DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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