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57-50 4) Visually inspect the R.H. flap attachment and hinge. 600   X  0 NOTE 1
57-50 5) Visually inspect the visible portions of the 600    X X 
 R.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.       
57-50 6) Visually inspect the R.H. flap hinge fittings, check the ball joints and the attach fittings. 600    X  
57-60 Ailerons       
57-60 1) Visually inspect the L.H. aileron attachment and hinge. 500   X  0 NOTE 1
57-60 2) Check the L.H. aileron balancing weight attach fittings for condition. 500   X X 0 NOTE 1
57-60 3) Visually inspect the L.H. aileron hinge
fittings, check the ball joints, the attach
fittings and the stops. 500    X  
57-60 4) Visually inspect the visible portions of the 500    X X 
 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.       
57-60 5) Check the L.H. aileron for freedom of
rotation - refer to 27-10-00 201. 500   X X 0 NOTE 1
57-60 6) Visually inspect the R.H. aileron attachment and hinge. 600   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 20-01Page 237
(IN JUN 01
 

ATA OPERATIONS Area INSPECTIONS
   1st
25 hrs 50
hrs 100
hrs Major Ann. Other
57-60 7) Check the R.H. aileron balancing weight attach fittings for condition. 600   X X 0 NOTE 1
57-60 8) Visually inspect the R.H. aileron hinge
fittings, check the ball joints, the attach
fittings and the stops. 600    X  
57-60 9) Visually inspect the visible portions of the 600    X X 
 R.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.       
57-60 10) Check the R.H. aileron for freedom of
　
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