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Commercial or passenger aircraft are usually designed for optimum performance around their cruise speed (VC) and cruise altitude. Factors affecting optimum cruise speed and altitude include payload, center of gravity, air temperature, and humidity.
The subject of aircraft performance includes aircraft speed, ceiling, range and fuel efficiency, take-off distance required, and climb rate. It also includes aircraft controllability speeds.
Aircraft cruise speeds vary based on optimization of fuel burn, range, and efficiency. Jet engine efficiency increases with altitude and speed due to factors like air density and thrust. The range of a jet aircraft depends on speed, drag, and fuel efficiency, impacted by factors like weight and wind.
Factors affecting optimum cruise speed and altitude include payload, center of gravity, air temperature, and humidity. Cruise altitude is usually where the higher ground speed is balanced against the decrease in engine thrust and efficiency at higher altitudes.
It depends on many factors, such as the design of the aircraft, the engine power, the flight conditions, and the pilots skills. If we have to choose one factor that has the most predominant effect on aircraft performance, it would be the atmospheric conditions.
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With a heavier aircraft, your AOA in cruise is closer to the critical AOA, causing you to stall at a faster airspeed. A lighter aircraft will have more degrees of AOA to increase before it encounters the critical AOA, causing you to stall at a lower airspeed.
The primary factors most affected by performance are the takeoff and landing distance, rate of climb, ceiling, payload, range, speed, maneuverability, stability, and fuel economy.
An aircrafts optimal speed and altitude during cruise depend on several factors, such as payload, center of gravity, air temperature, humidity, and fuel efficiency. Generally, commercial airliners cruise at altitudes between 31,000 and 39,000 feet, where the air is thinner and drag is minimized.

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