Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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