DA20 Operating Limits (All)

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

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