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At a glance
Measured figures
Il-103 · Length
Single source8 m (26 ft 3 in)[source]
Bulldog Series 120 · Length
Single sourceConfiguration
| Specification | Ilyushin Il-103 | Scottish Aviation Bulldog |
|---|---|---|
| Type | Training aircraft[source] | Basic trainer with aerobatic capability[source]Bulldog |
| National origin | Soviet Union / Russia[source] | United Kingdom[source] |
| Manufacturer | Ilyushin[source] | Beagle Aircraft / Scottish Aviation[source]Bulldog |
| Designer | Genrikh Novozhilov[source] |
23 ft 3.06 in (7.0881 m)[source]
Empty; Il-103 · Empty weight
Single sourceMaximum take-off; Il-103 · Max takeoff weight
Single source900 kg (1,984 lb)[source]
1,310 kg (2,888 lb)[source]
Empty; Bulldog Series 120 · Empty weight
Single sourceMaximum take-off; Bulldog Series 120 · Max takeoff weight
Single sourceIl-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]
Bulldog Series 120 · Range
Single source540 nmi (620 mi, 1,000 km)[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]
Bulldog Series 120 · 1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine, 200 hp (150 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Status | In service[source] | Active[source]Bulldog |
|---|
| Primary user | see Operators[source] | Royal Air Force[source]Bulldog |
|---|
| Number built | 66[source] | 328[source]Bulldog |
|---|
| Manufactured | 1994–present[source] | 1969–1982[source]Bulldog |
|---|
| Introduction date | 1996[source] | 1971[source]Bulldog |
|---|
| First flight | 17 May 1994[source] | 19 May 1969[source]Bulldog |
|---|
| Capacity | 4 pax ( max payload: 270 kg (600 lb))[source] | — |
|---|
| Aspect ratio | 7.6[source] | 8.4[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] | 2-bladed Hartzell constant speed propeller[source] |
|---|
| Stall speed | 117 km/h (73 mph, 63 kn) flaps up; 111 km/h (69 mph; 60 kn) 10° flaps[source] | 54 kn (62 mph, 100 km/h)[source] |
|---|
| Never exceed speed | 340 km/h (210 mph, 180 kn)[source] | 185 kn (213 mph, 343 km/h)[source] |
|---|
| g limits | Utility: =4.4 / -1.8; Aerobatic: +6 / -3[source] | + 6g - 3g, with no longer than 15 seconds sustained inverted flight.[source] |
|---|
| Wing loading | 89.1 kg/m 2 (18.2 lb/sq ft)[source] | 18.2 lb/sq ft (89 kg/m 2 )[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 | — |
|---|
| Developed from | — | Beagle Pup[source]Bulldog |
|---|
| Airfoil | — | NACA 63 2 615[source] |
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