-
Forced landing final approach airspeed (flaps LDG, kts)
55
-
Min. engine-out aispeed to sustain windmilling prop (kts)
60
-
Forced landing final approach airspeed (flaps T/O, kts)
60
-
Forced landing final approach airspeed (flaps CRUISE, kts)
64
-
Best glide airspeed (1764 lbs) (L/D Max)
73
-
VFE (flaps LDG, kts) (Max. Airspeed with flaps extended)
78
-
VFE (flaps T/O, kts) (Max. Airspeed with flaps extended)
100
-
VA (kts, 1764 lbs) (No full or abrupt control inputs above VA or overstress conditions will occur.)
106
-
VNO (Max. structural cruising speed, kts)
118
-
Force propeller to windmill if stopped, starter inop (kts)
137
-
VNE (Never exceed airspeed, kts)
164
-
Max. permissible bank angle for steep turns (in degrees)
60
-
Voltmeter green arc (volts)
12.5-16
-
Usable fuel (US gal.)
24.0
-
Max. takeoff weight (lbs)
1764
-
Min. rpm during flight if beyond gliding range of a runway (area idle)
1400
-
Min. rpm operations with fuel pump off
1400
-
Max. permissible continuous rpm (redline)
2800
-
Oil pressure normal operating range (psi)
30-60
-
Max. time for oil pressure to reach 10 psi after start (secs.)
30
-
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 (secs.)
10
-
Max. cumulative starter op. before cooling 3-5 min. (secs.)
30
-
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
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