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52-10 79) Thoroughly examine and fluorescent dye penetrant inspect the steel latches for cracks, check for distortion and interference. 200 2000 hrs 
56-00 80) Visually inspect the windshield and the windows. Check the transparent material and the seals for condition and security. 200  
52-30 81) Visually inspect cargo door (baggage compartment) 219 and its seal. 200  

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05-20-06Page 210
(EA) JUN 01
 

ATA ANNUAL INSPECTION (AI)
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
53-00 82) Thoroughly inspect the firewall (front and rear faces), forward table and central pedestal sides, for loose rivets, distortion, cracks and evidence of corrosion. 000  
 Inspect equipment for security.   
53-00 83) 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 84) 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 NOTE 1 
53-00 85) Visually inspect the floor stiffeners and the cabin floor for loose rivets, distortion, cracks and evidence of corrosion. 200  
53-00 86) Visually inspect (do not remove) the visible portions of the fuselage structure for loose rivets, distortion and
evidence of corrosion. 200  
76-00 87) Check travel and visually inspect attach fittings and routing of controls : 000 NOTE 1 
 - propeller governor,
- alternate air,
- mixture,
- throttle.   
76-00 NOTE : Make sure that the powerplant stops are reached before the control unit stops. 000 NOTE 1 
76-00 88) Ensure that there is no slack, and that the control friction knob on the pedestal is effective. 200  
20-00 89) Reinforce the anticorrosion protection - refer to 200  
 20-00-04 201 and lubricate - refer to 12-21-02 201.   

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
　
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