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)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 02-003
Material No. 04-018 Material No. 04-022 Material No. 09-018 Material No. 09-019 Material No. 11-026
Material No. 15-007 Material No. 19-003
C. Expendable Parts
F NSA 307110 TYPE 4
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(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
(Ref. 20-31-00)
USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 11 O-ring
11 O-ring
14 O-ring
22 cotter pin
22 cotter pin
31 O-ring
36 O-ring
29-11-05 07H-06029-11-05 07K-06027-54-05 41 -05027-54-05 25D-24027-54-05 25E-24027-54-05 40 -04029-12-05 25B-030 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart 20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage R and in the Wings (this does not include the tanks)-27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-50-00-866-008 Extension of the Flaps on the Ground
27-51-00-710-001 Operational Test of the Wing Tip Brake and the
Pressure Off Brake
27-54-45-400-008 Installation of the Torque Shafts
6216CM(6266CM)/6226CM(6276CM)
27-54-45-400-011 Installation of the Torque Shafts
6224CM(6274CM)/6230CM(6280CM) 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-10-00-864-003 Depressurize the Blue Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
R 57-51-37-000-004 Removal of the Access Panels R 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB R (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB) R 57-51-37-400-004 Installation of the Access Panels R 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB R (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
27-51-51-991-001 Fig. 401
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-51-51-991-001)
Subtask 27-51-51-941-060
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 pressurize the hydraulic systems.
1EFF : ALL 1 27-51-51Page 409 1 1 Aug 01/02 1 1 1CES 1
(3) Make sure that the warning notice is in position to tell persons not to operate the flight controls.
Subtask 27-51-51-860-053
B. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are extended fully (Ref. TASK 27-50-00-866-008).
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4(125)
