DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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Max. takeoff weight (lbs)
Forced landing final approach airspeed (flaps LDG)
Force propeller to windmill if stopped and starter is inop
Best glide airspeed (1764 lbs) (L/D Max)
Max structural cruising speed
Max. oil quantity (US qts)
Max. oil pressure (psi)
Max. time for oil pressure to reach 10 psi after start
Maximim possible bank angle for steep turns
Max. permissable continuous rpm
Min. rpm for in-flight (area) idle beyond gliding rane of a runway
Max. cumulative starter op. before cooling 3-5 min.
Min. rpm operations with fuel pump off
Vfe (flaps T/O) Max. Airspeed with flaps extended)
Max crosswind component student solo (kts)
Max total wind student solo (kts)
Oil pressure normal operating range (psi)
Max. continuous starter operation
Min. engine-out airspeed to sustain windmilling prop
Max. rpm after start until oil temp indication registers
Oil temperature normal operating range (F)
Min. oil quantity (US qts)
Max tailwind component (kts)
Va (1764 lbs) (No full or abrupt control inputs above Va or overstress conditions will occur)
Forced landing final approach airspeed (flaps CRUISE)
Vne (Never exceed airspeed)
usable fuel (US gal.)
Voltmeter green arc (volts)
Vfe (flaps LDG) (Mas. Airspeed with flaps extended)
Min oil temp. to begin an area SFL at Area Idle (F)
Max total wind student dual (kts)
Forced landing final approach airspeed (flaps T/O)
DA20 max demonstrated crosswind component (kts)

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Created Feb 12, 2010ReportNominate
Tags:DA 20, inquiry, limit, ops, Ops Limits, red