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The Airbus A321 is a member of the Airbus A320 family of short to medium range, narrow-body, commercial passenger twin engine jet airliners; [b] it carries 185 to 236 passengers. It has a stretched fuselage which was the first derivative of the baseline A320 and entered service in 1994, about six years after the original A320.
Engine accessories are mounted on the side instead of bottom to accommodate lateral mounting. Also has an option in the cockpit to add 3,000 pounds (13 kN) additional thrust for "hot and high" conditions; The 33,000 lbf (150 kN) thrust V2533-A5 for the Airbus A321; The 31,330 lbf (139.4 kN) thrust V2531-E5 for the Embraer C-390 Millennium
The A320 engine, the PW1100G, had made its first static engine test run on November 1, 2012, [20] and was first tested on the 747SP on May 15, 2013. [21] The first flight of the Airbus A320neo followed on September 25, 2014. [22] The PW1100G engine achieved FAA type certification on December 19, 2014. [23]
In total, 28 test engines will be used by CFM to achieve engine certification, and 32 others will be used by Airbus, Boeing and COMAC for aircraft certification and test programs. [1] [17] The first engine entering the test program reached and sustained 33,000 lbf (150 kN) of thrust, required to satisfy the highest rating for the Airbus A321neo ...
Among the transatlantic A321neo business class seats I've seen, JetBlue is the most amenity-heavy with sliding doors and a unique front-row "Studio."
The Airbus A321neo is a single-aisle airliner created by Airbus. The A321neo (neo being an acronym for "new engine option") is developed from the Airbus A321 and Airbus A320neo family. It is the longest stretched fuselage of Airbus's A320 series, and the newest version of the A321, with the original A321ceo entering service in 1994 with ...
PARIS (Reuters) -A rift between Airbus and engine makers over plans for higher jet output blotted strong aerospace earnings this week, with worries over the supply chain's industrial capacity ...
Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.