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The Comac C919 is a narrow-body airliner developed by Chinese aircraft manufacturer Comac. The development program was launched in 2008. Production began in December 2011, with the first prototype being rolled out on 2 November 2015; the maiden flight took place on 5 May 2017. On 29 September 2022 the C919 received its CAAC type certificate.
The corporation is a designer and constructor of large passenger aircraft with capacities of over 150 passengers. The first aircraft marketed by Comac is the ARJ21 regional jet, which was developed by China Aviation Industry Corporation I (AVIC I). This was followed by the C919 narrow-body aircraft, which can seat up to 168 passengers and made ...
Data from Chinese Aircraft:China's aviation industry since 1951 [1] General characteristics. Crew: 5 (pilot, co-pilot, flight engineer, navigator, radio operator) Passenger capacity: High density: 178; All economy: 149; Mixed class: 124; Max payload: 16,700 kg (36,817 lb) Length: 42.93 m (140 ft 10 in) Wingspan: 42.24 m (138 ft 7 in)
Powered by Pratt & Whitney Canada PW127J turboprop engines, it has a 60-passenger capacity. [citation needed] As of October 2018, over 300 have been ordered. [citation needed] Xi'an Aircraft Industry Co., manufacturer of the MA600, noted that the successful test flight is "an important milestone" in Chinese domestic aircraft production.
Y-5A – First mass-produced, version, light passenger transport, equivalent to the An-2T. Y-5B – agricultural aircraft, equivalent to the An-2 SKh. Y-5B-100 – Y-5B aircraft fitted with triple tipsails on the upper wing tips, which reputedly gave 20% higher climb rate and improved L/D ratio by 15%.
The 2008 model was equipped with 6-bladed slightly swept propellers and showed 28 passenger windows per side. Powered by Pratt & Whitney Canada PW150C turboprops, the fly-by-wire aircraft will seat up to 86 passengers, will have a maximum take-off weight of 26.5 t (58,000 lb) and a range of up to 2,700 km (1,500 nmi). [8]
Data from Jane's All The World's Aircraft 2003–2004 General characteristics Crew: 2 Capacity: 62 passengers Length: 24.71 m (81 ft 1 in) Wingspan: 29.2 m (95 ft 10 in) Height: 8.86 m (29 ft 1 in) Wing area: 75 m 2 (810 sq ft) Airfoil: root: TsAGI S-5-18; tip: TsAGI S-3-13 Empty weight: 13,700 kg (30,203 lb) Max takeoff weight: 21,800 kg (48,061 lb) Powerplant: 2 × Pratt & Whitney Canada ...
The Y-9 is designed for 25 tons of cargo but can carry up to 30 tons in overload configuration. The cargo area has a length of 16.2 m (53 ft), a width of 3.2 m (10 ft), and a height of 2.35 m (7.7 ft). The aircraft can fit up to 106 passengers, 132 paratroopers, or 72 stretchers.