Antonov An-74
Antonov
About
The Arctic development of the An-72, with the same engines mounted above and ahead of the wing so that their exhaust blows over it and adds lift — the Coandă arrangement that lets a jet work from short, unpaved, snow and ice runways. Interstate Aviation Committee type certificate 13-74 gives a maximum take-off mass of 34,800 kg, a maximum ramp mass of 35,150 kg and a maximum payload of 7,500 kg, with two landing masses rather than one: 33,000 kg onto a paved or ice runway and 30,000 kg onto snow or unprepared ground. It is certificated to 10,100 m at a maximum operating Mach of 0.65, and it is flown by four — captain, first officer, navigator and flight engineer — for no more than ten passengers.
Weightscompared to Airbus A318
Capacitycompared to Airbus A318
Passenger Capacity
8% of A318 maximum capacity
Crew
Sources12 figures on this page
- Карта данных сертификата типа № 13-74 (Ан-74)13-74 rev Издание 12Aviation Register of the Interstate Aviation Committee · tier 1 · 12 figures · pages 3, 4, 5, 6
Engine Specifications
Engine Count
2×
Engine Model
Ivchenko-Progress D-36
Thrust per Engine
63.7 kN(14320 lbf)
Fuel & Cargo
Fuel Capacity
17,045 L
Production & History
Production Status
Out of production
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