DA20 Operating Limits (All)

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

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