Miscellaneous Quiz / DA20 Operating Limits (All)

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QUIZ: Can you name the DA20 Operating Limits (All)?

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

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