THE CITATION MUSTANG.
TAKE THE REINS OF A POWERFUL NEW BREED OF BUSINESS JET.
Moving into a jet is one of the great rites of passage in a pilot's life. With some aircraft, that move might be intimidating. Let the Citation Mustang put you at ease. The Mustang is the product of a profound understanding of what an entry-level business jet should be, created by a company that has designed, built, and certified more jets for single-pilot operation than any other manufacturer. And the result? Stellar performance in a stylishly sophisticated aircraft that makes the transition to flying a jet as easy and intuitive as possible. All at a price point well below some single-engine turboprops.
FEATURES
THE INCOMPARABLE PERFORMANCE OF A JET.
There's more to a Mustang's sleek and sporty design than just good looks. The entire aircraft is an expression of aerodynamic principles finely tuned to achieve superior performance. The nearly straight wing, for example, is engineered to provide docile handling characteristics while delivering exceptional short-field performance and the ability to climb to 41,000 feet in 27 minutes. Throughout the aircraft, the Mustang's systems are intentionally simple. So it's not surprising that it can cost less to operate than most comparably-sized twin turboprops while clocking in at speeds upwards of 400 mph.
At just under 340 knots (630 km/hr), the Mustang is an ideal balance of Citation good looks, performance and efficiency. It's pure-jet performance will enable you to take off from just 3,110 feet (948 m) of runway, climb swiftly to 41,000 feet (12,497 m) and fly 1,150 nautical miles (2,130 km). And with its more-than-ample storage area, advanced engine controls and sleek aerodynamic design, the Mustang is the bold, smart choice for an entire new generation of jet-aspiring aviators.
PERFORMANCE & SPECS
| Maximum Cruise Speed (31,000 ft / 9,449 m, mid-cruise weight) | 453 ktas | 839 km/hr |
| NBAA IFR Range (100 nm alternate) Full fuel, maximum takeoff weight | 2,002 nm | 3,708 km |
| Airport Performance (dry, level, hard-surface runway, zero wind) Takeoff distance (SL, ISA, MTOW) Landing distance (SL, ISA, MTOW) | 3,130 ft 2,700 ft | 954 m 823 m |
| Ceiling Maximum certified Single engine | 45,000 ft 28,200 ft | 13,716 m 8,595 m |
| Rates of Climb All engines Single engine | 3,945 ft/min 1,270 ft/min | 1,202 m/min 387 m/min |
| Airspeed Limits VMO from 8,000 ft (2,438 m) to 27,884 ft (8,499 m) MMO above 27,884 ft (8,499 m) | 305 kias M 0.77 | 565 km/hr (indicated) |
| Stall Speed MLW, landing configuration | 86 kcas | 159 km/hr |
| PressurizationNominal pressure differential | 9.0 psi | .62 bar |
| Outside Dimensions Overall length Overall height Wingspan | 53 ft 4 in 15 ft 4 in 50 ft 10 in | 16.26 m 4.67 m 15.49 m |
| Cabin Dimensions
(with typical interior installed) Length (excluding cockpit) Height Width |
17 ft 4 in 57 in 58 in | 5.28 m 1.45 m 1.47 m |
| Engines Two Williams International FJ44-4A Takeoff thrust Bypass ratio | 3,621 lb 1.8:1 | 16.11 kN |
| Design Weights and Capacities Maximum ramp weight Maximum takeoff weight Maximum landing weight Maximum zero fuel weight Maximum fuel capacity (6.7 lb/gal) Typical empty weight* Two crew plus stores Typical basic operating weight (BOW) Useful load** Payload with full fuel |
17,070 lb 16,950 lb 15,500 lb 12,360 lb 5,828 lb 9,915 lb 400 lb 10,315 lb 6,828 lb 927 lb |
7,743 kg 7,688 kg 7,031 kg 5,606 kg 2,644 kg 4,497 kg 181 kg 4,679 kg 3,097 kg 420 kg |
* Reflects standard aircraft with typical options, typical interior, and unusable fuel and oil.
**Amount of payload and fuel that can be carried, over and above crew (based on ramp weight).
