DA20 Operating Limits (All)

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

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