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Measured figures
Il-103 · Length
Single source8 m (26 ft 3 in)[source]
Il-103 · Wingspan
Single source10.56 m (34 ft 8 in)[source]
Il-103 · Height
Single source3.135 m (10 ft 3 in)[source]
Il-103 · (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)
Single source800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)[source]
Il-103 · 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine
Single source1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)[source]
Il-103 · Wing area
Single source14.71 m 2 (158.3 sq ft)[source]
Il-103 · maximum certified altitude
Single source3,000 m (9,840 ft) (maximum certified altitude)[source]
Il-103 · 623.4 ft/min
Single source3.167 m/s (623.4 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | L-15Z | Ilyushin Il-103 |
|---|---|---|
| Variant description | L-15Z : Designation of L-15 advanced fighter trainer in Zambian Air Force service.[source]Only the source-declared variant L-15Z | — |
| Type | — | Training aircraft[source] |
| National origin | — | Soviet Union / Russia[source] |
| Manufacturer | — | Ilyushin[source] |
| Designer | — | Genrikh Novozhilov[source] |
| Status | — | In service[source] |
| Primary user | — | see Operators[source] |
| Number built | — | 66[source] |
| Manufactured | — | 1994–present[source] |
| Introduction date | — | 1996[source] |
| First flight | — | 17 May 1994[source] |
| Capacity | — | 4 pax ( max payload: 270 kg (600 lb))[source] |
| Aspect ratio | — | 7.6[source] |
| Fuel capacity | — | 150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks[source] |
| Propellers | — | 2-bladed Hartzell BHC-C2YF-1BF/F8459A-8R[source] |
| Stall speed | — | 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps[source] |
| Never exceed speed | — | 340 km/h (210 mph, 180 kn)[source] |
| g limits | — | Utility: =4.4 / -1.8; Aerobatic: +6 / -3[source] |
| Wing loading | — | 89.1 kg/m 2 (18.2 lb/sq ft)[source] |
| Power/mass | — | 8.37 kg/kW (13.75 lb/hp)[source] |
| Role | — | single-engine, low-wing training aircraft[source] |
| Source measurement | — | The Ilyushin Il-103 is a single-engine, low-wing training aircraft developed by the Ilyushin Design Bureau that started in 1990 in the Soviet Union . The aircraft is now produced in Russia . It was the first Russian aircraft to achieve Federal Aviation Administration certification in 1998, it is for sale in the United States .[source]Ilyushin Il-103 · Lead; only the objects and conditions stated in this passage Russia’s United Aircraft Corporation reached an agreement with Aviation Engineering Zrt of Pécs, Hungary, to develop and licence produce a modernised version of the Ilyushin Il-103 in Hungary in March 2021.[source]Ilyushin Il-103 · Operational history / Hungary; only the objects and conditions stated in this passage Capacity: 4 pax ( max payload: 270 kg (600 lb))[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Length: 8 m (26 ft 3 in)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Wingspan: 10.56 m (34 ft 8 in)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Height: 3.135 m (10 ft 3 in)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Wing area: 14.71 m 2 (158.3 sq ft)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Empty weight: 900 kg (1,984 lb)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Max takeoff weight: 1,310 kg (2,888 lb)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Fuel capacity: 150 kg (330 lb) / 200 L (53 US gal; 44 imp gal) in two wing tanks[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Powerplant: 1 × Teledyne Continental IO-360-ES2B 6-cyl. air-cooled horizontally-opposed piston engine, 157 kW (211 hp)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Maximum speed: 220 km/h (140 mph, 120 kn)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Cruise speed: 180 km/h (110 mph, 97 kn)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Stall speed: 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Never exceed speed : 340 km/h (210 mph, 180 kn)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Range: 800 km (500 mi, 430 nmi) (at cruising speed, pilot and 270 kg (600 lb) payload with 30 min fuel reserve)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Service ceiling: 3,000 m (9,840 ft) (maximum certified altitude)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage Rate of climb: 3.167 m/s (623.4 ft/min)[source]Ilyushin Il-103 · Specifications (Il-103); only the objects and conditions stated in this passage |