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时间:2011-03-21 14:12来源:蓝天飞行翻译 作者:admin
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R  asymmetric rigging value from track 3 label (42), +/- 4 mm 
R  (0.16 in.). 
R  (3) If the flap rigged position is not correct, adjust as necessary until 
R  the flap is in the specified limits (Ref. TASK 27-51-00-820-008). 

R 1EFF : 051-052, 1 27-51-00Page 589 1 1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,

 

 Subtask 27-51-00-220-057-A
 C. To Do a Check of the Outboard Flap Rigged Position
 **ON A/C 062-099, 151-153, 204-207,

 (Ref. Fig. 511/TASK 27-51-00-991-060) R **ON A/C 106-149, 154-199, 208-299, 401-499,
 (Ref. Fig. 511A/TASK 27-51-00-991-060-A) R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
 (Ref. Fig. 512A/TASK 27-51-00-991-058-A)
 NOTE : The tolerances given in the work steps that follow are in-service

____ tolerances only. They are not initial adjustment tolerances. The tolerances for initial adjustment are given in the flap rigged position adjustment procedure (Ref. TASK 27-51-00-820-008).
 NOTE : The scale must be read from the outboard side of the flap track
____
 beam.

 (1) At the track 3 and track 4 positions, make sure that the top surface of the trailing edge aligns with the scale block (41) as follows:
 (a)
 Check the value shown on the label (42) attached to the outboard side of the flap track 3 beam.

 (b)
 If the value on the label (42) is '0', make sure that the trailing edge aligns with the zero mark +/- 4 mm (0.16 in.).

 (c)
 If the value on the label (42) shows a plus value, subtract this value from the dimension shown on the scale block (41). The remaining value must be zero +/- 4 mm (0.16 in.).

 (d)
 If the value on the label (42) shows a minus value, add this value to the dimension shown on the scale block (41). The remaining value must be zero +/- 4 mm (0.16 in.).


R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-51-00Page 590 1401-499, 1Aug 01/05 1 1 1CES 1


 (2) If the flap rigged position is not correct, adjust as necessary until the flap is in the specified limits (Ref. TASK 27-51-00-820-008).
 **ON A/C 301-399,
 Subtask 27-51-00-220-057-D
 C. To Do a Check of the Outboard Flap Rigged Position (Ref. Fig. 511B/TASK 27-51-00-991-060-B, 512B/TASK 27-51-00-991-058-B)
 NOTE : The tolerances given in the work steps that follow are in-service
____ tolerances only. They are not initial adjustment tolerances. The tolerances for initial adjustment are given in the flap rigged position adjustment procedure (Ref. TASK 27-51-00-820-009).
 NOTE : The scale must be read from the outboard side of the flap track
____
 beam.

 (1)
 At the track 3 and track 4 positions, make sure that the top surface of the trailing edge aligns with the scale block (41) as follows:

 (a)
 Check the value shown on the label (42) attached to the outboard side of the flap track 3 beam.

 (b)
 If the value on the label (42) is '0', make sure that the trailing edge aligns with the zero mark +/- 4 mm (0.16 in.).

 (c)
 If the value on the label (42) shows a plus value, subtract this value from the dimension shown on the scale block (41). The remaining value must be zero +/- 4 mm (0.16 in.).

 (d)
 If the value on the label (42) shows a minus value, add this value to the dimension shown on the scale block (41). The remaining value must be zero +/- 4 mm (0.16 in.).

 

 (2)
 If the flap rigged position is not correct, adjust as necessary until the flap is in the specified limits (Ref. TASK 27-51-00-820-009).


R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-51-00Page 591 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


R  **ON A/C 001-001, 
R  Subtask 27-51-00-080-050 
R  D. Removal of the Rigging Tools 
R  (1) Remove the KIT-FLAP RIGGING (98D27504038000): 
R  (Ref. Fig. 504/TASK 27-51-00-991-018) 
R  - for the inboard flap, from the flap track 2 beam assembly 
R  - for the outboard flap, from the flap track 3 beam assembly. 
R  (a) Remove the pin (12) and remove the fin (11) from the base 
R  assembly (15). 
R  (b) Hold the base assembly (15) and loosen the knurled screws (17). 
R  (c) Move the two lower clamps (16) clear of the flap track beam (18) 
R  and remove the base assembly (15). 

R  (Ref. Fig. 503/TASK 27-51-00-991-017) 
R  (2) Remove the PIN RIGGING-FLAPS (TRACK 1) (1) at the track 1 position. 
R  **ON A/C 002-049, 053-061, 101-105, 201-203, 
 
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