Piper PA-44 Seminole
Summary
| Category | Training aircraft |
| Origin country | 🇺🇸 United States |
| First flight | 1 January 1976 |
| Year of introduction | 1979 |
| Number produced | 926 units |
| Average unit price | $0.6 million |
Description
The Piper PA-44 Seminole is a twin-engine light aircraft primarily developed for military purposes. It was initially introduced in the late 1970s and has since been deployed in various military aviation units around the world. The Seminole has a low-wing design and a fixed tricycle landing gear configuration. It is equipped with two Lycoming O-360 four-cylinder engines, providing a reliable power source for training missions and multi-engine operations. With its robust construction and advanced avionics, the Seminole offers a versatile platform for military training exercises, flight instruction, and navigation proficiency. Its deployment spans across different military branches, aiding in the development of pilots' skills and enhancing operational readiness.
Technical specifications
| Version: PA-44 Seminole | |
|---|---|
| Crew | 1 pilot + 3 passengers |
| Operational range | 1695 km (1053 mi) |
| Maximum speed | 311 km/h (193 mph) |
| Wing area | 17.1 m² (183.8 sqft) |
| Wingspan | 11.8 m (38.6 ft) |
| Height | 2.6 m (8.5 ft) |
| Length | 8.4 m (27.6 ft) |
| Service ceiling | 5200 m (17060 ft) |
| Empty weight | 1068 kg (2355 lbs) |
| Max. takeoff weight | 1724 kg (3801 lbs) |
| Powerplant | 2 × Lycoming O-360-E1A6 air-cooled flat four delivering 180 hp (130 kW) |
Current operating countries
| Country | Units | ||
|---|---|---|---|
|
Peru | 1 | |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.