• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:47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

 (4)
 Remove the access platform(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 


 FAIRINGS - WING TO FUSELAGE - REMOVAL/INSTALLATION
__________________________________________________
 TASK 53-25-11-000-001
 Removal of the Wing-to-Fuselage Fairings (191AT, 191AB, 192AT, 192AB)
 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.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific access platform 3.5 m (11 ft. 6 in.)

 B. Referenced Information -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-25-11-991-001 Fig. 401
 **ON A/C 301-399,

 53-25-11-991-001-A Fig. 401A
 EFF : ALL
53-25-11Page 401


 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-25-11-991-002  Fig. 402
 **ON A/C 301-399,
 53-25-11-991-002-A  Fig. 402A
 **ON A/C ALL
 53-25-11-991-003  Fig. 403
 3. Job Set-up__________
 Subtask 53-25-11-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR COND/RAM/AIR/INLET 1HZ D10 106VU CSM/G /EV/MAN/SPLY 6XE B04 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R  122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC  21HH 23HH 1HH 3HH 24HH 22HH  W22W21X22X21Y21Y20 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302, 
R  122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC  4HH  Y19

 EFF : ALL
53-25-11Page 402


R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 
R R  122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC **ON A/C 106-149, 303-399,  2HH  Y18 
R  122VU  4HH  Y19
 **ON A/C ALL
 Subtask 53-25-11-869-052
 B. Aircraft Maintenance Configuration (1) Make sure that the slats are extended (Ref. TASK 27-80-00-866-004). Subtask 53-25-11-010-050
 C. Get Access
 (1) Put the access platform in position in the zones 191 and 192. 4. Procedure_________ Subtask 53-25-11-020-051
R  A. Removal of the Fairing-Wing to Fuselage **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 53-25-11-991-001) **ON A/C 301-399,
 (Ref. Fig. 401A/TASK 53-25-11-991-001-A)

 EFF : ALL
53-25-11Page 403


 Fairing - Left Access Panels Figure 401/TASK 53-25-11-991-001 
R  EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,  53-25-11 Page 404 Aug 01/05
 CES 

 

R R  Fairing - Left Access Panels Figure 401A/TASK 53-25-11-991-001-A 
R  EFF :  301-399,  53-25-11 Page 405 May 01/04
 CES 

 

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 402/TASK 53-25-11-991-002)
 
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2(33)