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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.
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
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.
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In the United States, the FAA uses a slightly different categorization, adding a block between medium and heavy, labeling aircraft capable of maximum takeoff weights more than 41,000 pounds (19 t) and less than 300,000 pounds (140 t) as "Large". [7] Of special note here is the narrow-bodied Boeing 757.