• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:32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

 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 safety barriers No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001)
 27-80-00-866-005 Retracting the Slats on the Ground
 32-12-00-010-001 Open the Main Gear Doors for Access
 27-84-45-991-001 Fig. 401
 27-84-45-991-002 Fig. 402

 

 INTENTIONALLY BLANK

 

R 1 1


27-84-45Page 429
1 1 Feb 01/00 1 1 1CES 1


 INTENTIONALLY BLANK

R 1 1


27-84-45Page 430
1 1 Feb 01/00 1 1 1CES 1


 3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-052
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in position to tell persons not to operate the slat controls.

 (3)
 Put a warning notice in position to tell persons not to operate the landing gear doors.


 Subtask 27-84-45-860-067
 B. Aircraft Maintenance Configuration
 (1)
 Retract the slats fully (Ref. TASK 27-80-00-866-005).

 (2)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever on panel 114VU.


 Subtask 27-84-45-865-052
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 Subtask 27-84-45-010-052
 D. Get Access
 (1)
 Open the main gear doors (Ref. TASK 32-12-00-010-001).

 (2)
 Make sure that the GROUND LOCK SLEEVE in on the applicable main gear door actuator.

 (3)
 Put the access platform in position below zones 191, 192.


 1EFF : ALL 1 27-84-45Page 431 1 1 May 01/98R 1 1 1CES 1


 (4) Remove the applicable access panel:
 -
FOR 6010CM
 remove 191BT and 521AB


 -
FOR 6060CM
 remove 192BT and 621AB.

 

 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-84-45-991-001, 402/TASK 27-84-45-991-002)
 Subtask 27-84-45-020-053
 A. Removal of the Torque Shafts 6010CM(6060CM)
 (1)
 Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.

 (2)
 Remove the nuts (2), the bolts (4) and the shaft (3).

 (3)
 Remove the universal joint (1).

 (4)
 Remove the retaining ring (6), the pin (7) and the universal joint (5).


 1EFF : ALL 1 27-84-45Page 432 1 1 May 01/98R 1 1 1CES 1


 TASK 27-84-45-400-005
 Installation of the Torque Shaft 6010CM(6060CM)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 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 safety barriers
 No specific warning notice
 No specific Torque Wrench : range 0.20 to 3.60 m.daN


 
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7(134)