DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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

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Created Feb 12, 2010ReportNominate
Tags:DA 20, inquiry, limit, ops, Ops Limits, red