R Parallel Motion for Emergency Exit Door
R Figure 504/TASK 52-22-00-991-006
1EFF : 301-399, 1 52-22-00 Page 524
1 1 May 01/04
1 1
1CES 1
R (c) Install the bush (10), the bolt (8), the washers (9) and the nut
R (11).
R NOTE : The bolt (8) must go in smoothly.____
R (d) If you can not install the bolt (8) smoothly, adjust the position
R of the lower attachment fitting (3).
R NOTE : This adjustment is the same as for the upper attachment____
R fitting (4).
R (e) Tighten the nut (11) and safety it with the new cotter pin (12).
R (6) Make sure that the motion of the door is parallel to the fuselage.
R Subtask 52-22-00-820-051
R B. Adjustment of the Skin Offset (Y-Axis of the Door)
R (Ref. Fig. 505/TASK 52-22-00-991-007, 506/TASK 52-22-00-991-008, 507/TASK
52-22-00-991-009)
R (1) Move the door rearwards and pull it inboard until the guide rollers
R (21) and (23) engage the guide fittings (22) and (24).
R (2) Measure the clearance "B" between the guide rollers (21) and (23) and
R the guide fittings (22) and (24).
R NOTE : The clearance must be between 0.1 mm (0.0039 in.) and 0.5 mm____
R (0.0196 in.).
R (3) If the clearance "B" is out of tolerance, change the position of the
R guide fittings (22) and (24) parallel to the loftline.
R (4) Make sure that the distance "D" between the head of the stop bolts
R (35) and the surface of the stop bracket (34) is pre-adjusted with
R 4.0 mm (0.1574 in.).
R (5) Operate the outboard locking handle to close the door from the outer
R side.
R (6) Examine that a minimum of three stop bolts (35) touch the related
R fuselage fitting (31).
R NOTE : Make sure that a minimum of one stop bolt (35) on each side____
R has contact.
1EFF : 301-399, 1 52-22-00Page 525 1 1 May 01/04 1 1 1CES 1R Emergency Exit Door - Guide Assembly Adjustment R Figure 505/TASK 52-22-00-991-007
1EFF : 301-399, 1 52-22-00Page 526 1 1 May 01/04 1 1 1CES 1
R Skin Offset Fuselage/Emergency Exit Door
R Figure 506/TASK 52-22-00-991-008
1EFF : 301-399, 1 52-22-00 Page 527
1 1 May 01/04
1 1
1CES 1
R Skin Offset Fuselage/Emergency Exit Door
R Figure 507/TASK 52-22-00-991-009
1EFF : 301-399, 1 52-22-00 Page 528
1 1 May 01/04
1 1
1CES 1
R (7) Measure the skin offset "C" which must be always out of wind between
R the door contour and the fuselage contour.
R NOTE : The skin offset at the forward doors must be between 0.4 mm____
R (0.0157 in.) and 3.6 mm (0.1417 in.).
R The skin offset at the rear doors must be between 0.1 mm
R (0.0039 in.) and 3.1 mm (0.1220 in.).
R (8) If the skin offset "C" is out of tolerance, adjust the stop bolts
R (35) as follows:
R (a) If necessaary, bend the lock plates (32) to release the nuts
R (33).
R NOTE : In this case, replace the lock plates (32).____
R (b) Loosen the nuts (33) and turn the stop bolts (35) as required
R until the skin offset is correct.
R NOTE : Make sure that the distance "D" is not more than 6.0 mm____
R (0.2362 in.).
R (c) TORQUE the nuts (33) to between 2.0 and 2.2 m.daN (14.74 and
R 16.22 lbf.ft).
R (d) Safety the nuts (33) with the lock plates (32).
R Subtask 52-22-00-820-052
R C. Adjustment of the Gaps around the Door (X-Axis of the Door)
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門3(68)
