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57-20 8) Visually inspect the L.H. main-landing-gear attachment area for loose rivets, distortion, cracks and evidence of corrosion. 500  
57-20 9) Visually inspect the L.H. main-landing-gear hinged strut attachment bearing and the retraction actuator
attachment fitting. 500  
57-20 10) 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 
57-60 11) Visually inspect the L.H. aileron attachment and hinge. 500  
57-60 12) Check the L.H. aileron balancing weight attach fittings for condition. 500  
57-60 13) Check the L.H. aileron for freedom of rotation - refer to 27-10-00 201. 500  
57-50 14) Visually inspect the L.H. flap attachment and hinge. 500  
20-00 15) Reinforce the anticorrosion protection - refer to 500  
 20-00-04 201 and lubricate - refer to 12-21-04 201.   

AIAA
Validity : S / N 1 - 9999 05-20-04 (JA) Page 210
JUN 01
 

ATA "4A" INSPECTION - 100 HOURS
R.H. WING INSPECTION (AREA 600) AREA OTHER INSPECTION
PERFORMED
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  
27-50 3) Remove and clean R.H. flap control bellcrancks. Perform a detail examination. Lubricate. Install. 600 1000 hrs 
30-10 4) Visually inspect the porous leading edges (if installed) on the R.H. wing. 600  
57-20 5) Visually inspect the R.H. main-landing-gear attachment area for loose rivets, distortion, cracks and evidence of corrosion. 600  
57-20 6) Visually inspect the R.H. main-landing-gear hinged strut attachment bearing and the retraction actuator
attachment fitting. 600  
57-20 7) 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 
57-60 8) Visually inspect the R.H. aileron attachment and hinge. 600  
57-60 9) Check the R.H. aileron balancing weight attach fittings for condition. 600  
57-60 10) Check the R.H. aileron for freedom of rotation - refer to 27-10-00 201. 600  
　
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