(2)
Remove the applicable access panels:
-
FOR 6012CM
remove 521AB, 521CB and 521BB, 191BT
-
FOR 6062CM
remove 621AB, 621CB and 621BB, 192BT.
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4. Procedure
_________
(Ref. Fig. 403/TASK 27-84-45-991-003) Subtask 27-84-45-020-054
A. Removal of the Torque Shafts 6012CM(6062CM)
(1)
Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.
(2)
Remove the nuts (36) and (38), the bolts (37) and (39) and then the shaft (29). If applicable, remove the spacers.
(3)
Remove the nuts (32), the bolts (31) and the shaft (30). NOTE : Spacers between the universal joint (35), the shaft (30) and
____ the shaft (29) adjust the length of the transmission. It is possible that there are none or more than one installed.
(4)
Remove the universal joint (28).
(5)
Remove the retaining ring (34), the pin (33) and the universal joint (35).
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R Torque Shafts - Slat Power Transmission Figure 403/TASK 27-84-45-991-003
1EFF : 1 1 1CES ALL 1 111 27-84-45 Page 442 May 01/05
TASK 27-84-45-400-006
Installation of the Torque Shaft 6012CM(6062CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-80-00-866-005 Retracting the Slats on the Ground
27-84-00-710-001 Operational Test of the Slat System
27-84-45-991-001 Fig. 401
27-84-45-991-002 Fig. 402
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-84-45-991-001)
Subtask 27-84-45-941-062
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-055
B. Aircraft Maintenance Configuration
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(137)
