DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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