DA20 Operating Limits (All)

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

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