Miscellaneous / DA20 Operating Limits (All)

Random Miscellaneous Quiz

Can you name the DA20 Operating Limits (All)?

Quiz not verified by Sporcle

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

You're not logged in!

Compare scores with friends on all Sporcle quizzes.
Sign Up with Email
Log In

You Might Also Like...

Show Comments


Your Account Isn't Verified!

In order to create a playlist on Sporcle, you need to verify the email address you used during registration. Go to your Sporcle Settings to finish the process.