DA20 Operating Limits (All)

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

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