ADAA
Validity : S / N 1 - 9999 05 30 03Page 201
(EA) JUN 01
 

TB20 TYPICAL TEST FLIGHT AIRCRAFT S/N : F : 2/8
  Pilot
Date
Time 
 2 - TAXIING
 Autopilot test    
   
 Park brake warning light off    
   
 Rudder stop-to-stop travel    
   
 Nose wheel steering and differential braking    
   
 Pilot and (if installed) R.H. station symmetrical braking    
   
 Controls and trims travel    
  
 Turning radius    
 3 - COMPENSATION
Max error 5°
 Strobe lights ON    
   
 Turn indicator ON    
 N = 2000 RPM
  Heading Taxiway Runway 
  Gyro   
  Compass   
 
 HSI manual alignment    
 

ADAA
Validity : S / N 1 - 9999 05-30 03Page 202
(EA) JUN 01
 

TB20 TYPICAL TEST FLIGHT AIRCRAFT S/N : F : 3/8
  Pilot
Date
Time 
 4 - ENGINE RUN-UP
 Mixture check    
   
 Propeller control check    between 2000 and 1500 RPM
   
 Parking brake check   
   
 Magneto selection    
 N . 2000 RPM A Ni = A N2 , A N < - 175 RPM
A N1_ A N2 < 50 RPM
 Altimeter setting 1013 mb displayed    
 
 Parameters IOAT
°C RPM Manifold
pressure
in.Hg Fuel flow
US G/h CHT
°F EGT
°F Oil
temp. Oil
press. U
volts Vacuum
in.Hg
 Results
Full throttle          
 5 - FLIGHT
Climb to FL = 100 - 95 KIAS
 Parameters ZP
ft Time IOAT
°C RPM Manifold
pressure
in.Hg Fuel
flow
US G/h CHT °
　
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