DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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