ATrainer aircraft
Lockheed CP-140 Aurora
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
Credit
Ken Mist · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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ATrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
CP-140 Aurora · Length
Single sourceCP-140 · Length
Single sourceConfiguration
| Specification | Lockheed CP-140 Aurora | Saab Safari |
|---|---|---|
| Type | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] | Primary trainer[source] |
| Manufacturer | Lockheed Corporation[source] | Saab AB[source] |
| Status | Active (CP-140M only)[source] | Active[source] |
| Primary user | Royal Canadian Air Force[source] | — |
Safari · Length
Single source7.00 m (23 ft 0 in)[source]
Gross; CP-140 Aurora · Gross weight · Maximum gross weight
Single sourceGross; CP-140 · Gross weight
Single source61,362 lb (27,833 kg)[source]
64,410 kg[source]CP-140 Aurora · Maximum gross weight
Empty; Safari · Empty weight
Single sourceGross; Safari · Gross weight
Single sourceMaximum; CP-140 Aurora · Maximum speed · Maximum speed
Single sourceMaximum; CP-140 · below cruise ceiling
Single source375 kn (432 mph, 694 km/h) below cruise ceiling[source]
750 km/h[source]CP-140 Aurora · Maximum speed
Cruise; Safari · Cruise speed
Single sourceMaximum; Safari · at sea level
Single sourceCP-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]
Safari · 1 × Lycoming IO-360-A1B6 air-cooled flat-four piston engine
Single source1 × Lycoming IO-360-A1B6 air-cooled flat-four piston engine, 150 kW (200 hp)[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]
Safari · 807 ft/min
Single source4.10 m/s (807 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built |
|---|
21 (18 CP-140M + 3 CP-140A)[source] |
462[source] |
| Introduction date | 1980[source] | 1972[source] |
|---|
| First flight | 22 March 1979 (CP-140)[source] | 26 February 1971[source] |
|---|
| Retired | 2011 (CP-140A only)[source] | — |
|---|
| Developed from | Lockheed P-3 Orion[source] | Malmö MFI-9 Junior[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] | 190 L (42 imp gal; 50 US gal)[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] | 2-bladed Hartzell HC-C2YK-4F/FC7666A-2 constant speed propeller[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] | — |
|---|
| Designer | — | Malmö Flygindustri[source] |
|---|
| Primary users | — | Danish Air Force Royal Norwegian Air Force Pakistan Air Force[source] |
|---|
| Manufactured | — | 1971–1979[source] |
|---|
| Variant | — | PAC MFI-17 Mushshak[source] |
|---|
| Capacity | — | 1 passenger[source] |
|---|
| Stall speed | — | 107 km/h (66 mph, 58 kn) flaps down, power off[source] |
|---|
| Never exceed speed | — | 365 km/h (227 mph, 197 kn)[source] |
|---|
| Take-off run to 15 m (50 ft) | — | 385 m (1,263 ft)[source] |
|---|
| Landing run from 15 m (50 ft) | — | 390 m (1,280 ft)[source] |
|---|