DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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