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 230
(IA) JUN 011
ATA OPERATIONS Area INSPECTIONS
1st
25 hrs 50
hrs 100
hrs Major Ann. Other
53-00 2) Thoroughly inspect the firewall (front and rear faces), forward table and central
pedestal sides, for loose rivets, distortion, cracks and evidence of corrosion. 000 X X
Inspect equipment for security.
53-00 3) Using a borescope, thoroughly inspect
frames CO and C1 [get access through frame C1 and, from S / N 731, through fuel service door 213 (and, 214 if installed)] for loose rivets, distortion, cracks and evidence of corrosion. 200 X
53-00 4) Visually inspect (do not remove) the wing duct in the fuselage on cabin side and on wing spar side for loose rivets, distortion, cracks and evidence of corrosion. 200 X
53-00 5) Visually inspect frames C2, C3, C4, C5, C6, C7 and C8 for loose rivets, distortion, cracks and evidence of corrosion. 200 X
53-00 6) Visually inspect the flight control supports at frame CO (rear), between frames C3 and 200 X 500 hrs
C4, at frames C7 (front) and C9 (front).
Inspect for loose rivets, distortion, cracks and evidence of corrosion.
53-00 7) Visually inspect frame C9, from the outside and directly for the accessible portion, and using a mirror for the inner portion. Inspect for loose rivets, distortion, cracks and
evidence of corrosion. 200 X X 0 NOTE 1
53-00 8) Visually inspect the inter-frame stringers for loose rivets, distortion, cracks and evidence of corrosion. 200 X
53-00 9) Visually inspect the floor stiffeners and the cabin floor for loose rivets, distortion, cracks and evidence of corrosion. 200 X X
53-00 10) Visually inspect the inside of the fuselage skin for loose rivets, distortion, cracks and evidence of corrosion. 200 X
53-00 11) Visually inspect (do not remove) the visible portions of the fuselage structure for loose rivets, distortion and evidence of corrosion. 200 X X
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