DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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