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(7) Install the locking plates (13) and (38) and the nuts (14) and (40). (8) TORQUE the nuts (19) and (42) to between 4.2 and 4.8 m.daN (30.97 and 35.39 lbf.ft). (9) Safety the nuts (19) and (42) with the new cotter pins (5). (10) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003). (11) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully extend the slats. (12) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003). (13) Apply special materials: _______ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (a) Apply SEALANTS (Material No. 09-001) to: - the nuts (4), (6), (18), (19), (20), (31), (32) and (42) - the bolt heads (11), (12), (15), (16), (17), (37), (39) and (41) - the locking plates (13) and (38). (14) Remove the BLOCK-SLAT GAPPING from the No. 9 slat track. (15) Do a check of the slat lower trailing-edge, dimension L: (a) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003). (b) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats.
R
EFF : CES
051-051,
27-84-63
Page 429 May 01/05
飞行翻译公司 www.aviation.cn 本文链接地址：A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 18_部分15.pdf
(7) Install the locking plates (13) and (38) and the nuts (14) and (40). (8) TORQUE the nuts (19) and (42) to between 4.2 and 4.8 m.daN (30.97 and 35.39 lbf.ft). (9) Safety the nuts (19) and (42) with the new cotter pins (5). (10) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003). (11) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully extend the slats. (12) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003). (13) Apply special materials: _______ WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. (a) Apply SEALANTS (Material No. 09-001) to: - the nuts (4), (6), (18), (19), (20), (31), (32) and (42) - the bolt heads (11), (12), (15), (16), (17), (37), (39) and (41) - the locking plates (13) and (38). (14) Remove the BLOCK-SLAT GAPPING from the No. 9 slat track. (15) Do a check of the slat lower trailing-edge, dimension L: (a) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003). (b) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats.
R
EFF : CES
051-051,
27-84-63
Page 429 May 01/05
飞行翻译公司 www.aviation.cn 本文链接地址：A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 18_部分15.pdf
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