Subtask 27-54-48-020-050
A. Removal of the Bevel Gear Box
(1)
Remove the torque shaft (1) (Ref. TASK 27-54-45-000-009).
(2)
Remove the bolts (4) and the washers (3) from the bevel gearbox (2).
(3)
Remove the bevel gearbox (2) from the trailing edge rib and the torque shaft (5).
1EFF : ALL 1 27-54-48Page 405 1 1 Aug 01/02R 1 1 1CES 1
TASK 27-54-48-400-001
Installation of the Bevel Gear Box 6217CM(6267CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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 warning sign
No specific access platform 3 m (9 ft. 10 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
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. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
Material No. 19-003 (Ref. 20-31-00)USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R R 20-28-00-912-004 27-50-00-000-003 27-50-00-866-008 27-50-00-866-009 27-54-00-710-001 27-54-45-400-009 27-60-00-866-002 57-51-37-000-002 57-51-37-000-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Extension of the Flaps on the GroundRetraction of the Flaps on the GroundOperational Test of the Flap SystemInstallation of the Torque Shaft 6218CM(6268CM)Extension-Retraction of the Spoilers for Maintenance Removal of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB)Removal of the Access Panels
27-54-48-991-001 FOR FIN 6217CM 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)Fig. 401
R R 57-51-37-400-002 57-51-37-400-004 Installation of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB)Installation of the Access Panels
FOR FIN 6267CM 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(94)
