AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 212
JUN 01
ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
52-10 115) Check the small window(s) (if installed) for operation and check the seal(s) for condition. 200
52-10 116) Partially debond the insulating canvas from the door lower area, thoroughly inspect the locking mechanisms. 200
Lubricate - refer to 12-21-02 201 and rebond the
canvas.
52-10 117) Check the hooks and locks for adjustment and operation 200
- refer to 52-10-00 201.
56-00 118) Visually inspect the windshield and the windows. Check the transparent material and the seals for condition and security. 200
52-30 119) Visually inspect cargo door (baggage compartment) 219 and its seal. 200
53-00 120) 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.
53-00 121) Using a borescope, thoroughly inspect frames CO and C1 200
[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.
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