DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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