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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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34-00 53) Visually inspect the antennas (if installed). 200  
34-00 54) Visually inspect the cables of the antennas (if installed), check attach fittings and check for routing and
interference. 200  

AIM
Validity : S / N 1 - 9999 05-20-05 (JA) Page 207
JUN 01
 

ATA "80A" MAJOR INSPECTION
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
27-00 55) Visually inspect the control wheels for security on torque tubes. 200  
27-00 56) Visually inspect roll stops and ball joints for condition and play. 200  
27-00 57) Visually inspect the roll control, behind the instrument panel, for R.H. and L.H. gimbal joint play, the pylon and check that the control wheel can move forth and back without resistance. 200  
27-00 S / N 275 - 9999 200  
 58) Visually inspect the elevator trim tab control linkage   
 (cables, pulleys) for play - refer to 27-30-03 601,
20-00-07 201.   
27-00 S / N 1 - 9999 200  
 59) Visually inspect the flight controls control linkage (along the 3 axes) for play, check cabin sealing bellows for condition :   
 - roll - refer to 27-10-00 201,
- rudder and elevator - refer to 27-20-00 201,
27-30-00 201.   
 NOTE : Make sure that flight control stops are reached before rudder and elevator control stops.   
27-00 60) Visually inspect the rudder trim tab control linkage (ball control) for play - refer to 27-20-04 201. 200  
27-20 61) Visually inspect the rudder and trim tab input rods in the rear fuselage. 200  
27-20 62) Visually inspect the adjustable end of the rudder control 200  
 (on control surface side).   
27-20 63) Visually inspect the nose landing gear/rudder
interconnection rods on rudder pedals, check cabin sealing bellows, bellcranks and attaching hardware for condition - refer to 27-20-01 201. 200  
27-30 64) Visually inspect the elevator and trim tab control input rods in the rear fuselage. 200  
27-30 65) Visually inspect the support of the electrical pitch trim control servo-actuator and its attach fittings (if installed). 200  
27-50 66) Visually inspect the flap controls and the indicator - refer to 27-50-01 201. 200  
28-20 S / N 731 - 9999 200  
 67) Visually inspect the electric pump, the support, the unions, the vent hose and the connections.   
 
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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(25)