A320飞机维护手册 AMM DOORS 舱门7(43)

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 (e) Measure the operlap "E" of the safety angle (14) and the cockpit door (2).
 NOTE : The overlap "E" must be more than 2.0 mm (0.0787 in.).
____
 (f) Measure the clearance "F" of the closed cockpit door (2) and the safety angle (13).
 NOTE : The clearance "F" must be between 0.5 mm (0.0196 in.) and
____ 2.5 mm (0.0984 in.).
 (g) If one of these clearances is not in the limits, adjust the cockpit door (Ref. TASK 52-51-00-820-001).
 (2) Measure the clearances around the electrical release strikes as follows: (Ref. Fig. 501/TASK 52-51-00-991-013, 502/TASK 52-51-00-991-014)
 (a) Measure the clearance "G" of the closed cockpit door (2) and the safety angle (13) which must be smaller than 1.0 mm (0.0393 in.).
 NOTE : The top of the cockpit door (2) must always touch the
____
 safety angle (13).

 (b) Measure the clearance "J" between the latch tenon (22) and the catch (23) of the center electrical release strike (21).
 NOTE : The clearance "J" must be between 0.5 mm (0.0196 in.) and
____ 1.0 mm (0.0393 in.).
 (c) Adjust the position of center electrical release strike (21) (Ref. TASK 52-51-00-820-001) if:
 -
The clearance "G" is out of tolerance

 -
The clearance "J" is out of tolerance

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 Cockpit Door - Measurement of Clearances
 Figure 501A/TASK 52-51-00-991-013-A12 (SHEET 1)

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 Cockpit Door - Measurement of Clearances
 Figure 501A/TASK 52-51-00-991-013-A22 (SHEET 2)

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 Electrical Release Strikes - Measurement of Clearances
 Figure 502/TASK 52-51-00-991-014

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 (d) Measure the clearance "H" between the latch tenon (22) and the catch (23) of the upper and lower electrical release strikes (21).
 NOTE : The clearance "H" must be between 1.0 mm (0.0393 in.) and
____ 1.5 mm (0.0590 in.).
 (e) If the clearance "H" is not in the limits, adjust the upper and/or lower electrical release strikes (Ref. TASK 52-51-00-820-001).
 (3) Measure the clearances around the latch mechanism as follows: (Ref. Fig. 503/TASK 52-51-00-991-015)
 (a) Measure the clearance "P" between the latch tenon (23) and the slot of the access cover (17).
 NOTE : The clearance "P" must be between 3.0 mm (0.1181 in.) and
____ 5.0 mm (0.1968 in.).
 (b) Do a visible check on the three latch tenons (22) to make sure that the dimension "Q" is between 7.0 mm (0.2755 in.) and 9.0 mm (0.3543 in.).
 NOTE : The rear face of each latch tenon has three arrows marks.
____ If you can see only the last (inboard) arrow mark with the cockpit door closed, then dimension "Q" is correct.
 (c) If necessary, adjust the three latch mechanism (Ref. TASK 52-51-00-820-001).
 **ON A/C 218-220,
 Subtask 52-51-00-720-053-A
 A. Measurement of the Clearances
 (1) Measure the clearances around the cockpit door as follows: (Ref. Fig. 501A/TASK 52-51-00-991-013-A)
 (a) Measure the clearance "A" between the top of the cockpit door (2) and the cockpit-door wall-panel (1).
 NOTE : The clearance "A" must be a minimum of 4.0 mm (0.1574
____
 in.).

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 Electrical Release Strikes - Measurement of Clearances
 Figure 502A/TASK 52-51-00-991-014-A

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 Latch Mechanism - Measurement of Clearances
 Figure 503/TASK 52-51-00-991-015

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 (b) Measure the lateral clearance "B" between the cockpit door (2) and the inboard edge of the safety angle (13).
 NOTE : The clearance "B" must be a minimum of 3.7 mm (0.1456
____
 in.).

 (c) Measure the lateral clearance "C" between the cockpit door (2) and the lavatory wall (15).
 NOTE : The clearance "C" must be between 8.0 mm (0.3149 in.) and
____ 10.0 mm (0.3937 in.).
　
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