1975 ANTONOV AN 26

1975

ANTONOV

AN-26

Used

General description Airplane is in well condition. Perfectly fitted for operations in Africa. pax/cargo. VAT free. Airplane time TSN 25434.15 TBO 4842.15 Landings 14554 TBO 4183 Left Engine: ??-24??, SMOH: 3202:52 hours Right Engine: ??-24??, SMOH: 229:07 hours APU: RU19A-300, TSN: 923:34 hours Interior Please see pics attached. Exterior Good condition, please see pics attached. Avionics All log books. IFR equipped and certified, NAV/COM radios, transponder, autopilot, weather radar, TCAS and etc. Options Designed for the both pax and cargo operations. Cabin is transferable. Remarks Short tips about AN-26-100: 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 9? in) Height: 8.58 m (28 ft 1? in) Wing area: 74.98 m? (807 ft?) 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)