DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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