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

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