DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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