DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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