DA20 Operating Limits (All)

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

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