Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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