DA20 Operating Limits (All)

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

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