R  **ON A/C 151-199, 401-499,
 (Ref. Fig. 401A/TASK 25-55-41-991-001-A) R **ON A/C 062-099, 106-149, 151-199, 203-299, 401-499,
 (1)
 Remove the cargo net(s) (5), if installed:

 (a)
 Disconnect the net fittings (6) from the applicable net attachment fittings of the cargo-compartment floor and ceiling areas.

 (b)
 Remove the cargo net(s) (5).

 (2)
 Remove the tie-down points (2): NOTE : The removal procedure for all the tie-down points (2) is the

____ same. Therefore, the removal procedure for one tie-down point
 (2) only is given here.
 (a)
 Remove the nuts (4), and remove the screws (1) from the tie-down point (2).

 (b)
 Remove the tie-down point (2) from the structure (3).

 (3) Remove the tie-down points (8): NOTE : The removal procedure for all the tie-down points (8) is the
____ same. Therefore, the removal procedure for one tie-down point
 (8) only is given here.
 (a)
 Remove the nuts (10), and remove the screws (7) from the tie-down point (8).

 (b)
 Remove the tie-down point (8) from the plug housing (9).

 (c)
 If necessary, remove the plug housing (9) from the structure (3).

 (4) Remove the seat-track sections (12): NOTE : The removal procedure for all the seat-track sections (12) is
____ the same. Therefore, the removal procedure for one seat-track section (12) only is given here.
R  EFF : 062-099, 106-149, 151-199, 203-299, 25-55-41Page 409 401-499, Aug 01/05
 CES

 Tie-Down and Net Attachment Fittings - AFT Cargo-Compartment Floor Area Figure 401A/TASK 25-55-41-991-001-A12 (SHEET 1)
R EFF : 151-199, 401-499, 25-55-41Page 410 Aug 01/05
 CES

 Tie-Down and Net Attachment Fittings - AFT Cargo-Compartment Floor Area Figure 401A/TASK 25-55-41-991-001-A22 (SHEET 2)
R EFF : 151-199, 401-499, 25-55-41Page 411 Aug 01/05
 CES

 (a)
 Remove the nuts (13), and remove the screws (11) from the seat-track section (12).

 (b)
 Remove the seat-track section (12) from the structure (3).

 (5) Remove the tie-down fittings (15): NOTE : The removal procedure for all the tie-down fittings (15) is
____ the same. Therefore, the removal procedure for one tie-down fitting (15) only is given here.
 (a)
 Remove the nuts (16), and remove the screws (14) from the tie-down fitting (15).

 (b)
 Remove the tie-down fitting (15) from the structure (3).

 (6)
 Remove the tie-down fitting (18):

 (a)
 Remove the nuts (19), and remove the screws (17) from the tie-down fitting (18).

 (b)
 Remove the tie-down fitting (18) from the structure (3).

 (7)
 Remove the tie-down fitting (21):

 (a)
 Remove the nuts (22), and remove the screws (20) from the tie-down fitting (21).

 (b)
 Remove the tie-down fitting (21) from the structure (3).

 (8)
 Remove the tie-down fitting (24):

 (a)
 Remove the nuts (25), and remove the screws (23) from the tie-down fitting (24).

 (b)
 Remove the tie-down fitting (24) from the structure (3).

 (9)
 Remove the tie-down fittings (27): NOTE : The removal procedure for all the tie-down fittings (27) is

____ the same. Therefore, the removal procedure for one tie-down fitting (27) only is given here.
 (a)
 Remove the nuts (28), and remove the screws (26) from the tie-down fitting (27).

 (b)
 Remove the tie-down fitting (27) from the structure (3).

R  EFF : 062-099, 106-149, 151-199, 203-299, 25-55-41Page 412 401-499, Aug 01/05
 CES

 (10) Remove the tie-down fittings (30): NOTE : The removal procedure for all the tie-down fittings (30) is
____ the same. Therefore, the removal procedure for one tie-down fitting (30) only is given here.
 (a)
 Remove the nuts (31), and remove the screws (29) from the tie-down fitting (30).

 (b)
 Remove the tie-down fitting (30) from the structure (3).

 (11)
 Remove the tie-down fitting (33):

 (a)
 Remove the nuts (34), and remove the screws (32) from the tie-down fitting (33).

 (b)
 Remove the tie-down fitting (33) from the structure (3).

 
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM EQUIPMENT/FURNISHINGS 設(shè)備4(43)