曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

R  NOTE : The specification given for the two subassemblies, and used in____ 
R  this topic, is cone/rear fuselage (FR70 to FR77) and tailcone 
R  (FR77 to FR86). 
R  (2) The basic structure of both subassemblies is similar. They are made 
R  of frames, stringers and skin panels riveted together to make the 
R  cone/rear fuselage and tailcone shells. 
R  (3) The rear pressure bulkhead is installed at FR70 in the cone/rear 
R  fuselage. The vertical stabilizer attach fittings are included on the 
R  top of FR70, FR72 and FR77 (Ref. AMM 553000). The trimmable 
R  horizontal stabilizer is installed between FR74 and FR77 (Ref. AMM 
R  551000). Four tailcone attach fittings are included on the rear face 
R  of FR77. 
R  (4) The Auxiliary Power Unit (APU) is installed in the tailcone (Ref. AMM 
R  535800). The APU compartment is a specified fire zone and firewalls 
R  close the compartment on all sides. The firewalls are made of 
R  titanium sheets. You can remove the tailcone from the aircraft as one 
R  complete unit. 
R  (5) Maintenance access doors are included in the lower right side of the 
R  two subassemblies (Ref. AMM 524100). The cone/rear fuselage access 
R  door 314AR is installed between FR78 and FR80; the APU access doors 
R  315AL and 316AR are installed between FR80 and FR84.

 EFF : ALL

53-00-00Page 7

 FUSELAGE - GENERAL - INSPECTION/CHECK
_____________________________________
 TASK 53-00-00-210-001
R Removal and Detailed Inspection of the Piston-Type Drain Valves in the Lower R Fuselage Shell
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 530000-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific clean cloth
 No specific access platform 1.8 m (5 ft. 11 in.)
 No specific access platform 2 m (6 ft. 7 in.)
 No specific 1 PROBE - NON METALLIC, FLEXIBLE

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump 52-41-00-010-002 Open the Avionics Compartment Doors for Access 52-41-00-410-002 Close the Avionics Compartment Doors after Access 53-22-14-000-001 Removal of the FWD Cargo-Compartment Floor-Panels 53-22-14-400-001 Installation of the FWD Cargo-Compartment
 Floor-Panels 53-42-14-000-001 Removal of the AFT Cargo-Compartment Floor-Panels Zone 150 53-42-14-400-001 Installation of the AFT Cargo-Compartment
 Floor-Panels Zone 150 53-42-17-000-001 Removal of the BULK Cargo-Compartment Floor-Panels 53-42-17-400-001 Installation of the BULK Cargo-Compartment
 Floor-Panels
 EFF : ALL

53-00-00Page 601

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-149, 201-299,
 53-00-00-991-001 Fig. 601 R **ON A/C 151-199, 401-499,
 53-00-00-991-001-A Fig. 601A
 **ON A/C 301-399,

 53-00-00-991-001-B Fig. 601B
 **ON A/C ALL

 3. Job Set-up
__________
 **ON A/C 001-049, 051-099, 101-149, 201-299,

 Subtask 53-00-00-010-050
 A. Get Access
 (1)
 Put the access platform in position.

 (2)
 Open the access doors 811, 824 (Ref. TASK 52-41-00-010-002). WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

_______ BEFORE YOU START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 (3)
 Open the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-00-860-001)

 (4)
 Put an access platform in position position below the cargo doors.

 EFF : ALL

53-00-00Page 602

 (5)
 Remove the floor panels 131AF, 131HF from the FWD cargo compartment (Ref. TASK 53-22-14-000-001).
　
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 FUSELAGE 機身1(32)