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 notices
 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) No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D57004037000 1 EXTRACTOR FLAP SPIGOT B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002  USA MIL-P-8116
 Material No. 09-001  PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-S-8802 TYPE I CLASS A
 Material No. 09-018  FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT
 Material No. 11-026 Material No. 19-003  (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819
 Material No. 19-010  LINT-FREE COTTON CLOTH (Ref. 20-31-00)USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
2  cotter pin 
R  2  cotter pin 
2  cotter pin 
R  2  cotter pin 
5  cotter pins 
R  5  cotter pins 
5  cotter pins 
R  5  cotter pins 
16  cotter pins 
R  16  cotter pins 
16  cotter pins 
R  16  cotter pins 
23  cotter pin 
R  23  cotter pin 
24  cotter pin 
24  cotter pin 
R  24  cotter pin 
27  cotter pin 
R  27  cotter pin 
28  cotter pin 

57-51-05 75C-040 57-51-05 75D-04057-51-09 21 -060 57-51-09 21A-06057-51-05 75C-070 57-51-05 75D-07057-51-09 21 -090 57-51-09 21A-09057-51-05 75C-070 57-51-05 75D-07057-51-09 21 -090 57-51-09 21A-09057-51-33 22 -010 57-51-33 22A-01057-51-33 02B-01057-51-33 02C-010 57-51-33 02D-01057-51-33 22 -230 57-51-33 22A-23057-51-33 22 -230 -------------------------------------------------------------------------------

FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
cotter pin  57-51-33 22A-230
 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)-
27-54-46-000-001 Removal of the Nos. 2, 3 and 4 Flap Carriages 27-54-46-400-001 Installation of the Nos 2, 3 and 4 Flap Carriages 27-54-49-400-002 Installation of the Flap Track 2 Actuator
 6211CM(6261CM) 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
 4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 4
 **ON A/C 301-399,
　
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 WINGS 機翼3(144)