Da-20 Ops Limits
33 Questions
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Questions and Answers
- 1.Forced landing final approach airspeed (flaps LDG, kts)
- 2.Min. engine-out airspeed to sustain windmilling prop (kts)
- 3.Forced landing final approach air speed (flaps T/O, kts)
- 4.Forced landing final approach airspeed (flaps CRUISE, kts)
- 5.Best glide air speed (1, 764 lbs) (L/D Max)
- 6.V (flaps LDG, kts) (MAX airspeed with flaps extended)
- 7.V (flaps T/O, kts) (MAX Airspeed with flaps extended)
- 8.Va (kts, 1764 lbs) (No full or abrupt control inputs above Va or overstress conditions will occur)
- 9.Vno (Max structrual cruising speed, kts)
- 10.Force propeller to windmill if stopped, starter inop (kts)
- 11.Vne (never exceed airspeed, kts)
- 12.Max permissible bank angle for steep turns (in degrees)
- 13.Voltmeter green arc (volts)
- 14.Usable fuel (US gal.)
- 15.Max takeoff weight (lbs)
- 16.Min. rpm during flight if beyond gliding range of runway (area idle)
- 17.Min. rpm operations with fuel pump off
- 18.Max permissible continuous rpm (redline)
- 19.Oil pressure normal operating range (psi)
- 20.Max time for oil pressure to reach 10 psi after start (secs)
- 21.Max oil pressure (psi)
- 22.Max rpm after start until oil temp indication registers
- 23.Oil temperature normal operating range (degrees F)
- 24.Min oil temp to begin an area SFL at area idle (degrees F)
- 25.Min oil quantity (US qts)
- 26.Max oil quantity (US quarts)
- 27.Max continuous starter operation (secs)
- 28.Max cumulative starter operation before cooling 3-5 min (secs)
- 29.Max total wind student dual (kts)
- 30.Max total wind student solo (kts)
- 31.DA20 max demonstrated crosswind component (kts)
- 32.Max crosswind component student solo (kts)
- 33.Max tailwind component (kts)
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