DA20 Operating Limits (All)

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

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