DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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