-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 27-54-45-020-050
A. Removal of the Torque Shaft 6202CM(6252CM)
(1)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on a flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the component to be removed.
(2)
Remove and discard the lockwire from the nuts (101).
(3)
Remove the nuts (101), the washers (103) and the U-bolt (102).
(4)
Remove the nuts (4) and (8), the bolts (3) and (9) and the torque shaft (2).
(5)
Remove the universal joint (1).
(6)
Remove the retaining ring (5), the pin (6) and the universal joint (7).
Torque Shafts - Flap Power Transmission Figure 402/TASK 27-54-45-991-002
1EFF : 1 1R 1CES ALL 1 11 1 27-54-45 Page 407 May 01/00
R Torque Shaft - Flap Power Transmission Figure 403/TASK 27-54-45-991-005
1EFF : 1 1 1CES ALL 1 111 27-54-45 Page 408 May 01/00
TASK 27-54-45-400-001
Installation of the Torque Shaft 6202CM(6252CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
CAUTION : MAKE SURE THE LATCH AND HINGE OF THE COUPLING DO NOT TOUCH ADJACENT
_______ COMPONENTS OR COWL DOORS (WHEN CLOSED). DO NOT USE FORCE TO ENGAGE THE SADDLE WASHER IN THE RECESS OF THE OTHER COUPLING HALF. DAMAGE TO COMPONENTS CAN OCCUR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
1EFF : ALL 1 27-54-45Page 409 1 1 May 01/00R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
Material No. 04-024 AIB AIMS 09-06-001
SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
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)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(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)
27-50-00-866-009 Retraction of the Flaps on the Ground
27-54-00-710-001 Operational Test of the Flap System
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
**ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-001 Fig. 401
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-001-A Fig. 401A -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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