DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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