Overview
Piper PA-44 Seminole — twin-engine training aircraftThe Seminole first flew in 1976 and entered service in 1978. It featured a low-wing configuration and fixed landing gear in early versions. The design focused on safety and controllability.Two Lycoming piston engines producing approximately 180 horsepower each powered the aircraft. Cruise speed approached 160 knots (296 km/h). Maximum takeoff weight exceeded 3,800 pounds (1,724 kg).The PA-44 became widely adopted for multiengine training programs. Its balanced handling characteristics made it suitable for instructional environments. Production continues in updated forms.
Live Fleet Activity (PA44)
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Specifications
- Engine
- 2 × Lycoming L/O 360 A1H6/ E1A6
- Engine type
- Piston
- Power
- 2 × 180 hp · 134 kW
- Avionics
- GARMIN G1000® NXI
- Wing tips
- No winglets
- Seats
- 4
- Crew
- —
- Cabin width
- 3 ft 5 in · 1.05 m
- Cabin height
- 3 ft 11 in · 1.20 m
- Cabin length
- 7 ft 3 in · 2.20 m
- Exterior length
- 27 ft 7 in · 8.40 m
- Tail height
- 8 ft 6 in · 2.60 m
- Fuselage diameter
- 3 ft 9 in · 1.15 m
- Wing span
- 38 ft 9 in · 11.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 3,800 lb · 1,700 kg
- Max landing weight
- 3,800 lb · 1,700 kg
- Max payload
- 1,200 lb · 550 kg
- Fuel capacity
- 110 gal · 400 L · 300 kg (AvGas)
- Max cruise speed
- 162 kt · 186 mph · 300 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 55 kt · 63 mph · 102 km/h
- Range
- 700 nm · 810 mi · 1,300 km
- Fuel burn
- 16.77 nm/gal · 8.20 km/L
- Ceiling
- 15,000 ft · 4,600 m
- Rate of climb
- 1,340 ft/min · 7 m/s
- Takeoff distance
- 2,200 ft · 670 m
- Landing distance
- 1,490 ft · 450 m
Gallery