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时间:2011-03-26 23:52来源:蓝天飞行翻译 作者:admin
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 1EFF : ALL 1 52-13-31Page 440 1 1 Feb 01/02R 1 1 1CES 1


 4. Procedure
_________
 Subtask 52-13-31-420-052

 A. Installation of the Girt Bar Fittings (Ref. Fig. 410/TASK 52-13-31-991-011, 411/TASK 52-13-31-991-012)
 (1)
 Clean all the contact surfaces between components with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003) if necessary.

 (2)
 Put the girt bar fittings (110) (120) in position.

 (3)
 Install the screws (111) (121).

 (4)
 Make sure that the peripheral clearance J1 is 4 +0 -0.5 mm (0.1574 +0.0000 -0.0196 in.).

 (5)
 Adjust the position of the girt bar fittings (Ref. TASK 52-11-00-820-001).

 (6)
 Tighten the screws (111) (121).

 (7)
 Apply a bead of SEALANTS (Material No. 09-005) between the fittings

 (110) (120) and the blanking plate (112) (122).

 (8)
 Apply SEALANTS (Material No. 09-005) on the heads of the screws (111) and (121).


 5. Close-up
________
 **ON A/C 001-002,

 Subtask 52-13-31-410-056
 A. Installation of Components
R (1) Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) R (Ref. TASK 52-10-00-080-001).
 (2)
 Install the door insulation.

 (3)
 Install the door linings (Ref. TASK 25-23-46-400-002).

 (4)
 Install the escape slide (Ref. TASK 25-62-44-400-001).


 1EFF : ALL 1 52-13-31Page 441 1 1 Feb 01/02 1 1 1CES 1


 Girt Bar Fitting Adjustment Figure 411/TASK 52-13-31-991-012
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-31 Page 442 Feb 01/02

 

R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-13-31-410-056-A
 A. Installation of Components
 (1)
 Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001).

 (2)
 Install the door insulation.

 (3)
 Install the door lining panels (Ref. TASK 25-23-46-400-002).


 (4) Install the escape slide/raft (Ref. TASK 25-62-44-400-001).
 **ON A/C ALL

 Subtask 52-13-31-865-057
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
 Subtask 52-13-31-410-057
 C. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Remove all the ground support equipment, the maintenance equipment, the standard and special tools and all other items.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (4)
 Close the passenger/crew door 832 (842) (Ref. TASK 52-10-00-410-001).

 (5)
 Remove the access platform(s).


 1EFF : ALL 1 52-13-31Page 443 1 1 Aug 01/05 1 1 1CES 1 TASK 52-13-31-000-006


 Removal of the Roller and Proximity Switch Mechanism
 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 access platform 3.60 m (11 ft. 10 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew
 Doors 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
 Door
 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 52-13-31-991-019 Fig. 412 R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 52-13-31-991-019-A Fig. 412A
 1EFF : ALL 1 52-13-31Page 444 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL


 3. Job Set-up
__________
 Subtask 52-13-31-861-053

 A. Aircraft Maintenance Configuration
 (1) Energize the ground service network
 (Ref. TASK 24-42-00-861-001).
 
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