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57-20 29) Visually inspect the attach fittings and check the L.H. wing front attachment for cracks and evidence of corrosion. 500
57-20 30) Visually inspect the attach fittings and check the L.H. wing rear attachment for cracks and evidence of corrosion. 500
57-20 31) Visually inspect the attach fittings and check the L.H. wing main attachment spacers for cracks and evidence of corrosion. 500
57-20 32) Visually inspect the L.H. wing ribs and inner skin for loose rivets, cracks, distortion and evidence of corrosion. 500
57-20 33) Inspect the L.H. wing upper and lower surface skins for condition, inspect the anti-skid coating and anti-wear 500
PTFE located at flap/wing junction for condition.
57-30 34) Visually inspect the L.H. wing tip attach fittings. 500
57-30 35) Visually inspect the visible portions of the L.H. wing tip for loose rivets, cracks and distortion. 500
57-60 36) Check the L.H. aileron balancing weight attach fittings for condition. 500
57-60 37) Visually inspect the L.H. aileron hinge fittings, check the ball joints, the attach fittings and the stops. 500
57-60 38) Visually inspect the visible portions of the L.H. aileron ; in case of doubt, remove the aileron and inspect for loose rivets, cracks, distortion and evidence of corrosion - refer to 57-60-00 201. 500
57-60 39) Check the L.H. aileron for freedom of rotation - refer to 27-10-00 201. 500
57-50 40) Visually inspect the visible portions of the L.H. flap ; in case of doubt, remove the flap and inspect for loose rivets, cracks, distortion and evidence of corrosion - refer to 57-50-00 201. 500
57-50 41) Visually inspect the L.H. flap hinge fittings, check the ball joints and the attach fittings. 500
AIAA
Validity : S / N 1 - 9999 05-20-05 Page 220
JUN 011
ATA "80A" MAJOR INSPECTION
L.H. WING INSPECTION (AREA 500) AREA OTHER
INSPECTION PERFORMED
BY
20-00 42) Reinforce the anticorrosion protection - refer to 500
20-00-04 201 and lubricate - refer to 12-21-04 201.
52-40 43) Install sealed inspection doors 513, 514 - refer
to 52-40-00 201. 500
57-30 44) Install wing tip 517 (if not riveted) - refer to 57-30-00 201. 500
AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 221
JUN 01
ATA "80A" MAJOR INSPECTION
R.H. WING INSPECTION (AREA 600) AREA OTHER INSPECTION
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飞机维护手册 05 时间限制维护检查 2(36)
