DA20 Operating Limits (All)

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Can you name the DA20 Operating Limits (All)?

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

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