Shanghai Y-10
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Y-10 | |
---|---|
Role | Narrow-body jet airliner |
Manufacturer | Shanghai Aircraft Manufacturing Factory
|
Designer | Shanghai Aircraft Research Institute[1] |
First flight | 26 September 1980[1] |
Number built | 3 |
The Shanghai Y-10 or Yun-10 (
Due to unavailability of the intended
History
Development work, given code name 708, began in Shanghai in August, 1970 for
Three aircraft were built by the Shanghai Aircraft Manufacturing Factory (now known as
The Y-10 is an indigenous Chinese design.
By the time the prototype was first flown, debate about its viability surfaced, based on a design that was already 30 years old. CAAC, which already owned a modest Western fleet, would not purchase the plane. China was beginning to embrace trade with the West, and some saw the isolationist design as an inefficient throwback to Maoism. China in the early reform era was ruled by rehabilitated cadres previously persecuted in the Cultural Revolution by Wang Hongwen, the project initiator, resulting in the cancellation of the project in 1983, officially due to cost and market concerns. During its maiden flights, no governmental officials attended the ceremonies for fear of the connection to Wang Hongwen and the Gang of Four. By 1985, Shanghai Aircraft Manufacturing Factory had been granted production licensing for the McDonnell Douglas MD-80 and shifted all efforts towards that program.
A model of an AWACS variant has been seen, resembling the Boeing E-3 Sentry AWACS aircraft.[1]
-
Cockpit
-
Overhead
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Flight engineer's station
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Navigator's station
Specifications (Y-10)
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)
- Height: 13.42 m (44 ft 0 in)
- Wing area: 244.5 m2 (2,632 sq ft)
- Empty weight: 58,120 kg (128,133 lb)
- Max takeoff weight: 102,000 kg (224,872 lb) (Some sources quote 110,227 kg (243,009 lb))
- Fuel capacity: 51,000 kg (112,436 lb)
- Powerplant: 4 × Pratt & Whitney JT3D-3B turbofanengines, 84.7 kN (19,000 lbf) thrust each
Performance
- Maximum speed: 974 km/h (605 mph, 526 kn)
- Max Cruise Speed: 917 km/h (570 mph; 495 kn)
- Economical Cruise Speed: 830–850 km/h (520–530 mph; 450–460 kn)
- Landing speed: 250 km/h (160 mph; 130 kn)
- Range:
- Max payload: 5,560 km (3,450 mi; 3,000 nmi)
- Max fuel: 8,000 km (5,000 mi; 4,300 nmi)
- Service ceiling: 12,330 m (40,450 ft)
- Thrust/weight: 0.313 [citation needed]
See also
- COMAC C919
- COMAC ARJ21
Aircraft of comparable role, configuration, and era
Related lists
- List of jet airliners
References
- ^ ISBN 978-1-902109-04-6.
- ISBN 978 7 313 09555 8
- ^ "航空工业六十年:从运十到COMAC919". 民航资源网. September 27, 2009. Retrieved August 10, 2017.
路透社评论:"在得到这种高度复杂的技术时,再也不能视中国为一个落后国家了。"
- ^ a b "Y-10". globalsecurity.org. Retrieved September 7, 2011.
- ^ 运-10研制经纬谈.
- JSTOR 30173489.
Further reading
Taylor, W. R. (Ed.). Jane's All the World's Aircraft, 1980–81. (London: Jane's Publishing Company), pp. 40 ff.