DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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