Specifications
Data from Jane's All The World's Aircraft 1988–89
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)
- Rate of climb: 8.0 m/s (1,575 ft/min)
Read more about this topic: Antonov An-26