ATA "80A" MAJOR INSPECTION
LANDING GEAR INSPECTION (AREA 700) AREA OTHER
INSPECTION PERFORMED
BY
32-20 15) Visually inspect the nose landing gear leg, the sliding body and the fork for cracks and distortion ; thoroughly inspect the half-scissors and hinged strut attachment bosses. 700  
 Remove, inspect and reinstall the half-scissors - refer to 32-20-03 201.   
32-20 16) Visually inspect the nose landing gear axles, bushings and hinge bearings ; check for evidence of wear and excessive play. 700  
32-20 17) Check the nose landing gear shock absorber for inflation and leaks - refer to 12-14-02 301. 700  
32-20 18) Visually inspect the nose landing gear door, check the attach fittings and look for cracks and distortion. 700  
32-20 19) Thoroughly examine the whole nose landing gear mount. 700  
 Fluorescent dye penetrant inspect the attach fittings and mount for cracks and distortion ; check for protection and absence of interference - refer to 32-20-01 201.   
32-20 20) Check that the nose landing gear mount is correctly attached to the firewall. Check the red painted marks on the bolts for alignment. 700  
32-20 21) Visually inspect the nose landing gear wheel-centering device. 700  
32-20 22) Visually inspect the nose landing gear interconnection system and check the levers for condition. 700  
32-30 23) Replace the landing gear actuating cylinders. 700 30000
cycles 
32-30 24) Visually inspect the 3 actuating cylinders and the attach fittings ; check for leaks and check the moving parts for evidence of wear or shock marks. 700  
32-30 Landing gear struts without grease nipples 700 500 hrs or 
 25) Remove the front part of the nose landing gear strut and remove the main landing gear struts. Thoroughly inspect the struts for excessive play, cracks, distortion and
evidence of corrosion.  1 year 
 Lubricate the inner flanks of the yokes, the axles and the ball joints - refer to the latest issue of SOCATA SB 45.   
 Install the struts - refer to 32-30-04 201, 32-30-03 201.   
32-30 All 700  
 26) Visually inspect the nose landing gear and main landing gear struts for excessive play, cracks, distortion and evidence of corrosion.   

AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 216
JUN 011
 

ATA "80A" MAJOR INSPECTION
LANDING GEAR INSPECTION (AREA 700) AREA OTHER
INSPECTION PERFORMED
BY
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飛機維護手冊 05 時間限制維護檢查 2(32)