DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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