-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-21-11-911-001 Tightening Torques for Standard Threaded Fasteners
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)-
21-00-00-100-001 Cleaning of Special Components in the Environmental
Control System (ECS)
21-00-00-615-001 Decontamination of the Environmental Control System
(ECS) when the Temperature is below 24 deg.C (APU)
21-00-00-615-002 Decontamination of the Environmental Control System
(ECS) when the Temperature is above 24 deg.C (APU)
24-23-51-400-001 Installation of the APU Generator 8XS
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
28-22-00-710-001 Operational Test of the APU Fuel-Pump System on
Ground to Purge the Fuel Line
28-22-14-400-001 Installation of the APU Fuel LP-Switch 5030QM
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
49-00-00-080-001 Removal of the APU Hoist Tool (APS 3200)
49-00-00-480-001 Installation of the APU Hoist Tool (APS 3200)
49-00-00-710-005 Self-Test of the ECB (APS 3200)
49-00-00-710-008 Operational Test of the APU (APS 3200)
49-00-00-790-002 Leak Test of the APU (APS 3200)
49-00-00-790-005 Air Leak Test with closed APU Doors
49-00-00-860-011 Update of APU Data (hours/cycles) (APS 3200)
49-12-00-210-004 Detailed Visual Inspection of APU Suspension Rods,
Shockmounts Structure including Brackets and Visible
Part of Attachment Fittings (APS 3200)
49-12-54-400-002 Installation of the APU Mount Brackets 4065KM,
4975KM, 4085KM (APS 3200)
49-17-00-200-001 Inspect the APU Drain System (APS 3200)
49-51-42-000-003 Air By-Pass Duct - Removal (APS 3200)
49-51-42-400-003 Air By-Pass Duct - Installation (APS 3200)
49-52-41-000-002 Removal of the Oil Cooler Outlet Duct (APS 3200)
49-52-41-400-002 Installation of the Oil Cooler Outlet Duct (APS 3200)
49-81-00-200-004 Visual Check of the Sealing Ring Coupling, V-Clamp
and Portion of Exhaust Duct Inside of the APU
Compartment (APS 3200)
49-81-00-200-005 Visual Check of the Sealing-Ring Coupling Bellows
(APS 3200)
49-81-41-000-002 Removal of the Exhaust Muffler (APS 3200)
49-81-41-400-002 Installation of the Exhaust Muffler (APS 3200)
49-90-00-600-004 Check Oil Level and Replenish (APS 3200)
49-91-42-200-003 Inspection of the Magnetic Drain Plug (APS 3200)
52-41-00-010-001 Open the APU Doors for Access
52-41-00-410-001 Close the APU Doors after Access
52-41-21-000-001 Removal of the APU Access Door 315AL
52-41-21-400-001 Installation of the APU Access Door 315AL
52-41-22-000-001 Removal of the APU Access Door 316AR and the related
Door Mechanism
52-41-22-400-001 Installation of the APU Access Door 316AR and the
related Door Mechanism
49-11-11-991-006 Fig. 401
49-11-11-991-008 Fig. 402
49-11-11-991-005 Fig. 403
49-11-11-991-007 Fig. 404
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 機載輔助動力 AIRBORNE AUXILIARY POWER2(59)
