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时间:2011-10-13 19:36来源:蓝天飞行翻译 作者:航空
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hrs Major Ann. Other
55-20 Elevator       
55-20 1) Remove the elevator and inspect for loose rivets, cracks and evidence of corrosion -refer to 55-20-01 201. 300    X  
 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 2) Visually inspect the elevator hinge bearings. S / N 1 - 1864, 1867 - 1869 300      1000 hrs
or 2 years
 Refer to the latest issue of SB 10-101-55.       
55-20 3) Check the balancing weight and the boom for security and evidence of corrosion. 300   X X 0 NOTE 1
55-30 Vertical stabilizer       
55-30 1) Visually inspect (do not remove) vertical stabilizer, structure, attachments at frames 300    X  
 C7 and C8, hinge bearings, skins and check for loose rivets, distortion, cracks and evidence of corrosion.       
55-40 Rudder       
55-40 1) Visually inspect the rudder hinges and
check for loose rivets, cracks and evidence of corrosion. 300     X 
55-40 2) Remove the rudder. 300    X  
 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 3) 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   X X 0 NOTE 1

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform the operations identified with a "0" unless the annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
AHAA
Validity : S / N 1 - 9999 05 20-01Page 233
(IN JUN 01
 

ATA OPERATIONS  INSPECTIONS
  Area 1st
25 hrs 50
hrs 100
hrs Major Ann. Other
56-00 WINDOWS       
56-00 General       
56-00 1) Visually inspect the windshield and the
windows. Check the transparent material
 
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