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时间:2011-03-26 23:52来源:蓝天飞行翻译 作者:admin
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R  (b) Prepare the shim washer (126) so that the distance "E" is 
R  correct. 
R  (c) Install the stop bolt (124) together with the shim washer (126), 
R  the washers (125) and (128) and the nut (127). 
R  (8) Remove the rigging pins (91) and (97).

 1EFF : 301-399, 1 52-22-00Page 544 1 1 May 01/04 1 1 1CES 1 1EFF : 301-399, 1 52-22-00Page 545 1 1 May 01/04 1 1 1CES 1 1EFF : 301-399, 1 52-22-00Page 546 1 1 May 01/04 1 1 1CES 1R Adjustment of the Drift Pin and the Locking Hook R Figure 514/TASK 52-22-00-991-018


R  (9) Adjust the dead center position of the locking shaft (103) as 
R  follows: 
R  (a) Move the inboard lever (77) up and put an adjustment gage (129) 
R  between the stop bolt (119) and the actuation lever (105). 
R  NOTE : The thickness of the adjustment gage (129) must be between____ 
R  2.6 mm (0.1023 in.) and 2.8 mm (0.1102 in.). 
R  (b) If required, cut and remove the lockwire from the nut (116). 
R  (c) Turn the adjustment screw (115) of the actuation lever (105) 
R  until it touches the surface of the indication lever (117). 
R  (d) Tigthen the nut (116) and safety it with the lockwire, corrosion 
R  resistance steel, dia 0.8 mm (0.30 in.) on the actuation lever 
R  (105). 
R  (10) Adjust the indication of the locking mechanism as follows: 
R  (a) Move the inboard lever (77) up so that the door is fully lifted. 
R  (b) Make sure that the red "UNLOCKED" label (100) is in the center of 
R  the indication plate (101). 
R  (c) If not, loosen the screws (102), put the indication plate (101) 
R  in the correct position as required and tighten the screws (102) 
R  again. 
R  (d) Move the inboard lever (77) down to close the door. 
R  (e) Make sure that the green "LOCKED" label (99) is in the center of 
R  the indication plate (101). 
R  (f) If not, replace the self-adhesive labels (99) and (100) so that 
R  they are in the correct center position of the indication plate 
R  (101).

 

R  Subtask 52-22-00-820-056 
R  C. Adjustment of the Drift Pin Assembly and the Locking Hook 
R  (Ref. Fig. 514/TASK 52-22-00-991-018) 
R  (1) Measure the clearance "J" between the top of the drift pin assembly 
R  (141) and the fuselage beam (142). 
R  NOTE : The clearance "J" must be between 2.7 mm (0.1062 in.) and 3.3____ 
R  mm (0.1299 in.). 
R  (2) If the clearance "J" is out of tolerance, add or remove the upper the 
R  adjustment washers (143) and (144) as follows: 
R  (a) Open the door to get access to the top of the drift pin assembly 
R  (141). 
R  (b) Remove the stop screw (147) together with the adjustment washers 
R  (143) and (144) and the sealing assy (146). 
R  (c) Add or remove the upper the adjustment washers (143) and (144) as 
R  required until the clearance "J" is correct. 
R  (d) Install the stop screw (147) together with the adjustment washers 
R  (143) and (144) and the sealing assy (146). 
R  (e) TORQUE the stop screw (147) to between 0.6 and 0.7 m.daN (53.09 
R  and 61.94 lbf.in). 
R  (f) Close the door again. 
R  (3) Measure the clearance "G" and "H" between the locking hook (133) and 
R  the lock fitting (132). 
R  NOTE : The clearance "G" and "H" must be between 0.5 mm (0.0196 in.)____ 
R  and 0.1 mm (0.0039 in.). 
R  (4) If the clearance "G" is out of tolerance, adjust the length of the 
R  connection rod (136) as follows: 
R  (a) If required, cut and remove the lockwire and loosen the jam nuts 
R  (134). 
R  (b) Turn the rod (137) until the clearance "G" is correct.

 

 1EFF : 301-399, 1 52-22-00Page 547 1 1 May 01/04 1 1 1CES 1 1EFF : 301-399, 1 52-22-00Page 548 1 1 May 01/04 1 1 1CES 1


R  (c) Tigthen the jam nuts (134) and safety them with the lockwire, 
R  corrosion resistance steel, dia 0.8 mm (0.30 in.) on the locking 
R  devices (135). 
R  (5) If the clearance "H" is out of tolerance, change the position of the 
 
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