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?(c) ?Turn the eye end IN or OUT until the "Dimension X" is reached.
?(d) ?Tighten the eye end-lock nut and Torque to 14.6 m.daN (107.66 lbf.ft).
?(e) Safety the eye end with MISCELLANEOUS (Material No. 19-010). Subtask 32-31-44-560-051 ?E. Preparation for Installation ?(1) ?Clean the component interface and/or the adjacent area.
?(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. Procedure _________ ?(Ref. Fig. 401/TASK 32-31-44-991-001) Subtask 32-31-44-420-050 ?A. Installation of the MLG Uplock Assembly 2509GM (2510GM) ?(1) Install the MLG Uplock Assembly (8) view B WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE _______ ?SPECIAL MATERIAL. ?THIS MATERIAL IS DANGEROUS.
?(a) ?Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (11), the bushes (1) and the washer (12).
?(b) ?If removed install the inner bush (1).
?(c) ?Put the uplock assembly (8) in position on the aircraft structure.
?(d) ?Install the outer bush (1), the washer (12), the bolt (11) and the nut (2).
?(e) ?TORQUE the nut (2) to between 6.8 and 7.8 m.daN (50.14 and 57.52 lbf.ft) .
?(f) ?Safety the nut (2) with a new cotter pin (3).
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?(2) Install the Strut A (4) view E WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE _______ ?SPECIAL MATERIAL. ?THIS MATERIAL IS DANGEROUS.
?(a) ?Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (20) and the washer assembly (19), the washers (18) and (17).
?(b) ?Put the washer assembly (19) and the strut (4) in position.
?(c) ?Install the bolt (20), the washer (18), (17) and the nut (16).
?(d) ?Safety the nut (16) with a new cotter pin (15).
?(e) ?Put the bonding strap (13) in position and install the bolt (14), the washer (22) and the nut (21) (Ref. TASK 20-28-00-912-004).
?(3) Install the Strut B (10) view F WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE _______ ?SPECIAL MATERIAL. ?THIS MATERIAL IS DANGEROUS.
?(a) ?Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (23) and the washers (25), (26) and the washer assembly (24).
?(b) ?Put the washer assebmly (24) and the strut (10) in position and install the bolt (23), the washers (25), (26) and the nut (27).
?(c) ?Safety the nut (27) with a new cotter pin (28).
?(4) Install the Hydraulic hoses view B ?(a) ?Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
?(b) ?Remove the blanking plugs and connect the hydraulic hoses (7) and
?(9) to the uplock assembly (8) TORQUE the connections to between ?1.52 and 1.63 m.daN (11.20 and 12.02 lbf.ft).
?(c) ?Mark the connections with PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No. 07-010).
?(d) ?Remove the blanking caps from the electrical connectors.
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?(e) ?Make sure that the electrical connectors are clean and in the correct condition.
?(f) ?Connect the electrical connectors (5) and (6) to the uplock assembly (8).
?(5) Install the Free Fall Exstension Rod (35) view D WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE _______ SPECIAL MATERIAL. THIS MATERIAL IS DANGEROUS. ?(Ref. Fig. 401/TASK 32-31-44-991-001) ?(a) ?Install the RIGGING PIN (98DNSA20208060) at rigging points 1 and
?(b) ?If necessary, adjust the adjustable rod (35)
?(c) ?Apply SPECIAL MATERIALS (Material No. 05-002) to the bolt (33), the bush (34) and the washer (37).
?(d) ?Put the rod (35) in position and install the bush (34), the bolt (33), the washer (37) and the nut (36).
?(e) ?Safety the nut (36) with a new cotter pin (38).
?1_ Remove and discard the lockwire and loosen the nuts (41). ?2_ Release the lockwashers (40) and adjust length of the rod ?(35). ?3_ Make sure that all the installed rigging pins can be moved www.aero.cn 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架5
