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BTrainer aircraft
Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)
At a glance
Measured figures
T-7 · Length
Single source8.59 m (28 ft 2 in)[source]
CP-140 Aurora · Length
Single sourceConfiguration
| Specification | Fuji T-7 | Lockheed CP-140 Aurora |
|---|---|---|
| Type | Primary/Basic Trainer[source] | Maritime patrol aircraft (CP-140) MPA trainer aircraft (CP-140A)[source] |
| National origin | Japan[source] | — |
| Manufacturer | Fuji Heavy Industries[source] | Lockheed Corporation[source] |
| Status | Active[source] | Active (CP-140M only)[source] |
CP-140 · Length
Single sourceMaximum take-off; T-7 · Max takeoff weight
Single source1,585 kg (3,494 lb)[source]
Cruise; T-7 · at 915 m (3,002 ft)
Single source298 km/h (185 mph, 161 kn) at 915 m (3,002 ft)[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.
| Primary user |
|---|
Japan Air Self-Defense Force[source] |
Royal Canadian Air Force[source] |
| Number built | 49[source] | 21 (18 CP-140M + 3 CP-140A)[source] |
|---|
| Manufactured | 2002-present[source] | — |
|---|
| Developed from | Fuji T-3[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, 2.12 m (6 ft 11 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 | 104 km/h (65 mph, 56 kn) flaps and gear down[source] | — |
|---|
| Wing loading | 96.1 kg/m 2 (19.7 lb/sq ft)[source] | — |
|---|
| Power/mass | 0.2114 kW/kg (0.1286 hp/lb)[source] | — |
|---|
| Take-off distance to 15 m (49 ft) | 608 m (1,995 ft)[source] | — |
|---|
| Landing distance from 15 m (49 ft) | 566 m (1,857 ft)[source] | — |
|---|
| Introduction date | — | 1980[source] |
|---|
| First flight | — | 22 March 1979 (CP-140)[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] |
|---|