| Specifications
|
|---|
| Country of Origin | Russia
|
| Builder |
|
| Role |
|
| Similar Aircraft |
|
| Start of operation | April 20, 1959
|
| Total built | more than 800
|
| Cost |
|
| User Countries |
|
| Length | 117ft 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 m²
|
| Chassis | retractable, tricycle
|
| Weight Empty | 58,576lb (26,570kg) / 32.245–33.76 t
|
| Maximum take-off weight | 141,000lb (63,945kg) / 59–67 t
|
| Maximum landing weight | 48–53 t
|
| Engines | 4 × Ivchenko AE-20K/AI-20M turboprop engines
|
| Thrust (power) | 4 × 4252shp
|
| Fuel capacity | 30 (for option “D”) t
|
| Fuel consumption | first hour - 2600, then from 2200 to 1500 kg / h
|
| Cruising speed | 337kt (625km/h) / 570-630 (true) km / h
|
| Maximum speed | 364kt (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 payload | 2,000nm (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)
|
| capacity | 80–122 passengers
|
| Crew | 4-5 people
|
