johnbr

Antonov_An-26

General characteristics Crew: 5 (2 pilots, 1 radio operator, 1 flight engineer, 1 navigator) Capacity: 40 passengers Payload: 5,500 kg (12,125 lb) Length: 23.80 m (78 ft 1 in) Wingspan: 29.20 m (95 ft 9½ in) Height: 8.58 m (28 ft 1½ in) Wing area: 74.98 m² (807 ft²) Empty weight: 15,020 kg (33,113 lb) Max. takeoff weight: 24,000 kg (52,911 lb) Powerplant: 2 × Progress AI-24VT turboprops, 2,103 kW (2,820 ehp) each (plus one Tumansky Ru-19-A300 type 7.85 kN (1,795 lb st) thrust small turbojet in the right nacelle which serves as APU and climb rate / high altitude cruise booster) Performance Cruise speed: 440 km/h (237 knots, 273 mph) Range: 2,500 km (1,376 nmi, 1,584 mi) with maximum fuel; 1,100 km (594 nmi, 683 mi) with maximum payload Service ceiling: 7,500 m (24,600 ft)

Antonov_An-26
johnbr, Nov 22, 2012
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  • Album:
    Aircraft Cutaways
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    johnbr
    Date:
    Nov 22, 2012
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