DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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