SFCC 1
PPU DATE (DEG)
DATE:XXX XX UTC:XXXX
LH APPU FPPU RH APPU
***.* ***.* ***.*
***HEX ***HEX ***HEX ***
OTHER SFCC LH APPU FPPU RH APPU ***.* ***.* ***.* *** ***HEX ***HEX ***HEX
<RETURN PRINT>
Table 1 PPU DATA (DEG) displayed on the MCDU at the flap position FULL
Subtask 27-54-49-020-061
R C. Preparation for Removal
(1)
Remove the Asymmetry Position Pick-off Unit (APPU) (4) (Ref. TASK 27-51-18-000-001).
(2)
Hold the trailing edge of the flap on supports.
R (3) Use the clamp to hold the carriage in position.
NOTE : This will make sure that the carriage does not move.
____
(4) Remove the torque shaft (2) and the universal joint (1) (Ref. TASK 27-54-45-000-013):
-
FOR 6233CM
remove FIN 6232CM
-
FOR 6283CM
remove FIN 6282CM.
**ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 27-54-49-020-056
D. Removal of the Flap Track 4 Actuator 6233CM(6283CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1)
Remove the nuts (19), the washers (20), the bolts (17) and the countersunk washers (18).
(2)
Carefully remove the actuator assembly from the structure interface and the flap drive lever.
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
Subtask 27-54-49-020-056-A
D. Removal of the Flap Track 4 Actuator 6233CM(6283CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1)
Remove the nuts (12), the washers (11), the bolts (9) and the countersunk washers (10).
(2)
Carefully remove the actuator assembly from the structure interface and the flap drive lever.
**ON A/C ALL
TASK 27-54-49-400-004
Installation of the Flap Track 4 Actuator 6233CM(6283CM)
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.
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 4 mm (0.1574 in.) dia. rod
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
Material No. 04-024 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)AIB AIMS 09-06-001
SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM
Material No. 05-002 (Ref. 20-31-00)USA MIL-P-8116
Material No. 05-115 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-P-8116B
Material No. 09-018 JOINTING COMPOUND (CONDUCTIVE) (Ref. 20-31-00)USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(127)
