DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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