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It can take off at 3,640 ft (1,110 m) and climb to FL410 in 19 min and to FL430 in 26 min. It travels 400 nmi (740 km) in the first hour while burning 2,000 lb (910 kg) at FL410, 420 nmi (780 km) the second hour with 1,550 and 1,400 lb (700 and 640 kg) the third hour at FL430. [ 2 ]
Takeoff weight components. 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.
Embraer is firm on list price while Textron discounts the Latitude by up to 20% for $13.5–14 ... Empty weight: 18,656 lb (8,462 kg) Max takeoff weight: 30,800 lb ...
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
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
The difference between the maximum taxi/ramp weight and the maximum take-off weight (maximum taxi fuel allowance) depends on the size of the aircraft, the number of engines, APU operation, and engines/APU fuel consumption, and is typically assumed for 10 to 15 minutes allowance of taxi and run-up operations.
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 difference between the maximum taxi/ramp weight and the maximum take-off weight (maximum taxi fuel allowance) depends on the size of the aircraft, the number of engines, APU operation, and engines/APU fuel consumption, and is typically assumed for 10 to 15 minutes allowance of taxi and run-up operations.