DA20 Operating Limits (All)

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

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