B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (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. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
8  cotter pin  57-52-23 09 -020
 15  cotter pin  57-52-23 09 -020
 19  cotter pin  57-52-23 06A-010
 34  cotter pin  57-52-23 06A-010
 46  cotter pin  57-52-23 06A-010
 56  cotter pin  57-52-23 10 -110
 62  cotter pin  57-52-23 10 -110
 70  cotter pin  57-52-23 10 -110
 D. Referenced Information
 ------------------REFERENCE  -------------------------------DESIGNATION ------------------------------

-------------------------------------------------------------------------------
20-28-00-912-004  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)-
27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-54-41-000-001 Removal of the Right Angle Gearbox 6203CM,(6253CM) 27-54-41-400-001 Installation of the Right Angle Gearbox
 6203CM,(6253CM) 27-54-61-400-003 Installation of the Inboard Double-Slotted Flap 57-55-11-010-001 To Lower the Flap Track No. 2 Movable Fairing for
 Access
 1EFF : 301-399, 1 27-54-61Page 488 1 1 Aug 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
57-55-11-400-005 Installation of the Inboard and Outboard Flap Tab Hinge-Fairings 57-55-11-410-001 To Lift the Flap Track No. 2 Movable Fairing after
 Access 27-54-61-991-028 Fig. 413 27-54-61-991-027 Fig. 414 27-54-61-991-029 Fig. 415
 3. Job Set-up
__________
 Subtask 27-54-61-941-063
 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 landing gear.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.

 Subtask 27-54-61-865-055
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 27-54-61-860-060
 C. Aircraft Maintenance Configuration
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1) Make sure that the flaps are in the fully retracted position (Ref. TASK 27-50-00-866-009).
 1EFF : 301-399, 1 27-54-61Page 489 1 1 Aug 01/05R 1 1 1CES 1

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the slat/flap control lever.

 (3)
 Make sure that the applicable torque shaft has been disconnected (Ref. TASK 27-54-41-000-001).

 (4)
 Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft.

 (5)
 Make sure that the fairings have been removed from the tab hinges at the 1A and 1B positions (Ref. TASK 57-55-11-010-001).

 (6)
 Make sure that the flap track No. 2 movable fairing has been lowered (Ref. TASK 57-55-11-010-001).

 4. Procedure
_________
 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.
　
中國航空網 www.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6(38)