ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
32-30 84) Visually inspect the landing gear hydraulic system tubes for evidence of leaks and wear ; check the routing ; check the attach fittings and the unions for condition and interference. 200 500 hrs
32-40 85) Visually inspect the master cylinders. 200
Check the brake system for condition, attachment, union security and tightness.
32-40 86) Visually inspect the brake pedals and system, check attach fittings and clearances. 200
32-40 87) Visually inspect the parking brake system (including the cock and the indicating circuit), check attach fittings and look for leaks. 200
34-10 88) Visually inspect the air data systems (connectors, hoses, unions, attach fittings) and check for routing. 200
34-10 89) In case of frequent flights in highly humid atmosphere, drain the normal static pressure system and (if installed in rear fuselage) the emergency system - refer to 34-11-00 201. 200
34-10 90) Drain the normal static pressure system and (if installed in rear fuselage) the emergency system - refer to 200
34-11-00 201.
34-10 91) Perform a tightness test on air data systems and check the associated instruments - refer to 34-11-00 201. 200 300 hrs or
3 years
34-10 92) Visually inspect the pitot tube and the dynamic pressure system in the L.H. wing. Check the hoses and their attach fittings for condition. 500
34-10 93) Visually inspect the pitot tube (if installed) and the
dynamic pressure system in the R.H. wing. Check hoses and attach fittings for condition. 600
34-20 94) Visually inspect the slaved directional gyro (if installed). 200
Check the attach fittings, the dampers, the wiring and the
support ; look for cracks and evidence of corrosion.
AIM
Validity : S / N 1 - 9999 05 20 05 (JA) Page 210
JUN 01
ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
34-00 95) Check VFR equipment (if installed). 200
NOTE : Must be performed by an approved radio center in compliance with the regulation in force in the country of use.
(Examples :
- FAR Part 91.411 and 91.413 : 24 months, - GSAC Instruction bulletin P-41-15, Ed. 1 dated September 2000 :
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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(27)
