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The particular take-off distance required may be shorter than the available runway length. In this case a lower thrust may be used. Lower thrust settings increase engine life and reduce maintenance costs. The take-off thrust available from a civil engine is a constant value up to a particular ambient temperature.
The A321 entered service in January 1994 with Lufthansa; seen here is an A321-100. The Airbus A321 was the first derivative of the A320, also known as the Stretched A320, A320-500 and A325. [6] [7] Its launch came on 24 November 1988, around the same time as the A320 entered service, after commitments for 183 aircraft from 10 customers were ...
Its fuel capacity was increased to 30,030 L (7,930 US gal) and its maximum takeoff weight to 93,000 kg (205,000 lb). It first flew in December 1996 and entered service with Monarch Airlines in April 1997. The A321's closest Boeing competitors are the 737-900/900ER, [94] and the 757-200. [27] In 2018, the A321 list price was US$118.3 million. [85]
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 A321neo has a range of 3,995 nautical miles (7,399 km), with an MTOW (maximum take-off weight) of 97 tons (97 000 kg/213 848 lb), and its engine has 24,500–35,000 lbf (109–156 kN) of thrust. It received its type certification with Pratt & Whitney engines on 15 December 2016, and simultaneous EASA and FAA certification for the CFM LEAP ...
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.
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The payload fraction of modern twin-aisle aircraft is 18.4% to 20.8% of their maximum take-off weight, while single-aisle airliners are between 24.9% and 27.7%. An aircraft weight can be reduced with light-weight materials such as titanium , carbon fiber and other composite plastics if the expense can be recouped over the aircraft's lifetime.