For A+ Score!!!
Max. Permissible T/O RPM CORRECT ANSWERS 2800 RPM
Wing Span of the DA20 CORRECT ANSWERS 35 ft 9 in (10.89 m)
Length of the DA20 CORRECT ANSWERS 23 ft 9 in (7.24 m)
Height of the DA20 CORRECT ANSWERS 7 ft 1 in (2.16 m)
Tire Pressures (front and back) CORRECT ANSWERS Nose: 26 psi (1.8 bar)
Main: 33 psi (2.3 bar)
Engine Type CORRECT ANSWERS Continental IO-240-B
naturally aspirated, 4 cylinder, 4 stroke-engine, fuel injected, horizontally opposed, air
cooled.
Engine Output Power and RPM CORRECT ANSWERS Output Power: 125 hp (93.2
kW) At 2800 RPM
Type of Propeller CORRECT ANSWERS Two-bladed fixed pitch propeller,
manufactured by Sensenich
5 ft 9 in (1.752 m)
Approved type of Fuel CORRECT ANSWERS AVGAS 100 or 100LL (primarily this one,
only use the other if no other option)
Oil Capacity CORRECT ANSWERS Maximum: 6.0 US qt (5.68 litres)
Minimum: 4.0 US qt (3.78 litres) (MFC requires 5 qt)
Maximum Ramp Weight CORRECT ANSWERS 1770 lbs (803 kg)
Maximum Take-off Weight CORRECT ANSWERS 1764 lbs (800 kg)
Maximum Landing Weight CORRECT ANSWERS 1764 lbs (800 kg)
VA CORRECT ANSWERS Maneuvering Speed (106 KIAS)
Do not make full or abrupt control movement above this speed. Under certain conditions
the airplane may be overstressed by full control movement.
VFE (Takeoff) CORRECT ANSWERS Maximum flap extended speed (100 KIAS)
Do not exceed