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The Citation Excel fuselage was stretched for a 6.6 ft (2.0 m) longer cabin and joined with a large, newly designed 515.9 sq ft (47.93 m 2) wing with large trailing edge flaps for good runway performance, 16.3° wing sweep and a relatively high critical Mach number for efficient 445 kn (824 km/h) TAS cruise.
Viewed from below, showing wing sweep The 650 has a T-tail and two turbofans. In 1974, Cessna studied a long range model 700 stretch of its original Citation I powered by three JT15Ds called Citation III, with a 17,500 lb gross weight, an 8,000 lb empty weight and a 7,500 lb fuel capacity leaving 2,000 lb for the occupants, and targeting 1978 deliveries. [3]
The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.
The Cessna Citation Longitude is a business jet produced by Cessna, part of the Cessna Citation family.It remains the largest business jet by Cessna. Announced at the May 2012 EBACE, the Model 700 made its first flight on October 8, 2016, with certification obtained in September 2019.
In 2015, its unit cost was US$3.35 million. [8] Cessna ended production of the design in May 2017 due to lack of customer demand for the aircraft as a result of competition from the company's own Cessna Citation M2. The company had been selling an average of 40 Mustangs per year until the M2 was introduced in 2013, and then Mustang sales ...
Since 2020, there are four categories, based on maximum certificated take-off mass: [1]: 4-12 [2] Light (L) — aircraft types of 7,000 kg or less. Medium (M) — aircraft types more than 7,000 kg but less than 136,000 kg; and; Heavy (H) — all aircraft types of 136,000 kg or more, with the exception of aircraft types in Super (J) category; and
The 350 has the same takeoff and landing weights as the 300; maximum takeoff weight is 3400 lb (1542 kg) and the maximum landing weight is 3230 lb (1465 kg). [ 4 ] Like the 300 and 400, the 350 has a certified airframe life of 25,200 flight hours.
Max takeoff weight: 6,900 lb (3,130 kg) Fuel capacity: 106 US gal (88 imp gal; 400 L) Powerplant: 1 × Pratt & Whitney R-1340 Wasp 9-cylinder air-cooled radial engine , 600 hp (450 kW)