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

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