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
Forced landing final approach airspeed (flaps CRUISE)
Max structural cruising speed
Oil pressure normal operating range (psi)
Min. rpm operations with fuel pump off
Vne (Never exceed airspeed)
Max. oil pressure (psi)
Max crosswind component student solo (kts)
Best glide airspeed (1764 lbs) (L/D Max)
Min. engine-out airspeed to sustain windmilling prop
Vfe (flaps LDG) (Mas. Airspeed with flaps extended)
Min. rpm for in-flight (area) idle beyond gliding rane of a runway
usable fuel (US gal.)
Max. continuous starter operation
DA20 max demonstrated crosswind component (kts)
Forced landing final approach airspeed (flaps LDG)
Min oil temp. to begin an area SFL at Area Idle (F)
Oil temperature normal operating range (F)
Max. takeoff weight (lbs)
Vfe (flaps T/O) Max. Airspeed with flaps extended)
Max. rpm after start until oil temp indication registers
Min. oil quantity (US qts)
Max. oil quantity (US qts)
Max. permissable continuous rpm
Maximim possible bank angle for steep turns
Max total wind student solo (kts)
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 total wind student dual (kts)
Voltmeter green arc (volts)
Forced landing final approach airspeed (flaps T/O)
Max tailwind component (kts)
Max. time for oil pressure to reach 10 psi after start

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