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53-00 122) 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  
53-00 123) Visually inspect frames C2, C3, C4, C5, C6, C7 and C8 for loose rivets, distortion, cracks and evidence of corrosion. 200  
53-00 124) Visually inspect the flight control supports at frame CO 200 500 hrs 
 (rear), between frames C3 and C4, at frames C7 (front) and C9 (front). Inspect for loose rivets, distortion, cracks and evidence of corrosion.   
53-00 125) 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  
53-00 126) Visually inspect the inter-frame stringers for loose rivets, distortion, cracks and evidence of corrosion. 200  
53-00 127) Visually inspect the floor stiffeners and the cabin floor for loose rivets, distortion, cracks and evidence of corrosion. 200  
53-00 128) Visually inspect the inside of the fuselage skin for loose rivets, distortion, cracks and evidence of corrosion. 200  

AIM
Validity : S / N 1 - 9999 05-20-05 (JA) Page 213
JUN 01
 

ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
53-00 129) Visually inspect (do not remove) the visible portions of the fuselage structure for loose rivets, distortion and
evidence of corrosion. 200  
53-00 130) Visually inspect the anti-twist edges for loose rivets, distortion, cracks and evidence of corrosion. 200  
53-00 131) Visually inspect the footsteps for distortion and cracks especially near the attachment points, check the
anti-skid material for condition. 200  
53-00 132) Visually inspect the air regulation NACA inlets and the access door bottom area for sealing and drainage. 200  
53-00 Post-MOD. 151 200  
 133) Remove vertical stabilizer root front fairing 225, visually inspect for cracks and security.   
76-00 All 000  
 134) Check travel and visually inspect attach fittings and routing of controls :   
 - propeller governor,
- alternate air,
- mixture,
- throttle.   
76-00 NOTE : Make sure that the powerplant stops are reached before the control unit stops. 000  
76-00 135) Ensure that there is no slack, and that the control friction knob on the pedestal is effective. 200  
　
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