Forced landing final approach airspeed (flaps LDG)

55

Min. engine-out airspeed to sustain windmilling prop

60

Forced landing final approach airspeed (flaps T/O)

60

Forced landing final approach airspeed (flaps CRUISE)

64

Best glide airspeed (1764 lbs)  (L/D Max)

73

V_FE (flaps LDG)  (Max. Airspeed with flaps extended)

78

V_FE (flaps T/O) (Max. Airspeed with flaps extended)

100

V_A (1764 lbs) (No full or abrupt control inputs above V_A or overstress conditions will occur.)

106

V_NO (Max. structural cruising speed)

118

Force propeller to windmill if stopped and starter is inop

137

V_NE (Never exceed airspeed)

164

Maximum permissible bank angle for steep turns

60°

Voltmeter green arc (volts)

12.5-16

Usable fuel (US gal.)

24.0

Max. takeoff weight (lbs)

1764

Min. rpm for in-flight (area) idle beyond gliding range of a runway

1400

Min. rpm operations with fuel pump off

1400

Max. permissible continuous rpm

2800

Oil pressure normal operating range (psi)

30-60

Max. time for oil pressure to reach 10 psi after start

30 sec.

Max. oil pressure (psi)

100

Max. rpm after start until oil temp indication registers

1000

Oil temperature normal operating range (°F)

170-220

Min. oil temp. to begin an area SFL at Area Idle (°F)

170

Min. oil quantity (US qts)

4

Max. oil quantity (US qts)

6

Max. continuous starter operation

10 sec.

Max. cumulative starter op. before cooling 3-5min.

30 sec.

Max. total wind student dual (kts)

25

Max. total wind student solo (kts)

20

DA20 max. demonstrated crosswind component (kts)

20

Max. crosswind component student solo (kts)

10

Max. tailwind component (kts)

5