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Piper PA-44 Seminole

The Seminole is a four-seat, low-wing twin with two 180 hp Lycoming engines, retractable landing gear and a T-tail, which flight schools use for multi-engine training. This page covers the PA-44-180, approved by the FAA in 1978, and the turbocharged PA-44-180T. The figures are the PA-44-180's: span, length and height from the EASA data sheet, a maximum weight of 3,800 pounds, 108 US gallons usable, and the maximum cruise speed of 162 knots true airspeed that Piper gives. The ICAO code is PA44.

Cruise speed
162 knots (300 km/h)
Seats
About 4
Engines
Two piston engines on the wings: Lycoming O-360-E1A6D and LO-360-E1A6D; IO-360-B1G6 on current aircraft
Max takeoff weight
3,800 lb (1,724 kg)
Piper PA-44 Seminole
Photo: Gons, CC BY-SA 4.0
Piper PA-44 Seminole seen from above: length 27 ft 7 in (8.41 m), wingspan 38 ft 7 in (11.75 m)
Drawing: cwsi.net, from published dimensions (a schematic, not to exact detail)

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Specifications

Length27 ft 7 in (8.41 m)
Wingspan38 ft 7 in (11.75 m)
Height8 ft 6 in (2.59 m)
Fuselage width3 ft 11 in (1.20 m)
Fuel capacity110 US gal (408 L)
StatusIn service
Type codesICAO PA44

Private aircraft show specs only. No flight data is shown for them.

Sources