Miscellaneous / DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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