Credit
Xu Zheng · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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BTrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
Maximum take-off; L-15B · Max takeoff weight
Single source11,600 kg (25,574 lb)[source]
CP-140 · 4 × Allison T56-A-14-LFE turboprop engines each
Single source4 × Allison T56-A-14-LFE turboprop engines, 4,909 hp (3,661 kW) each[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]
CP-140 · Wing area
Single source1,300 sq ft (120 m 2 )[source]
CP-140 · on station at 1,000 nmi (1,151 mi; 1,852 km) radius
Single source8 hours 12 minutes on station at 1,000 nmi (1,151 mi; 1,852 km) radius[source]
CP-140 · Service ceiling
Single source35,100 ft (10,700 m)[source]
CP-140 · Hardpoints: 8 in weapons bay; 10 under-wing from capacity with a capacity of
Single sourceCP-140 · total in weapons bay, with provisions to carry combinations of
Single sourceHardpoints: 8 in weapons bay; 10 under-wing from 611 to 2,450 lb (277 to 1,111 kg) capacity with a capacity of 4,800 lb (2,177 kg) total in weapons bay, with provisions to carry combinations of:[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Hongdu JL-10 | Lockheed CP-140 Aurora |
|---|---|---|
| Type | Advanced jet trainer Light combat aircraft[source] | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] |
| Manufacturer | Hongdu Aviation Industry Corporation[source] | Lockheed Corporation[source] |
| Designer | AVIC II Yakovlev[source] | — |
| Status | In service[source] | Active (CP-140M only)[source] |
| Primary users | People's Liberation Army Air Force United Arab Emirates Air Force[source] | — |
| Introduction date | 2013[source] | 1980[source] |
| First flight | March 13, 2006[source] | 22 March 1979 (CP-140)[source] |
| Hardpoints | 7 for L-15AW and 9 for L-15B with a capacity of 3500kg[source] | 8 in weapons bay; 10 under-wing from 611 to 2,450 lb (277 to 1,111 kg) capacity with a capacity of 4,800 lb (2,177 kg) total in weapons bay, with provisions to carry combinations of: Other: signal chargers, smoke markers , illumination flares[source] |
| Rockets | Rockets[source] | air-to-surface rockets can be fitted after a minor retrofit.[source] |
| 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] | — |
| Bombs | LS-6 family of precision-guided bombs[source] | Mk 46 Mod V torpedoes, conventional bombs[source] |
| Country of origin | China[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. Hongdu JL-10 | United States[source] United States[source] |
| Primary user | — | Royal Canadian Air Force[source] |
| Number built | — | 21 (18 CP-140M + 3 CP-140A)[source] |
| Retired | — | 2011 (CP-140A only)[source] |
| Developed from | — | Lockheed P-3 Orion[source] |
| Fuel capacity | — | 7,661 imp gal (9,200 US gal; 34,828 L) usable fuel in one fuselage tank and four wing integral tanks[source] |
| Aspect ratio | — | 7.5[source] |
| Airfoil | — | root: NACA 0014 (modified) ; tip: NACA 0012 (modified)[source] |
| Propellers | — | 4-bladed Hamilton Standard 54H60, 13 ft 6 in (4.11 m) diameter constant-speed fully-feathering reversible-pitch propellers[source] |
| Maximum transit speed | — | 395 kn (455 mph; 732 km/h) at optimum altitude[source] |
| FAR balanced field length | — | 7,900 ft (2,408 m)[source] |
| Take-off distance to 50 ft (15 m) | — | 6,000 ft (1,829 m)[source] |
| Landing distance from 50 ft (15 m) | — | 3,200 ft (975 m) at 114,000 lb (51,710 kg) landing weight[source] |
| Other | — | signal chargers, smoke markers , illumination flares[source] |