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Sunday, 1 September 2013

Piper PA-44 Seminole Four-Seater Light Twin Aircraft



Piper PA-44 Seminole

PA. 44 180 Poh
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PA. 44 180
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Piper PA 44 180 Seminole
PA-44 Seminole




Trainer / Touring Aircraft

The Piper PA-44 Seminole is a twin-engined four-seat trainer and touring aircraft with retractable landing gear produced by the US-American manufacturer Piper Aircraft Corporation, later New Piper Aircraft and today Piper Aircraft, Inc..




Crew 1 / 2
Passengers 3 /4 

Propulsion 2 Piston Engines
Engine Model Lycoming O- / LO-360-A1H6
Engine Power (each) 134 kW 180 hp

max. Cruise Speed 300 km/h 169 kts
  194 mph
max. Speed (vne) 374 km/h 202 kts
  232 mph
Service Ceiling 15.000 m 49.212 ft
Range 1.630 km 880 NM
1.013 mi.

Empty Weight 1.071 kg 2.360 lbs
max. Takeoff Weight 1.724 kg 3.800 lbs
max. Landing Weight 1.724 kg 3.800 lbs

Wing Span 11,77 m 38,6 ft
Wing Area 17,1 m² 184 ft²
Length 8,41 m 27,6 ft
Height 2,59 m 8,5 ft






First Flight 05/1976
Production Status in production
Developed from Piper PA-28 Cherokee





ICAO Code PA44
FAA TCDS A19SO
Data for (Version) Piper PA-44-180 Seminole
Variants Piper PA-44-180, PA-44-180T
Remarks
The Piper PA-44 is a twin-engine development of the Piper PA-28.








1 comment:

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