DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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