Cessna Citation Mustang — Systems Description

1 systems description reference for the Cessna Citation Mustang.

Overview

Citation Mustang

The document is a systems description for the Cessna Citation Mustang, a light business jet designed for single-pilot operation. It provides an overview of the aircraft's performance, systems, and operational capabilities, catering to both individual operators and corporate flight departments. The Mustang is highlighted for its ease of use, advanced avionics, and operational efficiency, making it an attractive option for those transitioning from propeller aircraft to jets. The document also emphasizes the aircraft's reliability, safety features, and support network, ensuring that owners can operate the Mustang with confidence.

Maximum cruise speed: 340 KTAS at 35,000 ft
NBAA IFR range: 1,150 nautical miles (2,130 km)
Takeoff distance: 3,110 ft (948 m)
Landing distance: 2,380 ft (725 m)
Maximum certified altitude: 41,000 ft (12,497 m)
Garmin G1000 avionics suite with 15" MFD
Two Pratt & Whitney PW615F engines with 1,460 lb thrust each

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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

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