Credit
Xu Zheng · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
L-15B · Length
Single source12.4 m (40 ft 8 in)[source]
Il-103 · Length
Single sourceConfiguration
| Specification | Hongdu JL-10 | Ilyushin Il-103 |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Training aircraft[source] |
| Manufacturer | Hongdu Aviation Industry Corporation[source] | Ilyushin[source] |
| Designer | AVIC II Yakovlev[source] | Genrikh Novozhilov[source] |
| Status | In service[source] | In service |
8 m (26 ft 3 in)[source]
Ferry; L-15B · Ferry range
Single source2,600 km (1,600 mi, 1,400 nmi)[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]
L-15B · 2 × Ivchenko-Progress AI-222K-25F afterburning turbofan with afterburner
Single source2 × Ivchenko-Progress AI-222K-25F afterburning turbofan, 41.19 kN (9,260 lbf) with afterburner[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.
| Primary users | People's Liberation Army Air Force United Arab Emirates Air Force[source] | — |
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| Introduction date | 2013[source] | 1996[source] |
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| First flight | March 13, 2006[source] | 17 May 1994[source] |
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| Hardpoints | 7 for L-15AW and 9 for L-15B with a capacity of 3500kg[source] | — |
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| Rockets | Rockets[source] | — |
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| Missiles | SD-10 (PL-12) BVR air-to-air missiles (offered for export with the L-15B) PL-8 short-range air-to-air missiles PL-5 short-range air-to-air missiles[source] | — |
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| Bombs | LS-6 family of precision-guided bombs[source] | — |
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| Country of origin | China[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. Hongdu JL-10 | — |
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| National origin | — | Soviet Union / Russia[source] |
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| Primary user | — | see Operators[source] |
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| Number built | — | 66[source] |
|---|
| Manufactured | — | 1994–present[source] |
|---|
| Capacity | — | 4 pax ( max payload: 270 kg (600 lb))[source] |
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| Aspect ratio | — | 7.6[source] |
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| 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] |
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| Wing loading | — | 89.1 kg/m 2 (18.2 lb/sq ft)[source] |
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| Power/mass | — | 8.37 kg/kW (13.75 lb/hp)[source] |
|---|
| Role | — | single-engine, low-wing training aircraft[source] |
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| 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 |
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