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时间:2011-03-21 14:32来源:蓝天飞行翻译 作者:admin
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 4. Procedure
_________
 Subtask 27-84-44-420-065
 A. Preparation for Installation
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.


 (1)
 Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-004) to clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (4)
 Apply a layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to:

 -
the mating faces of the steady bearing (35) and the nose rib (36)

 -
the shanks of the bolts (33).

 


 Subtask 27-84-44-420-066
 B. Installation of the Steady Bearing FIN 6025CM (6075CM)
 (1)
 Use the bolts (33) to attach the steady bearing (35) and the anti-flailing cap (32) to the nose rib (36).

 (2)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the bolts (33) and the flange of the steady bearing (35).


 Subtask 27-84-44-410-054
 C. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable torque shaft (37) (Ref. TASK 27-84-45-400-011):

 -
FOR 6025CM
 install the torque shaft FIN 6024CM


 -
FOR 6075CM
 install the torque shaft FIN 6074CM.

 


 (3)
 Install the applicable torque shaft (34) (Ref. TASK 27-84-45-400-008):

 -
FOR 6025CM
 install the torque shaft FIN 6026CM


 -
FOR 6075CM
 install the torque shaft FIN 6076CM.

 


 (4)
 Install the applicable access panels 521EB, 522AB, 522CB (621EB, 622CB, 622EB).

 


 Subtask 27-84-44-865-061
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-44-710-054
 E. Test
 (1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001).
 5. Close-up
________ Subtask 27-84-44-942-054
 A. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 


 TASK 27-84-44-000-006
 Removal of the Steady Bearing FIN 6031CM(6081CM)
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 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)
 No specific safety barriers
 No specific warning notice(s)
 No specific adjustable access platform 3.6 m (11 ft. 10 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-84-44-991-001 Fig. 401 27-84-44-991-002 Fig. 402 FOR FIN 6081CM 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001)
 27-84-45-000-007  Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM)


 3. Job Set-up
__________
 (Ref. Fig. 401/TASK 27-84-44-991-001, 402/TASK 27-84-44-991-002)
 
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