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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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 35-00-00 201.   
37-00 106) Check the vacuum system paper filter (if installed) for cleanliness and condition, replace if necessary. 200 500 hrs or
1 year 
37-00 107) Check the foam filter of the vacuum system regulating valve (if installed) for cleanliness and condition, replace if necessary. 200  
37-00 108) Check the normal vacuum system (if installed) - refer to 37-11-00 201. 000  
37-00 109) Check the emergency vacuum system (if installed) - refer to 37-12-00 201. 000  
37-00 110) Replace the emergency vacuum pump (if installed). 200 10 years or 
   500 pump
hours 
37-00 111) Replace the elapsed time indicator (if installed). 200 Replace
ment
associated
with
emergency
vacuum
pump 
52-10 112) Visually inspect the cabin access doors, check the structure, the transparent material condition and check for distortion and cracks. 200  
52-10 113) Check the gas struts, hinges, seals, locks, rings and latches for condition. 200  
52-10 114) Thoroughly examine and fluorescent dye penetrant inspect the steel latches for cracks, check for distortion and interference. 200 2000 hrs 

AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 212
JUN 01
 

ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
52-10 115) Check the small window(s) (if installed) for operation and check the seal(s) for condition. 200  
52-10 116) Partially debond the insulating canvas from the door lower area, thoroughly inspect the locking mechanisms. 200  
 Lubricate - refer to 12-21-02 201 and rebond the
canvas.   
52-10 117) Check the hooks and locks for adjustment and operation 200  
 - refer to 52-10-00 201.   
56-00 118) Visually inspect the windshield and the windows. Check the transparent material and the seals for condition and security. 200  
52-30 119) Visually inspect cargo door (baggage compartment) 219 and its seal. 200  
53-00 120) Thoroughly inspect the firewall (front and rear faces), forward table and central pedestal sides, for loose rivets, distortion, cracks and evidence of corrosion. 000  
 Inspect equipment for security.   
53-00 121) Using a borescope, thoroughly inspect frames CO and C1 200  
 [get access through frame C1 and, from S / N 731,
through fuel service door 213 (and, 214 if installed)] for
loose rivets, distortion, cracks and evidence of corrosion.   
 
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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(29)