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BY
30-10 15) Visually inspect the porous leading edges (if installed) on the R.H. wing. 600  
33-40 16) Visually inspect the navigation lights on the R. H. wing and 600  
 (if installed) the anti-collision and identification lights.   
 Check the domes, glasses, supports and attach fittings for condition.   
34-20 17) Check the flux valve (if installed) and the support for general condition, corrosion, attachment and wiring. 600  
57-10 18) 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 19) Visually inspect the R.H. main-landing-gear attachment area for loose rivets, distortion, cracks and evidence of corrosion. 600  
57-20 20) Visually inspect the R.H. main-landing-gear hinged strut attachment bearing and the retraction actuator
attachment fitting. 600  
57-20 21) 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 22) Visually inspect the R.H. spar for loose rivets, cracks, distortion and evidence of corrosion. 600  
57-20 23) Visually inspect the attach fittings and check the R.H. wing front attachment for cracks and evidence of
corrosion. 600  
57-20 24) Visually inspect the attach fittings and check the R.H. wing rear attachment for cracks and evidence of
corrosion. 600  
57-20 25) Visually inspect the attach fittings and check the R.H. wing main attachment spacers for cracks and evidence of corrosion. 600  
57-20 26) Visually inspect the R.N. wing ribs and inner skin for loose rivets, cracks, distortion and evidence of corrosion. 600  
57-20 27) 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.   
57-30 28) Visually inspect the R.H. wing tip attach fittings. 600  

AIM
Validity : S / N 1 - 9999 05 20 05 (JA) Page 223
JUN 01
 

ATA "80A" MAJOR INSPECTION
R.H. WING INSPECTION (AREA 600) AREA OTHER INSPECTION
PERFORMED
BY
57-30 29) Visually inspect the visible portions of the R.H. wing tip for loose rivets, cracks and distortion. 600  
　
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