DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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