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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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 (c)
 Assemble the side-plate (62) and the thumb-nut (61) to the body assembly (65).

 (d)
 Adjust the screw (66) with the knob (64) until the flap carriage

 (60)
 is held in position.

 

 (3)
 At the track 2 position, install the KIT-FLAP RIGGING
 (98D27504038001):


 (a)
 Install the base assembly (71) on the flap track beam (76). Make sure that the aft dowels (73) touch the track beam end-stop (72).

 (b)
 Move the two bottom clamps (74) into position below the flap track beam (76) and tighten the knurled screws (75).

 (c)
 Move the fin (69) into position on the base assembly (71) and install the pin (70).

 (d)
 Put the scale block (68) on the fin (69).

 


 1EFF : 001-049, 051-061, 101-103, 201-203, 1 27-51-00Page A555 1 1 Aug 01/05R 1 1 1CES 1


 Rigging Kit Installation - Inboard Flap
 Figure 523A/TASK 27-51-00-991-073-A12 (SHEET 1)

R 1EFF : 002-049, 051-061, 101-103, 201-203, 1 27-51-00Page A556 1 1 Aug 01/05 1 1 1CES 1


 Rigging Kit Installation - Inboard Flap
 Figure 523A/TASK 27-51-00-991-073-A22 (SHEET 2)

R 1EFF : 002-049, 051-061, 101-103, 201-203, 1 27-51-00Page A557 1 1 Aug 01/05 1 1 1CES 1


 (4) Disconnect the flap drive-arm (4) and the rotary actuator drive-lever

 (5) at the track 1 position (Ref. TASK 27-54-61-000-001). R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
 Subtask 27-51-00-480-061-B
 G. Install the Inboard Flap Rigging Kit (Ref. Fig. 518/TASK 27-51-00-991-068, 523B/TASK 27-51-00-991-073-B)
 (1)
 Install the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) (1) in the drive-lever (5) at track 1.

 (2)
 At the track 1 position install the TOOL RESTRAINING TK1 (98D27504040000).

 (a)
 Put the body assembly (64) in position on the flap track beam (62).

 (b)
 Connect the stop (66) to the flap carriage (60).

 (c)
 Install the spigot (62) through the flap track beam (62) into the body assembly (64).

 (d)
 Adjust the screw (65) with the knob (63) until the flap carriage

 (60)
 is held in position.

 

 (3)
 At the track 2 position, install the KIT-FLAP RIGGING (98D27504038000):

 (a)
 Install the base assembly (71) on the flap track beam (76). Make sure that the aft dowels (73) touch the track beam end-stop (72).

 (b)
 Move the two bottom clamps (74) into position below the flap track beam (76) and tighten the knurled screws (75).

 (c)
 Move the fin (69) into position on the base assembly (71) and install the pin (70).

 (d)
 Put the scale block (68) on the fin (69).

 

 (4)
 Disconnect the flap drive-arm (4) and the rotary actuator drive-lever


 (5) at the track 1 position (Ref. TASK 27-54-61-000-001).
R 1EFF : 002-049, 051-099, 101-149, 151-199, 1 27-51-00Page A558 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-061, 101-103, 201-203,


 Subtask 27-51-00-820-075
 H. Set the Main Eccentric Bearings of the Inboard Flap to the Zero Datum Position
 (Ref. Fig. 521/TASK 27-51-00-991-071, 524/TASK 27-51-00-991-074)
 NOTE : The main eccentric bearings are spherical bearings installed in
____
 the flap attachment fittings at the flap carriages.

 At track 1, an eccentric bush (86) is installed in the bearing
 (87). A pin on the eccentric bush (86) engages with the toothplate
 (85). The bearing (87) is at zero datum when the pin on the
 eccentric bush (86) is at the position shown.
 (Ref. Fig. 524/TASK 27-51-00-991-074)
 Detail D.

 At track 2, red paint marks on the bearing and on the fitting show
 the zero datum position. The bearing is at the zero datum position
 when the red paint marks are aligned.
 (Ref. Fig. 521/TASK 27-51-00-991-071)

 Adjust the bearings at one position then the other in small
 increments.

 (1) At the track 1 position set the main eccentric bearing to the zero datum position as follows:
 (a) Remove these items:
 -
the bolt (80)

 -
the tabwasher (81)

 -
the stop (82)

 -
the nut (83)

 -
the lockwasher (84)

 -
the toothplate (85).


 (b) Use the TOOL-FLAP ADJUSTING (98D27504002000) to move the eccentric bush (86) to the position shown. (Ref. Fig. 524/TASK 27-51-00-991-074) Detail D.
 
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