• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:21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

 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
 **ON A/C 001-003, 051-052,
 27-64-44-991-001  Fig. 401
 **ON A/C 004-049, 053-099, 101-149, 201-299,
 27-64-44-991-001-A  Fig. 401A
R **ON A/C 151-199, 301-399, 401-499,
 27-64-44-991-001-B  Fig. 401B
 **ON A/C 001-003, 051-052,
 27-64-44-991-002  Fig. 402
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 27-64-44-991-002-A  Fig. 402A **ON A/C ALL


 3. Job Set-up
__________
 **ON A/C 001-003, 051-052,

 (Ref. Fig. 401/TASK 27-64-44-991-001)
 **ON A/C 004-049, 053-099, 101-149, 201-299,

 (Ref. Fig. 401A/TASK 27-64-44-991-001-A) R **ON A/C 151-199, 301-399, 401-499,
 (Ref. Fig. 401B/TASK 27-64-44-991-001-B)
 **ON A/C ALL

 Subtask 27-64-44-941-055
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notice is in position to tell persons not to pressurize the hydraulic systems.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.


 Subtask 27-64-44-860-052
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap and slat control lever on panel 114VU.

 (2)
 Make sure that the spoiler 4 is extended (Ref. TASK 27-60-00-866-002).

 (3)
 Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.

 


 Subtask 27-64-44-865-051
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
 4. Procedure
_________
 **ON A/C 001-003, 051-052,

 (Ref. Fig. 401/TASK 27-64-44-991-001)
 **ON A/C 004-049, 053-099, 101-149, 201-299,

 (Ref. Fig. 401A/TASK 27-64-44-991-001-A) R **ON A/C 151-199, 301-399, 401-499,
 (Ref. Fig. 401B/TASK 27-64-44-991-001-B)
 **ON A/C 001-003, 051-052,

 (Ref. Fig. 402/TASK 27-64-44-991-002) R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 402A/TASK 27-64-44-991-002-A) **ON A/C ALL


 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
 EDGE:

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.


 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 **ON A/C 001-049, 051-099, 101-149, 201-299,
 Subtask 27-64-44-560-050
 A. Preparation of a Replacement Component
 (1) Put the SPOILER MAINTENANCE KEY (98D27603002000) or the SPOILER MAINTENANCE KEY (98D27603002001) into the maintenance device of the applicable spoiler servo-control and turn it to the maintenance position.

R **ON A/C 151-199, 301-399, 401-499,
 Subtask 27-64-44-560-050-A
 A. Preparation of a Replacement Component
 (1) Make sure that the pointer of the maintenance device on the applicable spoiler servo-control is in the 'M' (Maintenance) position.
 **ON A/C 001-003, 051-052,
 Subtask 27-64-44-420-051
 B. Preparation for Installation
 (1)
 Clean the component interface and/or the adjacent with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 


 If the spoiler is safetied with STA-LOK nuts, do the steps that follow:
 (4)
 If the shaft (23) is removed:

 -install the shaft (23) in the hinge fitting
 -attach the spoiler 3 (Ref. TASK 27-64-43-400-001).

 (5)
 Apply COMMON GREASE (Material No. 04-022) to the:

 -
hinges on the rear spar

 -
hinges on the spoiler
 
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 FLIGHT CONTROLS 飞行操纵6(167)