DA20 Operating Limits (All)

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

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