DA20 Operating Limits (All)

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

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