DA20 Operating Limits (All)

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

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