ILYUSHIN IL-18 Civil Aircraft Model Details

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General Information of ILYUSHIN IL-18

Designer : Ilyushin

First Flight : 21005

Number Built : 850+

Primary Users : Aeroflot Soviet Airlines; Rossiya

Produced : 1959–1978

Role : Turboprop airliner

Status : Out of production, in military and limited civilian service

Unit_Cost : $24,500,000 (2011 USD equivalent)

Variants : Ilyushin Il-38

General characteristics of ILYUSHIN IL-18

Capacity : 65-120 passengers

Crew : 9

Empty Weight : 35,000 kg (77,162 lb)

Fuel Capacity : 30,000 l (6,599 imp gal)

Height : 10.165 m (33 ft 4 in)

Length : 35.9 m (117 ft 9 in)

Max Takeoff Weight : 64,000 kg (141,096 lb)

Powerplant : 4 × Ivchenko AI-20M axial flow turboprop engines, 3,170 kW (4,250 hp) each

Propellers : 4-bladed AW-68 I constant speed feathering propellers, 4.5 m (14 ft 9 in) diameter

Wing Area : 140 m2 (1,500 sq ft)

Wingspan : 37.4 m (122 ft 8 in)

Performance of ILYUSHIN IL-18

Cruise Speed : 625km/h (388mph; 337kn) at 8,000m (26,247ft)

Maximum Speed : 675km/h (419mph; 364kn)

Range : 6,500km (4,039mi; 3,510nmi) with 6,500kg (14,330lb) payload, maximum fuel and reserves for one hour. 3,700km (2,299mi) with 13,500kg (29,762lb) maximum payload, at 84 - 85% of maximum continuous power.

Service Ceiling : 11,800m (38,714ft)

Take Off Run : 1,350m (4,429ft)

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