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Track width between the center of the landing gears is 10.73 meters (35 feet and 2.4 inches) and 12.84 meters (42 feet and 1.5 inches) between outer sides of landing gear. Maximum take-off weight started at 319,000 kg (700,000 lbs) and was expanded to 322,000 kg (710,000 lbs) by EASA.
Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms. The derived single wheel load is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) that would have the same pavement requirements as the aircraft.
The A350-1000 is the largest variant of the A350 family and is to seat 350 passengers in a three-class cabin and 9-abreast configuration. It has a range of 8,400 nm. It is designed to replace the Airbus A340-600.
Lufthansa Systems’ Lido/Flight 4D optimises climb, cruise and descent segments of a flight based on performance specifications (data files) of the particular airframe-engine combinations, as received from the aircraft original equipment manufacturers (OEMs), as well as specific operating philosophies (flight level caps, performance ...
It has four thrust levels to power the A350 variants: 75,000 lbf (330 kN) and 79,000 lbf (350 kN) for the regional variants of the A350-900 while the baseline A350-900 has the standard 84,000 lbf (370 kN) and 97,000 lbf (430 kN) for the A350-1000.
RAYTHEON B300 Super King Air 350 (LR-2) Super King Air 350. A searchable database of aircarft with recognition and performance data.
The A350-900 is the first A350 model and seats 314 passengers in a three-class cabin and 9-abreast layout. It has a standard design range target of 8,100 nm. The −900 is designed to replace the Airbus A340-300.
