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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
　
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