Takeoff Specifications for Citation X

Takeoff Specifications for Citation X thumbnail
The Cessna Citation X is a popular business class jet aircraft.

The Cessna Citation X is the fastest production civilian aircraft. The Citation X has Rolls Royce engines capable of speeds of Mach .92 or 972 km per hour. As of 2010, Citation X jets have taken off and landed approximately one million times.

  1. Maximum Weights

    • Maximum weights affect the takeoff and landing specifications for the Citation X. The maximum takeoff weight is 36,100 lbs. and the maximum landing weight is 31,800 lbs. The zero-fuel weight is 24,400 lbs. and the full-fuel payload is 1,369 lbs. The ramp weight is 36,400 lbs. The typically equipped empty weight is 22,100 lbs. The maximum payload is 2,300 lbs.

    Performance Calculations

    • The Cessna Citation X takeoff performance data is calculated with 15-degree flaps and required field lengths as per Federal Aviation Regulation No. 25. The takeoff field lengths are based on a level, hard surface, and a dry runway with no wind.

    Takeoff Specifications

    • At a weight of 36,100 lbs., at sea level at 59 Fahrenheit, the Citation X requires 5,140 feet. At an airport altitude of 5,000 feet at 41 F, 5,950 feet are required. At a weight of 25,000 lbs., taking off from sea level at 59 F, 3,480 feet are needed.

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References

  • Photo Credit jet engine image by Galyna Andrushko from Fotolia.com

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