Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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