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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
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本文鏈接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飛機維護手冊 05 時間限制維護檢查 2(62)
