DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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