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时间:2011-03-21 14:21来源:蓝天飞行翻译 作者:admin
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 (c)
 Temporarily install the toothplate (108) and the locknut (110).


 (2) At the track 2 position: (Ref. Fig. 404/TASK 27-54-61-991-006, 405/TASK 27-54-61-991-013)
 CAUTION : MAKE SURE THAT THE SPLINED BUSH IS FULLY ENGAGED WITH THE
_______ SPHERICAL BEARING. THIS PREVENTS DAMAGE TO THE PARTS.
 (a)
 Apply a thin layer of COMMON GREASE (Material No. 04-022) to the bolt (181) and the splined bush (180).

 (b)
 Installation of the carriage bolt: CAUTION : THE FLAP TO CARRIAGE BOLT ASSEMBLY HAS AN INNER AND AN


_______ OUTER BOLT WHICH MAKE ONE PART. DO NOT APPLY AN END OR A TORSION FORCE TO THE INNER BOLT BECAUSE THIS WILL CAUSE DAMAGE TO THE ASSEMBLY. APPLY FORCE TO THE OUTER BOLT ONLY WHEN YOU REMOVE/INSTALL THE BOLT ASSEMBLY.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 435 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 1 Use the EXTRACTOR - PIN to install the carriage bolt (181) in


_
 the flap track carriage.

 (c)
 Install the splined bush (180) correctly over the bolt (181).

 (d)
 Remove the EXTRACTOR - PIN from the bolt (181).

 (e)
 Temporarily install the locking plate (179) and the nut (174) hand tight only.

 (f)
 Make sure that the failsafe hook nuts (184) are hand tight only.


 (3)
 Hold the trailing edge of the flap and lower the hoisting sling sufficiently to let the flap move forward.

 (4)
 Manually push the flap forward until the flap drive arms engage with the rotary actuator drive-levers.


 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
 Subtask 27-54-61-420-054-B
 D. Connect the Flap Drive Arms to the Rotary Actuator Drive-Levers
 (Ref. Fig. 403/TASK 27-54-61-991-005)

 (1) At the track 1 position:
 (a) Connect the flap drive arm to the rotary actuator drive-lever as follows:
 1 Install the bushes (85) on the rotary actuator drive-lever.
_ 2 Put and hold the packers (84) in position on the rotary
_
 actuator drive-lever.

 3 Put the rotary actuator drive-lever in position on the flap
_
 drive arm.

 4 Install the shear bolt (80), with the bolt head inboard.
_
 5 Install the washer (81) and the nut (83).

_

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 436 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 (2) At the track 2 position:


 (a) Connect the flap drive arm to the rotary actuator drive-lever as follows:
 1 Put the rotary actuator drive-lever in position on the flap
_
 drive arm.

 2 Install the bolt (86), the washer (87) and the nut (88).
_ R **ON A/C 106-149, 159-199, 211-299, 401-499,
 Subtask 27-54-61-420-054-C
 D. Connect the Flap Drive Arms to the Rotary Actuator Drive-Levers (Ref. Fig. 403A/TASK 27-54-61-991-005-B)
 (1) At the track 1 position:
 (a) Connect the flap drive arm to the rotary actuator drive-lever as follows:
 1 Put the rotary actuator drive-lever in position on the flap
_
 drive arm.

 2 Install the bolt (79), the washer (78) and the nut (76).
_
 (2) At the track 2 position:
 (a) Connect the flap drive arm to the rotary actuator drive-lever as follows:
 1 Put the rotary actuator drive-lever in position on the flap
_
 drive arm.

 2 Install the bolt (80), the washer (81) and the nut (82).
_
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 437 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 

 Subtask 27-54-61-860-056
 E. Aircraft Configuration
 (1)
 Remove the hoisting sling (Ref. TASK 27-50-00-000-002).

 (2)
 Lower the spoilers as follows:

 (a)
 Connect a pneumatic wrench to the ADAPTOR-DRIVE, SLAT (AND FLAP) and slowly move the flaps to the fully retracted position.

 (b)
 Lower the spoilers (Ref. TASK 27-60-00-866-002). NOTE : The spoiler may rest on the upper surface of the flap.

____

 (c)
 On the servo-control, make sure that the pointer on the hexagon head is opposite the letter 'O' (Operation) on the housing.

 


 Subtask 27-54-61-820-051-B
 F. Check and Adjustment of the Inboard Flap Rigged Position
 NOTE : Before you do the rigging procedure, make sure that:

____
 -
the aircraft weight is on the landing gear or on jacks

 -
the number 1 and the number 2 engines are both installed or not installed
 
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