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| AIRCRAFT - FIXED-WING - CIVIL - Russian Federation
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Design study announced early 1991.
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Included in state development programme of civil aviation in the Russian Federation for the period extending to the year 2000. Adopted by Russian Transport Minister 22 May 1992. |
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No production plans announced by January 1997. |
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Four versions projected: single class with up to 168 seats; mixed class for 12 first class and 114 tourist passengers; convertible passenger/freighter; casualty evacuation version. |
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Conventional low-wing monoplane with underwing engines, |
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supercritical high aspect ratio wings, sweptback 25º, with winglets, |
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all-swept tail surfaces, with tailplane mounted on tailcone.
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Fly-by-wire. |
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Hydraulically retractable tricycle type; four-wheel bogie main units, twin nosewheels. |
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Two Samara high bypass turbofans, each rated at 107.9 kN (24,250 lb st). |
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Crew of two side by side on flight deck,provision for flight engineer if required. |
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Typically 150 seats six-abreast with centre aisle; galley, toilets, seats for flight attendants front and rear. |
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Doors at front and rear of cabin on port side; service doors opposite; two emergency exits each side over wing. |
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Integrated flight and nav/com systems for operation to ICAO Cat. IIIa standards.::: (estimated). |
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