A320飞机维护手册 AMM FUSELAGE 机身3(144)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

No specific corrosion-resistant steel lockwire 0.6 mm (0.0236 in.) dia. No specific corrosion-resistant steel lockwire 0.8 mm (0.032 in.) dia
 Material No. 04-004  USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 Material No. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (Ref. 20-31-00)
 EFF : ALL
53-58-11Page 431
Aug 01/05
R
 CES

 -------------------------------------------------------------------------------
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 FUSELAGE 机身3(144)