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-engined development of the Piper Cherokee single-engined aircraft, primarily intended for multi-engine flight training. The first prototype Seminole took flight in May 1976, and the design was publicly announced on February 21, 1978. Certification was achieved on March 10, 1978, with the aircraft introduced as a 1979 model in late 1978.
Initial production models featured two 180 hp Lycoming O-360-E1A6D engines; the right-hand engine was a Lycoming LO-360-E1A6D variant, rotating in the opposite direction. This counter-rotating engine configuration eliminates the critical engine, enhancing control during engine shutdown or failure. Later production models utilized Lycoming O-360-A1H6 engines. The PA-44 also incorporates a high T-tail. A turbocharged variant, the PA-44-180T Turbo Seminole, certified on November 29, 1979, included two 180 hp Lycoming TO-360-E1A6D engines to improve performance at high altitudes. The aircraft is equipped with Hartzell fully-feathering metal constant-speed propellers, measuring 6 ft 2 in in diameter.
Production of both versions initially ceased in 1982, with 361 Seminoles and 87 Turbo Seminoles built during this period. Production restarted in 1988 with modifications to the electrical systems and instrumentation. Production stopped again in 1990 but resumed in 1995.
The Piper PA-44 Seminole has seen operational use in both civil and military sectors. Its main role is in air charter companies and flight schools, where it serves as a multi-engine trainer. However, it is also operated by private individuals and companies for personal transport. Military operators include the Royal Jordanian Air Force and the Peruvian Air Force.
Main Variants:
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PA-44-180 Seminole: The base model, powered by two Lycoming O-360-E1A6D or two O-360-A1H6 engines.
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PA-44-180T Turbo Seminole: Features two Lycoming TO-360-E1A6D engines with turbochargers for improved high-altitude performance.
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PA-44 Seminole DX: A proposed variant that would have used two Continental Motors CD-170 diesel engines.
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.