DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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