Antonov An-38-100
Antonov
About
The stretched, Western-engined development of the An-28, designed at Antonov and built at the Chkalov works in Novosibirsk — an unglamorous high-wing commuter for unprepared strips, fitted with American turboprops and Hartzell propellers because no suitable engine was available at home. Interstate Aviation Committee type certificate 129-38 gives a maximum take-off mass of 9,500 kg, a maximum ramp mass of 9,550 kg, a maximum landing mass of 9,500 kg — the same as the take-off figure — a maximum zero-fuel mass of 8,400 kg and a maximum payload of 2,500 kg. Two TPE331-14GR turboprops drive five-blade Hartzell propellers. Two pilots carry up to 27 passengers, and the certificated ceiling depends on what is fitted: 3,000 m without oxygen equipment and 4,200 m with it. Fewer than a dozen were completed.
Weightscompared to Airbus A318
Capacitycompared to Airbus A318
Passenger Capacity
20% of A318 maximum capacity
Crew
Sources10 figures on this page
- Карта данных сертификата типа № 129-38 (Ан-38-100)129-38 rev Издание 03Aviation Register of the Interstate Aviation Committee · tier 1 · 10 figures · pages 2, 3
Engine Specifications
Engine Count
2×
Engine Model
AlliedSignal TPE331-14GR
Production & History
Production Status
Out of production
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