DA20 Operating Limits (All)

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

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