Ilyushin Il-18

· Ilyushin

Airplanes

Length

35.9 m

Flat Wing Span

37.4 m

Height

10.165 m

Flat Wing Area

140 m²

Max Seating

120

Cruise Speed

625 km/h

Max Speed

675 km/h

Max Mach

0.65 Mach

Max Ceiling

11800 m

Number of Engines

First Flight

1957-07-04

Number Built

678

Maximum Take-Off Weight

64 t (paragliders: kg)

Total Fuel Capacity

30000

Maximum Range

6500 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Ilyushin Il-18	64	30000	6500

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Shaanxi Y-9		36.065	38	106	Compare
Lockheed EC-121 Warning Star		35.4	38.45		Compare
Lockheed Constellation		35.3568	38.4048	95	Compare
Douglas DC-7	Wright R-3350 Duplex-Cyclone	34.1376	38.7096	105	Compare
Lockheed L-1249 Super Constellation		35.3568	35.6616	106	Compare
Shaanxi Y-8		34.02	38	90	Compare

All data (27 fields)

Name: Ilyushin Il-18
Manufacturer: Ilyushin
Description: The Ilyushin Il-18 (; NATO reporting name: Coot) is a large turboprop airliner that first flew in 1957 and became one of the best known Soviet aircraft of its era.
ICAO Code: IL18
First Flight: 1957-07-04
Production End: 1985-01-01
Designer: Ilyushin
Type: Turboprop airliner and reconnaissance aircraft
Length (m): 35.9
Height (m): 10.165
Cockpit Crew: 9
Max Seating: 120
Max Speed (km/h): 675
Cruise Speed (km/h): 625
Max Ceiling (m): 11800
Capacity Description: 65-120 passengers
Max Mach (Mach): 0.65
National Origin: Soviet Union
Number Built: 678
Powerplant Description: 4 × Ivchenko AI-20M axial flow turboprop engines, 3169 kW (4250 hp) each
Primary Users: Russian Air Force, Russian Naval Aviation , Air Koryo , Aeroflot (historical)
Status: In limited service
Wikipedia Article (URL): en.wikipedia.org/wiki/Ilyushin_Il-18
Flat Wing Span (m): 37.4
Flat Wing Area (m²): 140
Wake Category: M
Number of Engines: 4