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) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D57004037000 1 EXTRACTOR FLAP SPIGOT B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 Material No. 09-001 Material No. 09-018
Material No. 11-026 Material No. 19-003 Material No. 19-010
C. Expendable Parts
USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
2 cotter pin
R 2 cotter pin
2 cotter pin
R 2 cotter pin
5 cotter pin
R 5 cotter pin
5 cotter pin
R 5 cotter pin
16 cotter pins
R 16 cotter pins
16 cotter pins
R 16 cotter pins
23 cotter pin
23 cotter pin
R 23 cotter pin
23 cotter pin
R 23 cotter pin
27 cotter pin
R 27 cotter pin
57-51-05 77C-050 57-51-05 77D-05057-51-09 23 -060 57-51-09 23A-06057-51-05 77C-080 57-51-05 77D-08057-51-09 23 -060 57-51-09 23A-06057-51-05 77C-080 57-51-05 77D-08057-51-09 23 -060 57-51-09 23A-06057-51-33 04B-01057-51-33 04C-010 57-51-33 04D-01057-51-33 24 -010 57-51-33 24A-01057-51-33 24 -230 57-51-33 24A-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 27-54-49-400-004 Installation of the Flap Track 4 Actuator
6233CM(6283CM) 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,
57-51-33-991-002-A Fig. 402
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-51-33-991-004 Fig. 404
**ON A/C ALL
3. Job Set-up
__________
Subtask 57-51-33-941-057
A. Safety Precautions
(1)
Make sure the warning notices are in the cockpit to tell persons not to operate the flaps or slats.
(2)
Make sure that the safety barriers are in position.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-51-33-860-053
B. 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 fairings of the applicable No.4 flap track have been removed (Ref. TASK 57-55-11-000-001).
(2)
Make sure that the carriage has been removed from the applicable No.4 flap track beam (Ref. TASK 27-54-46-000-001).
(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.
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(157)
