AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 214
JUN 01
ATA "80A" MAJOR INSPECTION
LANDING GEAR INSPECTION (AREA 700) AREA OTHER
INSPECTION PERFORMED
BY
32-00 LANDING GEAR INSPECTION (AREA 700) 700
32-00 1) Perform an overall visual inspection of area 700. 700
11-00 2) Check installation and legibility of exterior placards and markings - refer to 11-20-00 1. 700
24-00 3) Visually inspect all cable connections on the nose and main landing gears. 700
Replace cables if damaged. Inspect cables for routing, clamp security, lugs and cleanliness.
32-40 4) Remove and check main landing gear wheel caps 737 and 747 for condition - refer to 32-41-01 201. 700
32-40 5) Deflate the tires and remove the wheels - refer
to 12-14-01 301, 32-41-01 201, 32-41-02 201. 700
32-40 6) Thoroughly fluorescent dye penetrant inspect the wheels and the wheel axles for cracks, distortion and evidence of wear and corrosion. 700
32-40 7) Thoroughly inspect the wheel bearings. 700
32-40 8) Visually inspect the tires ; look for evidence of uneven wear, cuts, distortion and displacement of the tire on the wheel. 700
32-40 9) Inspect the brake hydraulic system unions for security and tigthness. 700
32-40 10) Remove and thoroughly inspect the braking system for condition, attachment, brake plate and disk wear ; look for cracks on the brake unit and thrust plate. 700
Install the braking system - refer to 32-42-02 201.
32-10 11) Visually inspect the main landing gear bodies and rocker beams for cracks and distortion ; thoroughly inspect the shock absorber and hinged strut attachment bosses. 700
32-10 12) Visually inspect the main landing gear doors, the hinges and the control rod, inspect for security, excessive play, cracks and distortion. 700
32-10 13) Visually inspect the main landing gear axles and hinge bearings for cracks, distortion, evidence of wear and corrosion. Check for excessive play ; a friction mark on the stop stiffener shows that the play in the bearing ball joint is excessive. 700
32-10 14) Check the main landing gear shock absorbers for inflation and leaks - refer to 12-14-02 301. 700
AIM
Validity : S / N 1 - 9999 05 20-05 (JA) Page 215
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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(31)
