Antonov AN-26

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Data

ModelAN-26
IATAA26
ICAOAN26
ManufacturerANTONOV
StatusOperational
Wingspan29.3 m (96 ft 2 in)
Max Take-off Weight24,000 kg (52,911 lb)
Cruise speed440 km/h (273 mph; 238 kn)
Range2,500 km (1,553 mi; 1,350 nmi) with maximum fuel
Ceiling7,500 m (24,600 ft)
Engines2 x 2.820 SHP Ivchenko AI 24VT turboprops with 4 blade propellers and 8.83 kN RU 19-300 aux turbojet in starboard nacelle.
ICAO Mass Group2
Approach GroupB
Wake Turbulence GroupM
Type codeL2T

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Overview

Military tactical transport aircraft. In service since 1968. More powerful development of An-24 with rear loading ramp and redesigned tail for military use. Chinese versions Y-7 and Y-7H. Civil version An-26S. In production from 1968 to 1985. Over 550 An-26s are in world wide civil service.

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Sources as credited. May also contain data from any of the following - Wikipedia