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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