Cruise Performance

Cruise is the predominant phase of flight by time, making cruise performance one of the most influential factors on the duration and quality of a flight.



Cruise Performance

Cruise Performance Introduction



Cruise Performance

Understanding the Drag Curve



Cruise Performance

Maximum Range

  • As seen in Figure 5-6, at some given airspeed, total drag is at its minimum amount.
  • In determining the maximum range of aircraft, minimizing drag minimizes the thrust to overcome it.
  • The minimum power and maximum endurance occur at different points.


Cruise Performance

Maximum Endurance

  • The best endurance airspeed is an airspeed that allows an aircraft to remain flying for the longest time.
  • As weight increases, the airspeed required to maintain max endurance increases; however, the optimal angle of attack remains constant.
  • As weight decreases, airspeed required to maintain max endurance decreases; however, the optimal angle of attack remains constant.


Cruise Performance

Factors Impacting Cruise Performance

  • Wind Impacts on Cruise Flight:

    • Wind direction and intensity at various cruise altitudes are essential considerations to determine cruise performance.
    • Winds aloft are the most direct means to plan for winds at cruise altitudes along the route of flight.
    • Headwinds increase flight time and therefore fuel burn, reducing range, while tailwinds do just the opposite.
  • Icing Impacts on Cruise Flight:

    • When encountering icing, additional power may be necessary to overcome the increase in drag.
    • Airspeed may bleed off quickly (one example saw 50 knots in under 1 minute)
    • See also: Stall and Climb Performance.


Cruise Performance

Applying Maneuvering Speed to Cruise

  • Maneuvering speed, or Va, is an airspeed below which full deflection of the control surfaces should not cause damage.
  • If approaching bumpy weather, consider slowing to Va before penetrating turbulence.
  • Rule of thumb: for every 2% reduction in weight, Va reduces by 1%.


Cruise Performance

Aircraft Cruise Performance

  • Cruise Performance
    Cruise Performance
  • Cruise performance data enables pilots to plan long-distance, cross-country flights while simultaneously allowing pilots to determine fuel reserves.
  • Cruise Performance Chart Example:

    • Start by choosing the chart that meets the prerequisites (i.e., weight, temperature).
    • Choose the cruise altitude flown and move right to the appropriate temperature at altitude.
    • The RPM dictates the desired performance.
    • Fuel burn understandably increases with RPM setting:
      • Using 6,000 feet at standard temperature, 2100 RPM is 5.4 Gallons Per Hour (GPH) at 92 knots.
      • Increasing by 100 RPM increases fuel burn to 5.7 GPH (+6%) at 98 knots (+7%).
    • As you increase RPM, the aircraft (at least in our example) will experience diminishing returns where fuel burn increases are larger, and speed benefits are less.
      • Using 6,000 ft at standard temperature, 2500 RPM is 7.6 GPH at 115 knots.
      • Increasing by 100 RPM increases fuel burn to 8.4 (+11%) at 120 Knots (+4%).
  • Cruise Performance
    Cruise Performance


Cruise Performance

Cruise Performance Conclusion

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Cruise Performance

Cruise Performance References