Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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Min. engine-out airspeed to sustain windmilling prop
Fuel tank capacity (US gal.)
Max. time for CHT below 300 degrees F in descent (minutes)
Min. oil temp for full power operation if oil pressure norm
Max. oil temperature (degrees F)
Max. rpm after start until oil temp indication registers
Propeller approx. minimum ground clearance (inches)
Max. crosswind component student dual (kts)
Max. total wind student dual (kts)
Positive limit load factor (flaps CRUISE)
V A (1764 lbs) (No full or abrupt control inputs above V A or overstress conditions will occur.)
Min. rpm for in-flight (area) idle beyond gliding range of a runway
Negative limit load factor (flaps CRUISE)
Maximum permissible bank angle for steep turns
Voltmeter upper limit red line (volts)
Fuel pressure lower limit red line (psi)
V S0 (Stall speed in LDG configuration)
Aft CG limit (at or below 1653 lbs)
Fuel pressure upper limit red line (psi)
Min. rpm during engine runup idle check
Positive limit load factor (flaps T/O or LDG)
Voltmeter green arc (volts)
Max. crosswind component student solo (kts)
Max. rpm drop during magneto check
Max. oil pressure (psi)
Forward CG limit (1764 lbs)
Min. OAT (degrees C) cabin heat not req for 10 min. before T/O
V FE (flaps LDG) (Max. Airspeed with flaps extended)
Max. oil pressure for full power operation if OAT < 0 degrees C
Forced landing final approach airspeed (flaps CRUISE)
Min. rpm drop during magneto check
V S1 (Stall speed in CRUISE configuration)
Min. oil quantity (US qts)
Min. oil temperature (degrees F)
Oil temperature normal operating range (degrees F)
Max. OAT (degrees C) operation w/ partial winterization kit
Max. permissible continuous bhp
V Y (flaps T/O) (Best rate of climb)
Min. CHT (degrees F) takeoff & descent
Aft CG limit (1764 lbs)
Max. oil quantity (US qts)
V R (Rotate Speed)
Max. ramp weight (lbs)
Max. tailwind component (kts)
Max. weight in baggage compartment (lbs)
Forward CG limit (at or below 1653 lbs)
Max. time for oil pressure to reach 10 psi after start
Max. CHT (degrees F)
Max. continuous starter operation
Nose gear tire pressure (psi)
V FE (flaps T/O) (Max. Airspeed with flaps extended)
Lift-off airspeed
V NO (Max. structural cruising speed)
Max. OAT (degrees C) operation w/ full winterization kit
Min. idle mixture rise leaned to peak (runup/shutdown)
Min. oil pressure (psi)
Max. permissible continuous rpm
Maximum airplane structural temperature (degrees C)
Best glide airspeed (1764 lbs) (L/D Max)
Max. takeoff weight (lbs)
Force propeller to windmill if stopped and starter is inop
Max. cumulative starter op. before cooling 3-5min.
Forced landing final approach airspeed (flaps LDG)
Max. total wind student solo (kts)
Min. permissible static rpm (full throttle runup)
Min. rpm operations with fuel pump off
Forced landing final approach airspeed (flaps T/O)
No-Flap landing final approach airspeed
Approved fuel grade
CHT normal operating range (degrees F)
Main landing gear tire pressure (psi)
V NE (Never exceed airspeed)
V X (flaps CRUISE) (Best angle of climb)
DA20 max. demonstrated crosswind component (kts)
Oil pressure normal operating range (psi)
Max. rpm drop difference between magnetos
Tachometer normal operating range (rpm)
Usable fuel (US gal.)
CHT caution range (degrees F)
Normal landing final approach airspeed
V X (flaps T/O) (Best angle of climb)
Voltmeter lower limit red arc (volts)
Voltmeter caution range yellow arc (volts)
Max. landing weight (lbs)
V Y (flaps CRUISE) (Best rate of climb)
Negative limit load factor (flaps T/O or LDG)
Min. oil temp. to begin an area SFL at Area Idle (degrees F)

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Created Mar 28, 2010ReportNominate
Tags:limit, limitation, operating

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