DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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