A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(3)

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

Subtask 27-84-45-420-077
 B. Installation of the Torque Shafts
 (1) Install the universal joint (8).
 (2) Install the shaft (9) and attach it with the bolts (11) and the nuts (10).
 (3) TORQUE the nuts (10) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
 (4) Apply STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (10) - the bolts (11) - the flange of the universal joint (8) - the flanges of the shaft (9). 
R  (5) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-000-003): - from the torque shaft, inboard of the applicable component - from the torque shaft, outboard of the applicable component.

 

 Subtask 27-84-45-210-067
R  C. Dimensional/Visual Checks (Ref. Fig. 402/TASK 27-84-45-991-002) 
R R R R R R (1) Make sure that: - you cannot see the spline engagement groove at the movable joint - the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint. 
Subtask 27-84-45-865-077
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-45-710-055
 E. Test 
R R  (1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
 5. Close-up________ 
R  (Ref. Fig. 401/TASK 27-84-45-991-001)
 Subtask 27-84-45-865-078
 A. 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 27-84-45-410-055
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panel:

 -
FOR 6016CM
 install 521EB

 -
FOR 6020CM
 install 521EB

 -
FOR 6026CM
 install 522AB

 -
FOR 6030CM
 install 522CB

 -
FOR 6066CM
 install 621EB

 -
FOR 6070CM
 install 621EB

 -
FOR 6076CM
 install 622AB

 -
FOR 6080CM
 install 622CB.

 

 

 Subtask 27-84-45-865-079
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 27-84-45-942-056
 D. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 27-84-45Page 469 1 1 Feb 01/00R 1 1 1CES 1

 TASK 27-84-45-000-008
R Removal of the Torque Shaft 6018CM(6068CM)
 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.
 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 access platform 3.8 m (12 ft. 6 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
 27-84-44-000-002 Removal of the Steady Bearings FIN
　
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8(3)