32-11-13 02E-16032-11-13 02G-110 32-11-13 01A-06032-11-13 01E-06032-11-13 01F-06032-11-13 01G-060 32-11-13 01A-05032-11-13 01E-05032-11-13 01F-05032-11-13 01G-050 32-11-13 01A-01532-11-13 01E-01532-11-13 01F-01532-11-13 01G-015 32-11-11 60A-06032-11-11 60E-05032-11-11 60F-05032-11-11 60G-060 32-11-11 60A-04032-11-11 60E-04032-11-11 60F-04032-11-11 60G-04032-11-13 01E-15032-11-13 01F-15032-11-13 01E-14032-11-13 01F-140 32-11-11 60A-07032-11-11 60G-07032-11-11 65C-01032-11-11 65D-01032-11-11 60E-05032-11-11 60F-05032-11-11 65C-14032-11-11 65D-14032-11-11 65C-15032-11-11 65D-15032-11-13 01E-15032-11-13 01F-15032-11-13 01E-14032-11-13 01F-14032-11-11 65C-01032-11-11 65D-01032-11-11 65C-150
1EFF : ALL 1 32-11-13Page 424 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
61 backing ring 32-11-11 65D-150
62 O-ring 32-11-11 65C-140
62 O-ring 32-11-11 65D-140
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations
12-12-32-611-008 Hydraulic Replenishment of the MLG Two-Stage Shock
Absorber
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)-
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
29-10-00-863-001 Pressurize the Green Hydraulic System
29-10-00-863-002 Pressurize the Yellow Hydraulic System
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-00-00-860-001 Flight Configuration Precautions with Electrical
Power
32-00-00-860-002 Ground Configuration after Flight Configuration with
Electrical Power
32-11-13-400-003 Installation of the MLG Shock-Absorber Gland-Seals
32-11-43-400-003 Installation of the 1M and 2M Harnesses on the MLG
Axle
32-12-00-010-001 Open the Main Gear Doors for Access
32-31-00-720-002 Functional Test of the Normal Extension and
Retraction of the Landing Gear
32-41-11-400-006 Installation of the MLG Wheel
(2649GM,2650GM,2651GM,2652GM)
32-42-27-400-001 Installation of the Brake
(2641GM,2642GM,2643GM,2644GM)
1EFF : ALL 1 32-11-13Page 425 1 1 May 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM LANDING GEAR 起落架2(20)