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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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 P-41-15, Ed. 1 dated       
 September 2000 :       
 . operational test plus flight check every 18 months maximum,
. check on test bench every       
 3 years for equipment with       
 French type approval prior
to January 1, 1980 - refer to       
 GSAC Instruction bulletin       
 P-04-30.).       

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 226
(IA) JUN 01
 

ATA OPERATIONS Area INSPECTIONS
   1st
25 hrs 50
hrs 100
hrs Major Ann. Other
34-10 Flight environment data       
34-10 1) Visually inspect the air data systems 200    X  
 (connectors, hoses, unions, attach fittings) and check for routing.       
34-10 2) In case of frequent flights in highly humid atmosphere, drain the normal static
pressure system and (if installed in rear fuselage) the emergency system - refer to 34-11-00 201. 200   X X  
34-10 3) Drain the normal static pressure system and 200    X X 
 (if installed in rear fuselage) the emergency system - refer to 34-11-00 201.       
34-10 4) Perform a tightness test on air data systems and check the associated instruments - refer to 34-11-00 201. 200    X  300 hrs or
3 years
34-10 5) Visually inspect the pitot tube and the
dynamic pressure system in the L.H. wing. 500    X X 
 Check the hoses and their attach fittings for condition.       
34-10 6) Visually inspect the pitot tube (if installed) and the dynamic pressure system in the 600    X X 
 R.N. wing. Check hoses and attach fittings for condition.       
34-20 Attitude and direction       
34-20 1) Visually inspect the slaved directional gyro 200    X  
 (if installed). Check the attach fittings, the dampers, the wiring and the support ; look for cracks and evidence of corrosion.       
 
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