AN-26

The Antonov AN-26 is a twin-engine military transport aircraft designed in the Soviet Union and produced between 1968 and 1985. Derived from the AN-24, it has been specially modified for tactical transport missions, notably with the addition of a rear loading ramp to facilitate the transport of bulky freight and the dropping of paratroopers.

Key features

  • Dimensions :
    • Length: 69,1m.
    • Span: 73,3m.
    • Height: 20,78m.
  • Load capacity :
    • Maximum payload: 120 tonnes for the An-124-100 version, rising to 150 tonnes for the AN-124-100M-150 version.
    • Cargo volume : 750 m³.
  • Performances:
    • Cruising speed : 800 à 850 km/h.
    • Maximum range: 4,800 km with a 120-tonne load, up to 15,700 km in ferry configuration (unloaded).
    • Operating ceiling: 12,000m.
  • Motorisation : Four Lotarev D-18T turbojet engines, each developing 229.5 kN of thrust.
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Device details

Brand

Model

AN-26

Maximum payload

5500 kg

Dimensions of the main hold

1110x220x160 cm

Main door dimensions

220×165 cm

features

Total load volume

30 m³

Range

600 km

Cruising speed

440 km/h

Reservation

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