DA20 Operating Limits (All)

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

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