Credit
Rob Schleiffert from Holland · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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BTrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
T-5 · Length
Single source8.4 m (27 ft 7 in)[source]
CP-140 Aurora · Length
Single sourceConfiguration
| Specification | Fuji T-5 | Lockheed CP-140 Aurora |
|---|---|---|
| Type | Basic trainer[source] | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] |
| Manufacturer | Fuji Heavy Industries[source] | Lockheed Corporation[source] |
| Primary user | Japan Maritime Self-Defense Force[source] | Royal Canadian Air Force[source] |
| Introduction date | 1988[source] | 1980 |
CP-140 · Length
Single sourceCruise; T-5 · Cruise speed
Single sourceMaximum; T-5 · at 2,440 m (8,005 ft)
Single source357 km/h (222 mph, 193 kn) at 2,440 m (8,005 ft)[source]
287 km/h (178 mph, 155 kn)[source]
Maximum; CP-140 Aurora · Maximum speed · Maximum speed
Single sourceMaximum; CP-140 · below cruise ceiling
Single sourceT-5 · 1,690 ft/min
Single source8.6 m/s (1,690 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.
| First flight | 28 June 1984[source] | 22 March 1979 (CP-140)[source] |
|---|
| Developed from | Fuji KM-2[source] | Lockheed P-3 Orion[source] |
|---|
| Airfoil | root: NACA 23016.5 ; tip: NACA 23012[source] | root: NACA 0014 (modified) ; tip: NACA 0012 (modified)[source] |
|---|
| Propellers | 3-bladed constant-speed propeller[source] | 4-bladed Hamilton Standard 54H60, 13 ft 6 in (4.11 m) diameter constant-speed fully-feathering reversible-pitch propellers[source] |
|---|
| Stall speed | 104 km/h (65 mph, 56 kn)[source] | — |
|---|
| Never exceed speed | 413 km/h (257 mph, 223 kn)[source] | — |
|---|
| National origin | Japan[source] | — |
|---|
| Status | — | Active (CP-140M only)[source] |
|---|
| Number built | — | 21 (18 CP-140M + 3 CP-140A)[source] |
|---|
| Retired | — | 2011 (CP-140A only)[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] |
|---|
| 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] |
|---|