DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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