DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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