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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.
[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 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]
The Lanying R6000, or the Lanthanum Shadow, is designed with a maximum take-off weight of about 13,000 pounds and a maximum load of up to 4,400 pounds, the report says.
The additional fuel tanks increased the total capacity to 30,030 L (7,930 US gal). These modifications also increased the maximum takeoff weight of the A321-200 to 93,000 kg (205,000 lb). This variant first flew in December 1996, and entered service with Monarch Airlines in April 1997.
The Citation Excel fuselage was stretched and joined with an all-new, larger wing and more powerful Pratt & Whitney Canada PW306C engines for increased maximum takeoff weight and a 3,200 nmi (5,900 km) range.