DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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