Miscellaneous Quiz / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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