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Military


Il-18 Coot


Specifications
Country of Origin Russia
Builder 
Role
Similar Aircraft 
Start of operation April 20, 1959
Total built more than 800
Cost 
User Countries 
Length117ft 9in (35.9m)
Height 33ft 4in (10.16m) / 10.17 m
Maximum fuselage diameter 3.5 m
Wingspan 122ft 8.5in (37.4m)
Wing area 140 m
Chassis retractable, tricycle
Weight Empty58,576lb (26,570kg) / 32.24533.76 t
Maximum take-off weight141,000lb (63,945kg) / 5967 t
Maximum landing weight 4853 t
Engines 4 Ivchenko AE-20K/AI-20M turboprop engines
Thrust (power) 4 4252shp
Fuel capacity 30 (for option D) t
Fuel consumptionfirst hour - 2600, then from 2200 to 1500 kg / h
Cruising speed 337kt (625km/h) / 570-630 (true) km / h
Maximum speed364kt (675km/h) / 610 (instrument, with emergency reduction) km / h
Take-off distance 1000 m
Run length 800 m
Flight range IL-18 3,500nm (6,500km) (with fuel remaining for 1 hour of flight)
Range with max payload2,000nm (3,700km)
Practical ceiling more than 12,000 m, 10,000 m / 33,000ft (for flights with passengers) m
Armament 
Payload up to 15 tons (in cargo version)
capacity80122 passengers
Crew4-5 people



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Page last modified: 17-11-2019 19:08:25 ZULU