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File:Antonov An-158, Antonov Design Bureau AN1688634.jpg. Add languages. ... 1,001 KB, MIME type: image/jpeg) This is a file from the Wikimedia Commons.
The Antonov An-158 is a stretched fuselage version of the aircraft, accommodating up to 100 passengers. Following a crash in February 2018, all An-148 and An-158 in Russia were grounded by the Russian Ministry of Transport. [3] [4] In addition, Cubana grounded its An-158 fleet as of May 2018 due to several technical issues with the aircraft. [5]
Since independence, Antonov has certified and marketed both Soviet-era and newly developed models for sale in new markets outside of the former soviet sphere of influence. New models introduced to serial production and delivered to customers include the Antonov An-140, Antonov An-148 and Antonov An-158 regional airliners.
This page was last edited on 17 March 2010, at 08:42 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may ...
Image Origin Type Details Aircraft; Ilyushin Il-76 Soviet Union: Military transport aircraft: N/A [citation needed] Antonov An-26 Soviet Union: N/A [citation needed] Antonov An-72 Soviet Union: N/A [citation needed] Antonov An-12 Soviet Union: N/A [citation needed] Helicopter Eurocopter AS355N Écureuil France: Light utility helicopter
Antonov An-14: Soviet Union 1958 Transport Production 656 ft (200 m) 985 ft (300 m) [3] Antonov An-72: Soviet Union 1977 Transport Production 1,312 ft (400 m) 1,148 ft (350 m) [4] Auster AOP.9: UK 1954 Artillery observer Production 675 ft (206 m) 150 ft (46 m) [5] Australian Aircraft Kits Hornet STOL: Australia 2004 Ultralight Production
Antonov An-26 This page was last edited on 30 November 2024, at 12:16 (UTC). Text is available under the Creative Commons Attribution-ShareAlike 4.0 ...
Antonov decided to install less powerful D-436-148FM engines on the first An-178 prototype, perhaps as an interim measure. The D-436-148FM is a derivative of the production-standard D-436-148 with an upgraded fan, which boosted the takeoff thrust to 7,800 kgf; it has an emergency power rating of 8,580 kgf.