(2)
Make sure that the GROUND LOCK SLEEVE is correctly installed on the applicable MLG door actuating-cylinder.
(3)
Make sure the access platform is below the applicable fuel pump fairing at zone 540 (640).
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
(Ref. Fig. 401/TASK 28-21-49-991-001) R **ON A/C 106-149, 228-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 28-21-49-991-001-B)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-227,
Post SB 28-1093 For A/C 001-049,051-099,101-105,151-154,201-207,
(Ref. Fig. 401B/TASK 28-21-49-991-001-A)
**ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
(Ref. Fig. 402/TASK 28-21-49-991-002) R **ON A/C 106-149, 228-299, 301-399, 401-499,
(Ref. Fig. 402A/TASK 28-21-49-991-002-C)
**ON A/C 155-158, 208-210,
(Ref. Fig. 402B/TASK 28-21-49-991-002-A)
1EFF : ALL 1 28-21-49Page 419 1 1 Aug 01/05 1 1 1CES 1
Harness Bracket - Adjustment Details
Figure 402/TASK 28-21-49-991-002
R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 28-21-49Page 420 1201-207, 1May 01/05 1 1 1CES 1
Harness Bracket - Adjustment Details
Figure 402A/TASK 28-21-49-991-002-C
R 1EFF : 106-149, 228-299, 301-399, 401-499, 1 28-21-49Page 421 1 1 Aug 01/05 1 1 1CES 1
Harness Bracket - Adjustment Details R Figure 402B/TASK 28-21-49-991-002-A
1EFF : 155-158, 208-210, 1 28-21-49Page 422 1 1 May 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-227,
Post SB 28-1093 For A/C 001-049,051-099,101-105,151-158,201-210,
(Ref. Fig. 402C/TASK 28-21-49-991-002-B)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-227,
Subtask 28-21-49-420-052
A. Preparation for Installation
(1) There can be sealant between the fairings and the lower wing skin. If applicable, use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean all the old sealant from:
-
the cover plate (10) or (22)
-
the front fairing (8) or (20)
-
the intermediate fairing (5) or (17)
-
the rear fairing (4) or (16)
-
the lower wing skin in the related area.
R **ON A/C 106-149, 228-299, 301-399, 401-499,
Subtask 28-21-49-420-052-A
A. Preparation for Installation
(1) There can be sealant between the fairings and the lower wing skin. If applicable, use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean all the old sealant from:
-
the cover plate (11) or (24)
-
the front fairing (8) or (21)
-
the intermediate fairing (5) or (18)
-
the rear fairing (4) or (17)
-
the lower wing skin in the related area.
1EFF : ALL 1 28-21-49Page 423 1 1 Aug 01/05 1 1 1CES 1
Harness Bracket - Adjustment Details
Figure 402C/TASK 28-21-49-991-002-B
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-21-49Page 424 1201-227, 1May 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
Subtask 28-21-49-420-050
B. Installation of the Inboard Fuel Pump Fairing
NOTE : Install the inboard fuel pump fairing in this sequence:
____
-
the intermediate fairing (5)
-
the rear fairing (4)
-the front fairing (8) and the cover plate (10) assembly. NOTE : Sealant is not used between the fairings (8), (5) and (4) and the
____
lower wing skin.
(1)
Loosen the nuts (31), the bolts (32) and the clamp (33) on the bracket (34) and the guide (30).
(2)
Install the intermediate fairing (5) as follows:
(a)
Hold the intermediate fairing (5) in position near the wing skin.
(b)
Position the harness (25) inside the intermediate fairing (5).
(c)
Engage the key hole slots in the intermediate fairing (5) with the wing skin bolts.
(d)
Move the intermediate fairing (5) forward to engage the bolts fully.
(e)
Make sure that the harness (25) is not caught between:
-
the key-hole slot positions on the intermediate fairing (5) and the wing skin
-
the edge of the intermediate fairing (5) and the wing skin.
(3)
Install the rear fairing (4) as follows:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FUEL 燃油3(48)
