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时间:2011-10-13 19:40来源:蓝天飞行翻译 作者:航空
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 - cylinder head temperature C.H.T. system (if installed),
- exhaust gas temperature E.G.T. system (if installed).   
77-10 85) Replace the inlet pressure filter - refer to 77-10-02 201. 100  
20-00 86) Reinforce the anticorrosion protection - refer to 100  
 20-00-04 201 and lubricate - refer to 12-21-01 201.   

AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 230
JUN 01
 

ATA "80A" MAJOR INSPECTION
STABILIZER INSPECTION (AREA 300) AREA OTHER
INSPECTION PERFORMED
BY
55-00 STABILIZER INSPECTION (AREA 300) 300  
55-00 1) Perform an overall visual inspection of area 300. 300  
11-00 2) Check installation and legibility of exterior placards and markings - refer to 11-20-00 1. 300  
55-00 3) Check the control surfaces for freedom of rotation - refer to 27-10-00 201, 27-20-00 201 and 27-30-00 201. 300  
55-00 4) Check the play of the elevator hinge ball joints - refer to 55-20-01 201. 300  
55-20 5) Remove the elevator and inspect for loose rivets, cracks and evidence of corrosion - refer to 55-20-01 201. 300  
 Lubricate the inside of the balancing boom - refer to 12-21-03 201.   
 Visually inspect the elevator supports and hinges at frame C9.   
 Install the elevator - refer to 55-20-01 201.   
55-20 6) Visually inspect the elevator hinge bearings. 300 1000 hrs or 
 S / N 1 - 1864, 1867 - 1869  2 years 
 Refer to the latest issue of SB 10-101-55.   
55-20 7) Check the balancing weight and the boom for security and evidence of corrosion. 300  
55-40 8) Remove the rudder. 300  
 Visually inspect the hinges and check for loose rivets, cracks and evidence of corrosion.   
 Install the rudder - refer to 55-40-00 201.   
55-40 9) Check the balancing weight for attachment, and check for evidence of corrosion ; in case of doubt, remove the vertical stabilizer tip - refer to 55-40-00 201. 300  
55-30 10) Visually inspect (do not remove) vertical stabilizer,
structure, attachments at frames C7 and C8, hinge bearings, skins and check for loose rivets, distortion, cracks and evidence of corrosion. 300  
30-10 11) Visually inspect the porous leading edges (if installed) on the stabilizers. 300  
27-20 12) Visually inspect the adjustable end of the rudder trim tab control (on control surface side). 300  
 
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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(45)