-55-12-991-002 
R  EFF : 001-049, 051-099, 101-149, 201-299, 301-399,  25-55-12 Page 419 Aug 01/05
 CES 

 

 Ceiling Panels - AFT Cargo Compartment FR59/FR65 Figure 402A/TASK 25-55-12-991-002-A 
R  EFF :  151-199,  25-55-12 Page 420 Aug 01/05
 CES 

 

R  **ON A/C 401-499, 
R  (Ref. Fig. 402B/TASK 25-55-12-991-002-B) **ON A/C ALL
 Subtask 25-55-12-020-052 A. Removal of the Ceiling Panels NOTE : The removal of each ceiling panel is the same.____ (1) Remove the joint strip (5) from the ceiling panels (2). (2) Support the ceiling panels (2). (3) Loosen the studs (3),(4) and (7) of the ceiling panels (2). (4) Remove the ceiling panels (2) from the aircraft structure.
 
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