DA20 Operating Limits (All)

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

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