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

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