- ACAC ARJ21
Infobox Aircraft
name= ARJ21
caption= Artist's impression of the ACAC ARJ21 in flight.
type=Regional jet
manufacturer=ACAC consortium
designer=ACAC consortium
first flight= Scheduled for Q4 2008
introduced= 2005
status= Under Production As Of 2008
primary user=Kunpeng Airlines
more users=Shanghai Airlines
produced= Main Production Scheduled to begin in 2009
number built= 1
unit cost= 20 Million USD As Of 2008
developed from =
variants with their own articles = ARJ21-700, ARJ21-900, ARJ21F, & The ARJ21B.The ACAC ARJ21 Xiangfeng (翔凤 Flying Phoenix)cite web |url= http://news.therecord.com/Business/article/286248 |title='Flying Phoenix' is China's first homegrown commercial aircraft |accessdate=2007-12-24 |author=The Associated Press |authorlink= |publisher=TheRecord.com ] is a twin-engined
regional airliner , and is the first passenger jet to be developed and indigenously produced by thePeople's Republic of China . This program is supported by 19 major U.S. and European aerospace components suppliers, includingGeneral Electric (engine production)cite web | title=ACAC selects General Electric to power ARJ21 | work=GE Aviation | url=http://www.geae.com/aboutgeae/presscenter/cf34/cf34_20021104.html | accessdate=2002-11-04] andRockwell Collins (avionics production).cite web | title=Rockwell Collins announces first delivery for ARJ21 | work=Rockwell Collions | url=http://www.rockwellcollins.com/news/page8116.html | accessdate=2006-07-27]Development
The ARJ21 is a key project, led by the government-controlled
ACAC consortium , which began in March 2002 as part of China's "10th Five-Year Plan". The maiden flight of the ARJ21 was planned to take place in 2005 with formal handing over of the aircraft for use 18 months afterwards;cite web | title=China-Made ARJ21 Feeder Plane to Appear at Zhuhai Aviation Show | work=People's Daily | url=http://english.people.com.cn/200211/04/eng20021104_106234.shtml | accessdate=2002-11-04] however, the design work was delayed and the final trial production stage didn't begin until June 2006.cite web | title=Self-developed jet to fly maiden trip | work=XINHUA | url=http://news.xinhuanet.com/english/2006-06/01/content_4631760.htm | accessdate=2006-06-01] The first aircraft was rolled out on21 December 2007 with plans for a maiden flight in March 2008,, however this has been delayed until September 21 2008 [name="China Gate"] , and the aircraft is expected to become available to buyers in September 2009. The ACAC consortium aims to manufacture 11 ARJ21s a year by 2010, and 50 per year by 2015.Design
Although ACAC refers to the ARJ21 as "designed by Chinese with completely independent intellectual property rights",it is being built using tooling which was originally provided by the
McDonnell Douglas company for licence-production of the MD-90 in China. Consequently, it bears a strong resemblance to the DC-9 series of aircraft, with an identical cabin cross section, nose profile and tail. The general designer of the aircraft was Mr. Wu Guanghui (吴光辉), and the deputy general designer was Mr. Zhou Jisheng (周济生), with the general engineer was Ms. Jiang Liping (姜丽萍, 1968- ). An all-newsupercritical wing , which will have a sweepback of 25 degrees and be fitted with winglets to improve aerodynamic performance, has been designed byUkraine ’sAntonov . [http://www.antonov.com/news/index.xml?news=antk-main/news_20071224.xml Website "Antonov": News ] ] cite web | title=ARJ21-A | work=AINonline | url=http://web.archive.org/web/20060204221503/http://www.ainonline.com/Features/regionalbusaircraft/arj21a.html | accessdate=2006-06-23] [ [http://www.deagel.com/news/Chinese-ARJ21-700-Airliner-Roll-Out_n000003364.aspx Chinese ARJ21-700 Airliner Roll-Out ] ] Antonov Design Bureau also assisted project with geometrical determination and integral analysis of the construction strength of ARJ21. [http://www.antonov.com/news/index.xml?news=antk-main/news_20071224.xml Website "Antonov": News ] ]In addition to the baseline and the stretched passenger models, ACAC has also proposed extended-range, freight, and business jet variants.
Manufacturer
Members of the ACAC consortium, which was formed to develop the aircraft, will manufacture major components of the aircraft:
*Chengdu Aircraft Industry Group : construction of the nose
*Shanghai Aircraft Company : final assembly
*Shenyang Aircraft Corporation : construction of the empennage (complete tail unit)
*Xian Aircraft Company : construction of the wings and fuselageThe Shanghai Aircraft Research Institute and the
Xian Aircraft Design and Research Institute , which are also members of the consortium, are responsible for the design.Variants
* ARJ21-700 – baseline model which will have a capacity of 70 to 95 passengers.
* ARJ21-900 – stretched fuselage model based on the ARJ-700, which will have a capacity of 95 to 105 passengers.
* ARJ21F – dedicated freighter version of the ARJ21-700. It will have a capacity of 5 LD7 containers or PIP pallets, with a maximum payload of 10,150 kg.
* ARJ21B – business jet version of the ARJ21-700. A typical configuration would cater for 20 passengers.Orders and options
Entries shaded in pink have been announced, but have not yet signed a firm contract.
* Note that EIS dates on this table have not been updated to reflect the delay in EIS to 2009 mentioned earlier
pecifications (ARJ21-700)
aircraft specifications
plane or copter?=plane
jet or prop?=jetcrew=
capacity=78-85 passengers
* First class: 38 in seat pitch with 2+2 seating arrangement
* Economy class: 32 in seat pitch with 3+2 seating arrangement
payload main=16.799 m³
payload alt=593.25 ft³)
* Cabin length: 18.426 m (60 ft 5.43 in
length main= 33.46 m
length alt= 109 ft 9 in
span main=27.29 m
span alt=89 ft 7 in
height main=8.44 m
height alt=27 ft 8 in
area main= 79.86m²
area alt= 859.61ft²
empty weight main= 24.955kg
empty weight alt= 55,016lb
loaded weight main= kg
loaded weight alt= lb
max takeoff weight main=40,500 kg
max takeoff weight alt=89,300 lb)
* Fuel tank capacity: 10,386 kg (22,897 lbnumber of jets=2
engine (jet)=General Electric CF34 -10A
type of jet=turbofan s
thrust main= 68.20 kN
thrust alt=15,332 lbfcruise speed main=0.78 Mach
cruise speed alt=829 km/h, 515mph
ceiling main=11,900 m
ceiling alt=39,042 ft
climb rate main= m/s
climb rate alt= ft/min
loading main=
loading alt=
range main=3,700km (2,000nm)
* Standard: convert|1200|nmi|km|abbr=on
range alt=1,400 mi, 2,200 km)
* Extended: 2,000 nmi (2,300 mi, 3,700 km)ee also
aircontent
related=
*McDonnell Douglas MD-80/MD-90 similar aircraft=
* Bombardier CRJ700/900/1000
* Embraer 170/190
*Fokker 100
*Sukhoi Superjet 100
*Mitsubishi Regional Jet
*Antonov An-148
*Tupolev Tu-334 lists=
*List of airliners
*List of Chinese aircraft see also=
*Shanghai Y-10
*Xian MA60 References
External links
* [http://www.acac.com.cn/enindex.asp ACAC Manufacturer of ARJ21]
* [http://www.aerospace-technology.com/projects/arj21/index.html Aerospace Technology on ARJ21]
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