Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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Score 0/87 Timer 10:00
InquiryLimitation
Maximum airplane structural temperature (degrees C)
V S1 (Stall speed in CRUISE configuration)
Min. rpm during engine runup idle check
Max. crosswind component student solo (kts)
Max. takeoff weight (lbs)
Aft CG limit (at or below 1653 lbs)
V Y (flaps T/O) (Best rate of climb)
Max. landing weight (lbs)
Min. CHT (degrees F) takeoff & descent
Positive limit load factor (flaps T/O or LDG)
Forced landing final approach airspeed (flaps LDG)
Min. rpm for in-flight (area) idle beyond gliding range of a runway
Max. oil quantity (US qts)
Max. continuous starter operation
Maximum permissible bank angle for steep turns
Min. oil temp for full power operation if oil pressure norm
Min. oil quantity (US qts)
Max. crosswind component student dual (kts)
Forward CG limit (1764 lbs)
Max. rpm drop difference between magnetos
Lift-off airspeed
Forward CG limit (at or below 1653 lbs)
Max. permissible continuous bhp
Propeller approx. minimum ground clearance (inches)
V NE (Never exceed airspeed)
Fuel pressure lower limit red line (psi)
CHT caution range (degrees F)
Max. total wind student dual (kts)
Nose gear tire pressure (psi)
InquiryLimitation
Negative limit load factor (flaps CRUISE)
Min. engine-out airspeed to sustain windmilling prop
CHT normal operating range (degrees F)
Force propeller to windmill if stopped and starter is inop
V S0 (Stall speed in LDG configuration)
Max. ramp weight (lbs)
Max. weight in baggage compartment (lbs)
Min. oil temperature (degrees F)
Max. OAT (degrees C) operation w/ full winterization kit
Min. rpm drop during magneto check
V X (flaps T/O) (Best angle of climb)
Negative limit load factor (flaps T/O or LDG)
Usable fuel (US gal.)
V Y (flaps CRUISE) (Best rate of climb)
Min. idle mixture rise leaned to peak (runup/shutdown)
Min. oil pressure (psi)
No-Flap landing final approach airspeed
Voltmeter caution range yellow arc (volts)
Positive limit load factor (flaps CRUISE)
Aft CG limit (1764 lbs)
Max. rpm drop during magneto check
Min. rpm operations with fuel pump off
Voltmeter upper limit red line (volts)
V FE (flaps T/O) (Max. Airspeed with flaps extended)
Max. OAT (degrees C) operation w/ partial winterization kit
Min. permissible static rpm (full throttle runup)
Max. CHT (degrees F)
Oil temperature normal operating range (degrees F)
V R (Rotate Speed)
InquiryLimitation
Approved fuel grade
Min. OAT (degrees C) cabin heat not req for 10 min. before T/O
Normal landing final approach airspeed
V X (flaps CRUISE) (Best angle of climb)
Max. oil pressure (psi)
Max. rpm after start until oil temp indication registers
Min. oil temp. to begin an area SFL at Area Idle (degrees F)
V NO (Max. structural cruising speed)
Max. total wind student solo (kts)
Max. time for oil pressure to reach 10 psi after start
Forced landing final approach airspeed (flaps T/O)
V FE (flaps LDG) (Max. Airspeed with flaps extended)
Max. cumulative starter op. before cooling 3-5min.
DA20 max. demonstrated crosswind component (kts)
Main landing gear tire pressure (psi)
Forced landing final approach airspeed (flaps CRUISE)
Voltmeter lower limit red arc (volts)
Max. time for CHT below 300 degrees F in descent (minutes)
Fuel tank capacity (US gal.)
Max. tailwind component (kts)
Tachometer normal operating range (rpm)
V A (1764 lbs) (No full or abrupt control inputs above V A or overstress conditions will occur.)
Max. oil pressure for full power operation if OAT < 0 degrees C
Max. permissible continuous rpm
Max. oil temperature (degrees F)
Best glide airspeed (1764 lbs) (L/D Max)
Voltmeter green arc (volts)
Fuel pressure upper limit red line (psi)
Oil pressure normal operating range (psi)

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