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F EGT
F Oil
temp. Oil
press. U
volts Vacuum
in.Hg
 Take off            
 Climb
95 KIAS
Full rich 2500           
  5000           
  7500           
  10000           
 
 Engine instrument operation    
   
 Propeller governor operation    
   
 Engine reversion    from idling to full power
 
 Alternate air    
 

ADAA
Validity : S / N 1 - 9999 05-30 Page 203
03 (EA) JUN 01
 

TB20 TYPICAL TEST FLIGHT AIRCRAFT S/N : F : 4/8 
  Pilot :
Date : 
Time  
 5.1 - STALLS
Deceleration rate : 1 kt/s Idling 
 Flight
configuration Trim speed
KIAS Trim tab position
up 0 down Audio warning
KIAS (1) Stalling
KIAS (2) 
 Clean 100    
 Take off 90    
 Landing 80    
 (1) Audio warning 5 to 10 kt before mini indicated airspeed
(2) Indicated airspeed for 1200 kg - Increase or decrease
5.2 - WING FLAPS OPERATION 103 KIAS
Down At = sec.
Up At = sec.
5.3 - LANDING GEAR OPERATION 130 KIAS
Normal extension At = sec.
Normal retraction At = sec.
Landing gear lights  
Gear unsafe warning  
5.4 - LANDING GEAR OPERATION 97 KIAS
Emergency extension At = sec.
Normal retraction At = sec.
5.5 - CRUISE FL 50
Cruise performance stabilization 5') of 2.5 kt per 100 kg 
    
    
    
    
  RPM Manifold
pressure
in.Hg Fuel
flow
US G/h CHT
°F EGT
°F Oil
temp. Oil
press. VI
kt IOAT
°C Trim
up 0 down
 75 %
Best power 2400 23.1         
  
 
AIRCRAFT S/N :
Pilot :
Date :
 
Time
Control rigging
RPM = 2400 - Manifold pressure = 23.1 in.Hg - Best power
 
　
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