DA20 Operating Limits (All) Quiz by Lucius429

Inquiry	Limitation
Max. continuous starter operation
V FE (flaps LDG) (Max. Airspeed with flaps extended)
Min. permissible static rpm (full throttle runup)
Negative limit load factor (flaps T/O or LDG)
DA20 max. demonstrated crosswind component (kts)
Max. time for oil pressure to reach 10 psi after start
Propeller approx. minimum ground clearance (inches)
Main landing gear tire pressure (psi)
V X (flaps CRUISE) (Best angle of climb)
Lift-off airspeed
Max. landing weight (lbs)
Max. OAT (degrees C) operation w/ partial winterization kit
Max. takeoff weight (lbs)
Max. tailwind component (kts)
Forced landing final approach airspeed (flaps CRUISE)
Max. rpm drop difference between magnetos
Forced landing final approach airspeed (flaps T/O)
Forward CG limit (at or below 1653 lbs)
Forced landing final approach airspeed (flaps LDG)
Max. oil pressure for full power operation if OAT < 0 degrees C
Aft CG limit (at or below 1653 lbs)
Min. rpm for in-flight (area) idle beyond gliding range of a runway
V R (Rotate Speed)
V Y (flaps CRUISE) (Best rate of climb)
V Y (flaps T/O) (Best rate of climb)
Min. rpm operations with fuel pump off
Max. crosswind component student dual (kts)
Maximum airplane structural temperature (degrees C)
Min. rpm during engine runup idle check

Inquiry	Limitation
Oil temperature normal operating range (degrees F)
Voltmeter lower limit red arc (volts)
Max. total wind student dual (kts)
CHT normal operating range (degrees F)
V FE (flaps T/O) (Max. Airspeed with flaps extended)
Min. oil temperature (degrees F)
Max. oil temperature (degrees F)
Tachometer normal operating range (rpm)
V NE (Never exceed airspeed)
No-Flap landing final approach airspeed
Fuel pressure lower limit red line (psi)
Max. oil quantity (US qts)
Voltmeter green arc (volts)
Maximum permissible bank angle for steep turns
Approved fuel grade
Usable fuel (US gal.)
Fuel tank capacity (US gal.)
Min. idle mixture rise leaned to peak (runup/shutdown)
Max. permissible continuous bhp
Nose gear tire pressure (psi)
Max. total wind student solo (kts)
Max. time for CHT below 300 degrees F in descent (minutes)
Max. crosswind component student solo (kts)
Max. OAT (degrees C) operation w/ full winterization kit
V X (flaps T/O) (Best angle of climb)
Max. rpm after start until oil temp indication registers
V NO (Max. structural cruising speed)
V S1 (Stall speed in CRUISE configuration)
Min. oil quantity (US qts)

Inquiry	Limitation
Force propeller to windmill if stopped and starter is inop
Normal landing final approach airspeed
Max. CHT (degrees F)
Positive limit load factor (flaps CRUISE)
Voltmeter upper limit red line (volts)
Oil pressure normal operating range (psi)
Max. permissible continuous rpm
Min. rpm drop during magneto check
Aft CG limit (1764 lbs)
Max. oil pressure (psi)
V S0 (Stall speed in LDG configuration)
Max. weight in baggage compartment (lbs)
Positive limit load factor (flaps T/O or LDG)
Min. oil temp for full power operation if oil pressure norm
Min. CHT (degrees F) takeoff & descent
Fuel pressure upper limit red line (psi)
Min. oil temp. to begin an area SFL at Area Idle (degrees F)
V A (1764 lbs) (No full or abrupt control inputs above V A or overstress conditions will occur.)
CHT caution range (degrees F)
Max. cumulative starter op. before cooling 3-5min.
Min. oil pressure (psi)
Voltmeter caution range yellow arc (volts)
Negative limit load factor (flaps CRUISE)
Max. rpm drop during magneto check
Min. engine-out airspeed to sustain windmilling prop
Max. ramp weight (lbs)
Best glide airspeed (1764 lbs) (L/D Max)
Forward CG limit (1764 lbs)
Min. OAT (degrees C) cabin heat not req for 10 min. before T/O

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