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41 Cards in this Set

  • Front
  • Back
Engine Fire On The Ground
Fuel shutoff valve-off
Cabin Heat-off
Electrical Fire On The Ground
Gen/Bat Master Switch-off
Abort
Throttle-Idle
Brakes-As Required
Flaps-Cruise
Engine Malfunction in Flight (sufficient runway remaining to land)
Airspeed-60 KIAS
Flaps-LDG
Engine Malfunction in Flight(Fuel Pressure Loss)
Fuel Pump-on
Engine Fire During Flight
Fuel shutoff valve-off
Cabin Heat-off
Electrical Fire During Flight
Gen/Bat Master Switch-off
Air Vents and Windows-Open
Cabin Fire in Flight
Gen/Bat Master Switch-Off
Air Vents and Windows-open
Cabin Heat-off
Forced Landing Final Approach Airspeed (flaps ldg, kts)
55
Min. Engine-out airspeed 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
Vve (flaps LDG, kts) (max airspeed with flaps extended)
78
Vve(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
Vnd(Max structural cruising speed, kts)
118
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. Take-off 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
100
Max rpm after start until oil temp indication registers
1000
Oil temperature normal operating range (degreees fahrenheit)
170-220
Min oil temp to begin an area sfl at area idle (degrees fahrenheit)
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
Force Propeller to windmill if stopped, starter inop(kts)
137