(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE ------------------------ DESIGNATION-------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 09-005 USA MIL-S-81733 CLASS C
CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
---------FIG.ITEM ---------------|DESIGNATION -------------------------------------------------------|IPC-CSN
-------------------------------------------------------------------------------
29 cotter-pin 57-51-05 86 -010 29 cotter-pin 57-51-05 86J-010 29 cotter-pin 57-51-05 86W-010 29 cotter-pin 57-51-05 86Y-010 29 cotter-pin 57-51-05 86Z-010 43 cotter-pin 57-51-05 86 -010 43 cotter-pin 57-51-05 86J-010 43 cotter-pin 57-51-05 86W-010 43 cotter-pin 57-51-05 86Y-010 43 cotter-pin 57-51-05 86Z-010 59 cotter-pin 57-51-05 86 -010 59 cotter-pin 57-51-05 86J-010 59 cotter-pin 57-51-05 86W-010 59 cotter-pin 57-51-05 86Y-010 59 cotter-pin 57-51-05 86Z-010 72 cotter-pin 57-51-05 36H-030 72 cotter-pin 57-51-05 36T-030 80 cotter-pin 57-51-05 89A-010 80 cotter-pin 57-51-05 89C-010 80 cotter-pin 57-51-05 89E-010 80 cotter-pin 57-51-05 89F-010 98 cotter-pin 57-51-05 89A-010 98 cotter-pin 57-51-05 89C-010 98 cotter-pin 57-51-05 89E-010 98 cotter-pin 57-51-05 89F-010
1EFF : ALL 1 57-51-15Page 421 1 1 Aug 01/05R 1 1 1CES 1
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-23-11-917-001 20-28-00-912-004
27-00-00-080-002
27-50-00-866-008 27-50-00-866-009 27-54-45-400-003 29-00-00-864-001
32-12-00-010-001 32-12-00-410-001 32-43-31-400-001
R 32-43-32-400-001
R 53-35-11-400-001 Tightening practices for Hydraulic ConnectionsElectrical 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 Flap/Slat Control-Lever Locking Tool (98D27803000000)Extension of the Flaps on the GroundRetraction of the Flaps on the GroundInstallation of the Torque Shaft 6206CM(6256CM)Put the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessInstallation of the Alternate-Brake Servovalve Manifold 2614GM(2615GM) Installation of the Alternate-Brake Manifold 2853GM(2852GM)Installation of the Wing-to-Fuselage Fairings
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
57-51-15-991-002 Fig. 401 R **ON A/C 401-499, R 57-51-15-991-002-A Fig. 401A
R **ON A/C ALL
3. Job Set-up
__________ Subtask 57-51-15-941-053
A. Safety Precautions
(1) Make sure that the warning notices are in position to tell persons not to operate the flaps or the slats.
(2) Make sure that the safety barriers are in position. Subtask 57-51-15-860-051
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
(3)
Make sure that the MLG doors are open (Ref. TASK 32-12-00-010-001).
(4)
Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.
(5)
Make sure that the Yellow hydraulic system has been depressurized (Ref. TASK 29-00-00-864-001).
(6)
Make sure that the access platforms are in the correct positions in zone 570(670).
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(126)
