DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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