DA20 Operating Limits (All)

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

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