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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.
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 maximum takeoff weight (also known as the maximum brake-release weight) is the maximum weight authorised at brake release for takeoff, or at the start of the takeoff roll. The maximum takeoff weight is always less than the maximum taxi/ramp weight to allow for fuel burned during taxi by the engines and the APU.
The A321-100 maximum takeoff weight is increased by 9,600 kg (21,200 lb) to 83,000 kg (183,000 lb). [9] To maintain performance, double-slotted flaps were included, in addition to increasing the wing area by 4 m 2 (43 sq ft), to 128 m 2 (1,380 sq ft). [27] The maiden flight of the first of two prototypes came on 11 March 1993. [14]
[3] [11] [13] [14] Maximum Take-Off Weight (MTOW) was increased by 1,000 lb (450 kg). [12] After protracted development including extensive wind tunnel testing of the design (especially of the T-tail which was tunnel-tested for 375 hours), [ 11 ] the first prototype flew for the first time on October 27, 1972; [ 15 ] a second prototype took to ...
From the very beginning, the MD-11X was conceived in two different versions. The MD-11X-10, based on a DC-10-30 airframe, offered a range of 6,500 nautical miles (12,000 km; 7,500 mi) with passengers. That first version would have had a maximum takeoff weight (MTOW) of 580,000 pounds (260,000 kg) and would have used CF6-80C2 or PW4000 engines ...
[32] [33] [34] Both the earlier and later takeoff weights establish the An-225 as the world's heaviest aircraft, exceeding the weight of the double-deck Airbus A380 airliner. Airbus claims to have improved upon the An-225's maximum landing weight by landing an A380 at 591.7 t (652.2 short tons) during testing. [35] [a]
The introduction of the TBM 700C2, which increased the maximum takeoff weight from 6,578 to 7,394 lb (2,984 to 3,354 kg), enabled operators to fly with both fully laden fuel tanks and maximum cabin occupancy instead of compromising between the two due to weight restrictions.