DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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