DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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