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57-20 3) 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 4) Visually inspect the L.H. spar for loose
rivets, cracks, distortion and evidence of corrosion. 500    X  
57-20 5) Visually inspect the attach fittings and check the L.H. wing front attachment for cracks and evidence of corrosion. 500    X  
57-20 6) Visually inspect the attach fittings and check the L.H. wing rear attachment for cracks and evidence of corrosion. 500    X  
57-20 7) Visually inspect the attach fittings and check the L.H. wing main attachment spacers for cracks and evidence of corrosion. 500    X  
57-20 8) Visually inspect the L.H. wing ribs and inner skin for loose rivets, cracks, distortion and evidence of corrosion. 500    X  
57-20 9) Inspect the L.H. wing upper and lower surface skins for condition, inspect the
anti-skid coating and anti-wear PTFE
located at flap/wing junction for condition. 500    X X 
57-20 10) Visually inspect the R.H.
 main-landing-gear attachment area for loose rivets, distortion, cracks and evidence of corrosion. 600   X X 0 NOTE 1
57-20 11) Visually inspect the R.H. main-landing-gear hinged strut attachment bearing and the retraction actuator attachment fitting. 600   X X 0 NOTE 1

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform the operations identified with a "0" unless the annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
AHAA
Validity : S / N 1 - 9999 05-20-01P 235
(IA) JUN 01
 

ATA OPERATIONS Area INSPECTIONS
   1st
25 hrs 50
hrs 100
hrs Major Ann. Other
57-20 12) 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
　
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