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R (b) Set the access panel (2) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 R in.) along the full width of the panel inboard end. Try and set R the clearance as near as possible to 4.0 mm (0.1574 in.). R (c) Attach the access panel (2) to the wing with the remaining camloc R fasteners (1). R (d) Fill the clearance between the access panel (2) and the trailing R edge of the wing skin with SEALANTS (Material No. 09-016). R (3) Install the access panel 575CB(675CB) (12) as follows: R (a) Put the access panel (12) in position and attach it with two of R the outer camloc fasteners (11). R (b) Set the access panel (12) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 R in.) along the full width of the panel outboard end. Try and R set the clearance as near as possible to 4.0 mm (0.1574 in.). R (c) Attach the access panel (12) to the wing with the remaining R camloc fasteners (11). R (d) Fill the clearance between the access panel (12) and the trailing R edge of the wing skin with SEALANTS (Material No. 09-016). R (4) Install the access panel 575DB(675DB) (10) as follows: R (a) Put the access panel (10) in position and attach it with two of R the outer camloc fasteners (9). R (b) Set the access panel (10) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 R in.) along each full width of the panel. Try and set the two R clearances as near as possible to 4.0 mm (0.1574 in.).
R (c) Attach the access panel (10) to the wing with the remaining R camloc fasteners (9). R (d) Fill the clearance between the access panel (10) and the trailing R edge of the wing skin with SEALANTS (Material No. 09-016). R (5) Install the access panel 575EB(675EB) (8) as follows: R (a) Put the access panel (8) in position and attach it with two of R the outer camloc fasteners (7). R (b) Set the access panel (8) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 R in.) along each full width of the panel. Try and set the two R clearances as near as possible to 4.0 mm (0.1574 in.). R (c) Attach the access panel (8) to the wing with the remaining camloc R fasteners (7). R (d) Fill the clearance between the access panel (8) and the trailing R edge of the wing skin with SEALANTS (Material No. 09-016). R (6) Install the access panel 575FB(675FB) (6) as follows: R (a) Put the access panel (6) in position and attach it with two of R the outer camloc fasteners (5). R (b) Set the access panel (6) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is between 3.0 mm (0.1181 in.) and 6.0 mm (0.2362 R in.) along the full width of the panel inboard end. Try and set R the clearance as near as possible to 4.0 mm (0.1574 in.). R (c) Attach the access panel (6) to the wing with the remaining camloc R fasteners (5). R (d) Fill the clearance between the access panel (6) and the trailing R edge of the wing skin with SEALANTS (Material No. 09-016). www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼4
