(3)
Prevent damage to the component interface and the adjacent area.
**ON A/C ALL
TASK 27-54-49-400-003
Installation of the Flap Track 3 Actuator 6221CM(6271CM)
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 No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) FOR FIN 6271CM No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
1EFF : ALL 1 27-54-49Page 488 1 1 Aug 01/05R 1 1 1CES 1
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. 11-026 Material No. 15-007 (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)AIB TN 10138 TYPE II GRADE 1
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
Material No. 19-003 (Ref. 20-31-00)USA AMS 3819
FOR FIN 6271CM LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT
Material No. 09-019 (Ref. 20-31-00)USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 24-41-00-861-002 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)-Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
27-50-00-000-003 27-50-00-866-008 27-50-00-866-009 27-54-00-710-001 27-60-00-866-002 31-32-00-860-006 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 SystemExtension-Retraction of the Spoilers for MaintenanceProcedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
1EFF : ALL 1 27-54-49Page 489 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-54-49-000-003 Removal of the Flap Track 3 Actuator 6221CM(6271CM) (for corrective action)
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-54-49-991-003 Fig. 405
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-54-49-991-003-A Fig. 405A
FOR FIN 6221CM
27-54-45-400-007 Installation of the Torque Shafts
6214CM(6264CM)/6220CM(6270CM) 27-54-45-400-010 Installation of the Torque Shaft 6222CM(6272CM) FOR FIN 6271CM 20-28-00-869-002 Table of the Maximum Permitted Resistance Values 27-54-45-400-007 Installation of the Torque Shafts
6214CM(6264CM)/6220CM(6270CM)
27-54-45-400-010 Installation of the Torque Shaft 6222CM(6272CM)
**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 405/TASK 27-54-49-991-003)
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 405A/TASK 27-54-49-991-003-A) **ON A/C ALL
Subtask 27-54-49-941-071
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(120)
