Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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