曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
57-20 17) Visually inspect the L.H. main-landing-gear hinged strut attachment bearing and the retraction actuator
attachment fitting. 500 NOTE 1
57-20 18) Thoroughly inspect the L.H. main-landing-gear hinged strut attachment bearing - refer to the latest issue of SOCATA SB 10-080-57. 500 6000 Idg. or
4000 hrs,
then
1500 Idg. or
1000 hrs
57-20 19) 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 20) Visually inspect the L.H. wing tip attach fittings. 500
57-30 21) Visually inspect the visible portions of the L.H. wing tip for loose rivets, cracks and distortion. 500
57-60 22) Visually inspect the L.H. aileron attachment and hinge. 500 NOTE 1
57-60 23) Check the L.H. aileron balancing weight attach fittings for condition. 500 NOTE 1
57-60 24) 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 25) Check the L.H. aileron for freedom of rotation - refer to 27-10-00 201. 500 NOTE 1
57-50 26) Visually inspect the L.H. flap attachment and hinge. 500 NOTE 1
NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05-20-06Page 216
(EA) JUN 01
ATA ANNUAL INSPECTION (Al)
L.H. WING INSPECTION (AREA 500) AREA OTHER INSPECTION
PERFORMED
BY
57-50
20-00 27) 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.
28) Reinforce the anticorrosion protection - refer to
20-00-04 201 and lubricate - refer to 12-21-04 201. 500
500
NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05 20-06Page 217
(EA) JUN 01
ATA ANNUAL INSPECTION (AI)
R.H. WING INSPECTION (AREA 600) AREA OTHER
INSPECTION PERFORMED
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(62)
