Miscellaneous / DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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