-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
R Material No. 19-018 USA AMS 5687
R LOCKWIRE 0.6 MM (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
R 9 air seal 36-12-04 48 -130A 51 O-rings 28-22-04 11 -050 73 cotter pins 53-58-04 01 -040
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-21-12-911-001 Tightening Torques for Pipes Unions (not for OXYGEN unions)
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)-
26-13-00-710-001 Operational Test of the APU Fire and Overheat
Detection System
27-34-00-710-001 Operational Test of the Elevator and Hydraulic
Actuation
28-22-00-710-001 Operational Test of the APU Fuel-Pump System on
Ground to Purge the Fuel Line
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
33-31-00-710-001 Operational Test of the Service Area Lighting
33-41-00-710-001 Operational Test of the Navigation Lights
33-48-00-710-002 Operational Test of the Anti-Collision/Strobe
Lighting 36-12-00-710-001 Operational Test of the APU Bleed Air Supply and Crossbleed Systems 36-22-17-400-001 Installation of the APU Overheat Sensing-Elements
EFF : ALL
53-58-11Page 432
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300)
49-00-00-710-008 Operational Test of the APU (APS 3200)
49-00-00-710-010 Operational Test of the APU (131-9(A))
49-16-00-710-001 Operational Test of the Air Intake and Diverter (GTCP
36-300)
49-16-00-710-002 Operational Test of the Air Intake Flap and Diverter
(APS 3200)
49-16-00-710-003 Operational Test of the Air Intake Flap and Diverter
(131-9(A))
49-16-41-400-001 Installation of the retractable APU Diverter (GTCP
36-300)
49-16-41-400-002 Installation of the retractable APU Diverter (APS
3200)
49-16-43-400-001 Installation of the Air Intake Flap (GTCP 36-300)
49-16-43-400-002 Installation of the Air Intake Flap (APS 3200)
51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound
51-78-00-615-002 Aircraft Cleaning after a Hydraulic Fluid Leakage
53-58-11-991-008 Fig. 401
53-58-11-991-009 Fig. 402
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
53-58-11-991-010 Fig. 403
R **ON A/C 301-399,
R 53-58-11-991-010-A Fig. 403A
R **ON A/C ALL
53-58-11-991-016 53-58-11-991-011 Fig. 404Fig. 405
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 53-58-11-991-012 Fig. 406
EFF : ALL
53-58-11Page 433
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 106-149, 211-299, 301-399, 401-499,
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 FUSELAGE 機身3(144)
