曝光台 注意防骗
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BY
57-00 R.H. WING INSPECTION (AREA 600) 600
57-00 1) Perform an overall visual inspection of area 600. 600
11-00 2) Check installation and legibility of exterior placards and markings - refer to 11-20-00 1. 600 NOTE 1
24-00 3) Visually inspect all cable connections in the R.H. wing. 600
Replace cables if damaged. Inspect cables for routing, clamp security, lugs and cleanliness.
27-10 4) Visually inspect the visible portions of R.H. aileron rods. 600
27-50 5) Visually inspect (do not remove) the R.H. flap control rods. 600
27-50 6) Remove and clean R.H. flap control bellcrancks. Perform a detail examination. Lubricate. Install. 600 1000 hrs
28-10 7) Perform an operational test of the R.H. fuel tank cap and check the seal condition - refer to 28-10-00 301. 600
28-10 8) Visually inspect the R.H. fuel tank venting system for condition, security and obstruction. 600
30-10 9) Visually inspect the porous leading edges (if installed) on the R.H. wing. 600 NOTE 1
57-10 10) Check the pins of the R.H. wing-to-fuselage front, main and rear attachments ; make sure the nuts have not rotated, in case of doubt, torque the nuts - refer
to 20-00-01 201. 600
57-20 11) Visually inspect the R.H. main-landing-gear attachment area for loose rivets, distortion, cracks and evidence of corrosion. 600 NOTE 1
57-20 12) Visually inspect the R.H. main-landing-gear hinged strut attachment bearing and the retraction actuator
attachment fitting. 600 NOTE 1
57-20 13) Thoroughly inspect the R.H. main-landing-gear hinged strut attachment bearing - refer to the latest issue of SOCATA SB 10-080-57. 600 6000 Idg. or
4000 hrs,
then
1500 Idg. or
1000 hrs
57-20 14) Inspect the R.H. wing upper and lower surface skins for condition, inspect the anti-skid coating and anti-wear 600
PTFE located at flap/wing junction for condition.
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 Page 218
06 (EA) JUN 01
ATA ANNUAL INSPECTION (Al)
R.H. WING INSPECTION (AREA 600) AREA OTHER
INSPECTION PERFORMED
BY
57-30 15) Visually inspect the R.H. wing tip attach fittings. 600
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