DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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