DA20 Operating Limits (All)

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

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