DA20 Operating Limits (All)

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

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