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

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