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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]
Typical missions are 2.0–2.7 hours and with 400 kn (740 km/h) block speeds and most operators can fly 5–6 hours at Mach 0.72–0.76 for a 2,000–2,400 nmi range, with short takeoff requirements and good hot and high performance. A first hour fuel burn of 2,000–2,500 lb (910–1,130 kg) followed by 1,600–1,900 lb (730–860 kg) the ...
The ACN, a number that expresses the relative effect on an airplane of a given weight on a pavement structure for a specified standard subgrade strength; The PCN, a number (and series of letters) representing the pavement bearing strength (on the same scale as ACN) of a given pavement section (runway, taxiway, apron) for unrestricted operations.
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Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
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 ...
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.