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

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