AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 204
JUN 01
ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
25-10 15) Visually inspect the rear bench for overall condition, the anchoring and locking systems. 200
Tilt the backrest to perform an operational test, check attaching hardware - refer to 25-12-00 201.
25-10 16) Remove the front seats and the rear bench - refer to 25-11-00 201, 25-12-00 201. 200
25-10 17) Remove floor carpets and mats. 200
25-10 18) Visually inspect cabin furnishings (upholstery panels, ashtrays) for overall condition, wear and security. 200
25-10 19) Remove the upholstery panels and the sound-proofing panels. 200
52-40 20) Remove and check condition of access door 238L to landing gear hydraulic generator. 200
25-10 21) Thoroughly inspect the supports and the struts of front seats and locking points of rear bench for cracks and corrosion. 200
25-10 22) Thoroughly inspect the harnesses and safety belts, the reels and the anchor points. Inspect for cracks and corrosion. 200
Perform an operational test, check locking - refer
to 25-13-00 201.
25-50 23) Visually inspect baggage attaching straps in
compartment, inspect anchor points for cracks and
corrosion. 200
25-60 24) Visually inspect emergency locator transmitter (if
installed), check validity date of the battery(ies), attaching hardware, antenna, connector, and surface condition -refer to 05-10-00 1 and 25-61-00 601. 200 100 hrs or
6 months
25-60 25) Inspect external antenna of emergency locator
transmitter (if installed) and remote control system for condition and security. 200
25-60 26) Perform an operational test of the emergency locator transmitter (if installed) ; perform a test with the remote control system on instrument panel and a test with the control built into the emergency locator transmitter - refer to 25-61-01 201. 000 100 hrs or
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本文链接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飞机维护手册 05 时间限制维护检查 2(22)
