DA 20 Red Ops Limits

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Can you name the DA 20 Red Ops Limits?

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InquiryLimits
Max tailwind component (kts)
Force propeller to windmill if stopped and starter is inop
Max. oil quantity (US qts)
Max crosswind component student solo (kts)
Forced landing final approach airspeed (flaps T/O)
Forced landing final approach airspeed (flaps CRUISE)
Max total wind student dual (kts)
Max. permissable continuous rpm
Max. oil pressure (psi)
Min. rpm for in-flight (area) idle beyond gliding rane of a runway
Voltmeter green arc (volts)
Min. rpm operations with fuel pump off
Min oil temp. to begin an area SFL at Area Idle (F)
Min. engine-out airspeed to sustain windmilling prop
Max. cumulative starter op. before cooling 3-5 min.
Maximim possible bank angle for steep turns
Max structural cruising speed
InquiryLimits
usable fuel (US gal.)
Vne (Never exceed airspeed)
Oil temperature normal operating range (F)
Max. time for oil pressure to reach 10 psi after start
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)
Min. oil quantity (US qts)
Max. takeoff weight (lbs)
Vfe (flaps T/O) Max. Airspeed with flaps extended)
DA20 max demonstrated crosswind component (kts)
Oil pressure normal operating range (psi)
Vfe (flaps LDG) (Mas. Airspeed with flaps extended)
Max total wind student solo (kts)
Max. continuous starter operation
Forced landing final approach airspeed (flaps LDG)

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