Single Engine Performance and Airspeeds Flashcards
Vr
Rotation speed 71 KIAS
Vx
Best angle of climb 71 KIAS
Vy
Best rate of climb 85 KIAS
Vxse
Best angle 1 engine 85 KIAS
Vyse
Best rate 1 engine 85 KIAS
Vso
Stall speed w/ Flaps down 60 KIAS
Vs1
Stall Speed w/ Flaps up 70 KIAS
Vmc
Min Control 1 Engine 65 KIAS
Va 3000 lbs
Maneuvering 116 KIAS
Va Max Gross
Maneuvering 132
Vno
Max Structural Cruise 154
Vne
Never Exceed 194
Vsse
Safe Single Engine Speed (1 engine intentional) 71 KIAS
Vlr
Max gear retraction 112 KIAS
Vle/Vlo
Max gear Extension 140 KIAS
Vfe
Flap extension
20 degrees = 120
full flap = 110
Vg 3000 lbs
Best Glide 82
Vg Max Gross
Best Glide 95 KIAS
Xwind
Max Demonstrated 25 KIAS
What is Zero Fuel Weight
Zero fuel weight is the maximum weight of passengers and baggage less the fuel weight that the airplane can withstand before structural damage occurs. Zero fuel weight for the Duchess is 3,500 lbs.
Max Ramp Weight
3916 lbs
Max TO weight
3900 lbs
Max Landing Weight
3900 lbs
Max Zero Fuel Weight
3500 lbs
Max Weight Baggage compartment
200 lbs
Maximum useful load
1470 lbs
Accelerate-Stop Distance
Accelerate-Stop distance is the distance required to accelerate to liftoff speed (71) and, assuming failure of an engine at the instant liftoff speed is attained, bringing throttles to idle and stopping the airplane.
Accelerate-Go Distance
Accelerate-Go distance is the distance required to accelerate to liftoff speed (71) and, assuming failure of an engine at the instant liftoff speed is attained, continuing the takeoff and climbing to 50’. Know before you try to takeoff whether you can maintain control and climbout if you lose an engine with the
gear still down!
Takeoff Weight To Achieve A Positive Single Engine Rate Of Climb at Liftoff
This chart is for exactly what the title implies. Plug in your weight from the weight & balance to determine if you will be able to climb at liftoff, period. If you can’t, then you are committed to pulling throttles to idle and stopping the airplane. Accelerate-Go would be impossible in this case.