DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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