DA20 Operating Limits (All)

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

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