• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 14:35来源:蓝天飞行翻译 作者:admin
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

20-28-00-720-005 20-28-00-912-004 24-42-00-861-001  Check of the Electrical Bonding of the Different Components (But not the Fluid Systems and the Components Installed on Composite materials)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)-Energize the Ground Service Network from the External Power
 24-42-00-862-001  De-energize the Ground Service Network Supplied from the External Power
 29-14-00-614-001 29-14-00-614-002  Depressurization of the Hydraulic ReservoirsPressurization of the Hydraulic Reservoirs through the Ground Connector
 49-16-43-000-001 49-16-43-400-001 52-41-00-010-001 52-41-00-410-001  Removal of the Air Intake Flap (GTCP 36-300)Installation of the Air Intake Flap (GTCP 36-300)Open the APU Doors for AccessClose the APU Doors after Access
 49-16-41-991-006  Fig. 401 

 

 3. Job Set-up
__________ Subtask 49-16-41-860-063
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the warning notice is in position on panel 25VU to tell persons not to start the APU.

 (2)
 Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001) .

 (3)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-14-00-614-001).

 (4)
 Make sure that the access platform is in position below the access doors 312AR.

 (5)
 Make sure that the access door 312AR is open.

 (6)
 Make sure that the LIGHT control switch 3LJ is set to the ON position.

 (7)
 Make sure that the access platform is in position below the APU access doors 315AL, 316AR and the maintenance door 314AR.

 (8)
 Make sure that the maintenance door 314AR is open.

 (9)
 Make sure that the APU access doors 315AL, 316AR are open (Ref. TASK 52-41-00-010-001) .


 (10)
 Make sure that the LIGHT control swtich 11LJ is set to the ON position.

 (11)
 Make sure that the air intake flap is removed (Ref. TASK 49-16-43-000-001).

 


 4. Procedure
_________
 (Ref. Fig. 401/TASK 49-16-41-991-006) Subtask 49-16-41-140-050
 A. Preparation for installation. WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 (1)
 Remove all used sealant from component interface and/or adjacent area of the aircraft structure with a non-metallic scraper.

 (2)
 Clean the component interface of the aircraft structure with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.

 (3)
 Make sure that the component interface of the fixed diverter (12) is clean of sealant.


 NOTE : If there is sealant on the component interface of the fixed
____ diverter, clean it with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
 Subtask 49-16-41-420-055
 B. Installation of the fixed Diverter. WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
 (1)
 Apply SPECIAL MATERIALS (Material No. 05-013) with a non-metallic scraper to the surfaces of the fixed diverter (12) and the component interface of the aircraft structure.

 (2)
 Apply SEALANTS (Material No. 09-019) with a non-metallic scraper to the surfaces of the fixed diverter (12) and the component interface of the aircraft structure.


 NOTE : Make sure that the screw holes do not show any signs of
____
 sealant.

 (3)
 Put the fixed diverter (12) in position and install the screws (9) and the washers (10), (11) and tighten them.

 (4)
 Install the screws (7) and the washers (8).

 (5)
 Apply SEALANTS (Material No. 09-016) to the SEALANT AREA.

 (6)
 Install the screws (4) and clean them from the seleant with a lint-free cloth.

 (7)
 Install the washers (6) and the nuts (5).

 (8)
 Put the shim (3) between the FR77 and the fixed diverter (12). NOTE : If necessary use one or two shims.

____

 (9)
 Install the screws (1) and the washers (2).

 


 (10)
 Make sure that the electrical bonding of the screws (1) is not higher than 2 milliohms (Ref. TASK 20-28-00-720-005).

 (11)
 Bond the head of the screws (1) with washers (2) (Ref. TASK 20-28-00-912-004).

 (12)
 Apply a bead of MISCELLANEOUS (Material No. 19-016) between the fixed diverter and the aircraft structure and make it smooth.
 
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 机载辅助动力 AIRBORNE AUXILIARY POWER2(152)