DA20 Operating Limits (All)

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

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