DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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