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BTrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
Maximum; Maximum speed
Single source1,000 km/h (620 mph, 540 kn)[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]
2 × Owj turbojet engines (without afterburner version) thrust each
Single source2 × Owj turbojet engines (without afterburner version), 16 kN (3,600 lbf) thrust each[source]
with additional external fuel tanks
Single sourcewith internal fuel or
Single source90 minutes with internal fuel or 120 minutes with additional external fuel tanks[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 · 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 | HESA Yasin | Lockheed CP-140 Aurora |
|---|---|---|
| Type | Military trainer aircraft / Jet trainer[source] | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] |
| National origin | Iran[source] | — |
| Manufacturer | HESA[source] | Lockheed Corporation[source] |
| Designer | Iran Aviation Industries Organization and Islamic Republic of Iran Air Force[source] | — |
| Status | In production[source] | Active (CP-140M only)[source] |
| Primary user | IRIAF[source] | Royal Canadian Air Force[source] |
| Number built | 21 (18 CP-140M + 3 CP-140A)[source] | |
| Introduction date | 11 March 2023[source] | 1980[source] |
| First flight | 2019[source] | 22 March 1979 (CP-140)[source] |
| Stall speed | 200 km/h (120 mph, 110 kn)[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] |
| Hardpoints | — | 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] |
| 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] |
| Rockets | — | air-to-surface rockets can be fitted after a minor retrofit.[source] |
| Bombs | — | Mk 46 Mod V torpedoes, conventional bombs[source] |
| Country of origin | — | United States[source] United States[source] |