DA20 OPS LIMITS Flashcards
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Min. engine-out airspeed to sustain windmilling prop (kts)
60
Forced landing final approach airspeed (flaps LDG, kts)
55
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 3-5min. (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
