(Ref. Fig. 403B/TASK 32-11-16-991-005-B) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 404/TASK 32-11-16-991-007)
**ON A/C 301-399,
(Ref. Fig. 404A/TASK 32-11-16-991-007-A)
**ON A/C 001-003, 051-052,
Subtask 32-11-16-560-050
A. Preparation for a Replacement Side-Stay Assembly
(1)
Make sure that the lockstay has been safetied to the side-stay.
(2)
Install the SPLINT ASSEMBLY - SIDE STAY (98D32104013001) on the side-stay assembly (19) with:
-
the cables to the wing surface
-
the strap to the wing surface
-
the center joint of the side-stay located in the center hole of the side-stay splint assembly.
(3)
Tighten the strap and connect the cables to the hook. Tighten the cable.
1EFF : ALL 1 32-11-16Page 433 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 401-499,
Subtask 32-11-16-560-050-A
A. Preparation for a Replacement Side-Stay Assembly
(1)
Make sure that the lockstay has been safetied to the side-stay.
(2)
Install the SPLINT ASSEMBLY - SIDE STAY (98D32104013001) on the side-stay assembly (6) with:
-
the cables to the wing surface
-
the strap to the wing surface
-
the center joint of the side-stay located in the center hole of the side-stay splint assembly.
(3)
Tighten the strap and connect the cables to the hook. Tighten the cable.
**ON A/C 301-399,
Subtask 32-11-16-560-050-C
A. Preparation for a Replacement Side-Stay Assembly
(1)
Make sure that the lockstay has been safetied to the side-stay.
(2)
Install the HOIST (98D32104013004) on the side-stay assembly (6) with:
-
the cables to the wing surface
-
the strap to the wing surface
-
the center joint of the side-stay located in the center hole of the side-stay splint assembly.
(3)
Tighten the strap and connect the cables to the hook. Tighten the cable.
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 32-11-16Page 434 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 001-003, 051-052,
R Subtask 32-11-16-420-057-B
R B. Preparation for Installation
R (1) Clean the component interface and/or the adjacent area with a
R MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS
R (Material No. 11-026).
R (2) Do an inspection of the component interface and/or the adjacent area.
R (3) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
R (4) Make sure that the hydraulic line end-fittings are serviceable.
R (5) Examine these components for corrosion, damage and wear:
R - the pin (1)
R - the bushes in the side-stay bracket
R - the cardan bracket (3)
R - the bores of the MLG attachment lugs
R - the proximity sensors attachment brackets.
R (6) Get a new bolt (4) for installation.
R NOTE : In the step that follows, make sure that the Materials No.____
R 04-004 and No. 04-022 are not mixed together. Do not use them
R at the same time (Ref. SIL 12-008).
R (7) Lubricate with COMMON GREASE (Material No. 04-004) or COMMON GREASE
R (Material No. 04-022):
R - the pin (1)
R - the bushes in the side-stay bracket
R - the seal (54)
R - the bores of the MLG attachment lugs.
R 1EFF : 001-003, 051-052, 1 32-11-16Page 435 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 32-11-16-420-057-A
B. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Make sure that the hydraulic line end-fittings are serviceable.
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 LANDING GEAR 起落架2(49)
