FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
BTrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
Length
Single source8.05 m (26 ft 5 in)[source]
CP-140 Aurora · Length
Single sourceConfiguration
| Specification | Aeromot AMT-200 Super Ximango | Lockheed CP-140 Aurora |
|---|---|---|
| Type | Motor glider[source] | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] |
| National origin | Brazil[source] | — |
| Manufacturer | Aeromot[source] | Lockheed Corporation[source] |
| Designer | René Fournier[source] | — |
| Number built |
CP-140 · Length
Single source350 ft/min
Single source1.8 m/s (350 ft/min)[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.
126 (2009)[source] |
21 (18 CP-140M + 3 CP-140A)[source] |
| Introduction date | 1993[source] | 1980[source] |
|---|
| Developed from | AMT-100 Ximango[source] | Lockheed P-3 Orion[source] |
|---|
| Aspect ratio | 16[source] | 7.5[source] |
|---|
| Airfoil | NACA 64 3 -618[source] | root: NACA 0014 (modified) ; tip: NACA 0012 (modified)[source] |
|---|
| Fuel capacity | 90 L (24 US gal; 20 imp gal)[source] | 7,661 imp gal (9,200 US gal; 34,828 L) usable fuel in one fuselage tank and four wing integral tanks[source] |
|---|
| Propellers | 2-bladed Hoffmann HO-V62R/170FA , 1.70 m (5 ft 7 in) diameter[source] | 4-bladed Hamilton Standard 54H60, 13 ft 6 in (4.11 m) diameter constant-speed fully-feathering reversible-pitch propellers[source] |
|---|
| Stall speed | 76 km/h (47 mph, 41 kn)[source] | — |
|---|
| Never exceed speed | 245 km/h (152 mph, 132 kn)[source] | — |
|---|
| Maximum glide ratio | 31[source] | — |
|---|
| Rate of sink | .93 m/s (183 ft/min)[source] | — |
|---|
| Wing loading | 45.3 kg/m 2 (9.3 lb/sq ft)[source] | — |
|---|
| Status | — | Active (CP-140M only)[source] |
|---|
| Primary user | — | Royal Canadian Air Force[source] |
|---|
| First flight | — | 22 March 1979 (CP-140)[source] |
|---|
| Retired | — | 2011 (CP-140A only)[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] |
|---|
| 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] |
|---|