Miscellaneous / DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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