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1981 ANTONOV An-26
Turboprop
OFFERED FOR SALE BY:
KAREIVIU STREET, 19 NO.
VILNIUS, Lithuania
Phone: +37061390000
Web: http://www.vialjans.com
Please, mention FlightPlanet.com when you contact the seller.
Check Terms & Conditions before you enquire.
Invalid advertisement? Report here.
Last updated:14.02.2012
Advert views:2208
UAB VIALJANS
ANDREJ VIALJANS
KAREIVIU STREET, 19 NO.
VILNIUS, Lithuania
Phone: +37061390000
Web: http://www.vialjans.com
Please, mention FlightPlanet.com when you contact the seller.
Check Terms & Conditions before you enquire.
Contact seller via e-mail
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Last updated:14.02.2012
Advert views:2208
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Registration:
Year of construction:1981
Total time (TTAF):10000 TT
Country:Lithuania
City/Aerodrome:VILNIUS
General description:
The Antonov An-26 (NATO reporting name: Curl) is a twin-engined turboprop military transport aircraft, designed and produced in the USSR from 12 March 1968.[1]
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: 2,550 km ; 900 to 1100 (1,376 nm, 1,584 mi, 485 nm, 595 nm) (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)
Price:
The Antonov An-26 (NATO reporting name: Curl) is a twin-engined turboprop military transport aircraft, designed and produced in the USSR from 12 March 1968.[1]
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: 2,550 km ; 900 to 1100 (1,376 nm, 1,584 mi, 485 nm, 595 nm) (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)
Price: