Piper PA44180 Seminole Untitled Aviation Photo 0559334
PIPER PA-44 "SEMINOLE" / "TURBO SEMINOLE" 1978' Present By Plane and Pilot Updated January 28, 2016 Save Article STANDARD DATA: Seats 4. Gross wt. 3,800. Empty wt. 2,354. Fuel capacity 110. Engines two 180-hp Lycomings. PERFORMANCE: Top mph 193. Cruise mph 191. Stall mph 63. Initial climb rate 1,340. Ceiling 17,100. Range 898.
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The Piper PA-44 Seminole is a twin-engine, low-wing aircraft primarily used for multi-engine flight training, but also has applications in private transporta.
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Piper SEMINOLE PA-44-180 Information Manual Also See for SEMINOLE PA-44-180: Maintenance manual (882 pages) , Pilot operating handbook (344 pages) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28
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Piper PA-44-180 Seminole 1979 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32
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Interestingly the PA-44 is the only T-tail Piper currently in production, even though in the late 1970s most Piper aircraft had been modified to feature a T-tail. Powerplants PA-44-180 - Two 135kW (180hp) Lycoming O-360-E1AD flat four piston engines driving two or optionally three blade constant speed Hartzell propellers.
Piper PA44 Seminole Destination's Journey Aircraft, Aviation
Specifications: Wingspan: 11.75 m (38 ft 6½ in) Length: 8.41 m (27 ft 7 in) Height: 2.59 m (8 ft 6 in) Wing area: 16.72 m² (180 sq ft) Max speed at sea level: 309 km/h (192 mph) Cruising speed: 300 km/h (186 mph) Economical cruising speed: 273 km/h (170 mph) Stalling speed flaps down: 102 km/h (63 mph)
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The Piper PA-44 Seminole is the best twin-engine aircraft for training, which is why Epic Flight Academy purchases new Seminoles for its fleet directly from Piper. We have been training commercial airline pilots since 1999 and have come to rely on the Seminole as the perfect flight training aircraft for multi-engine ratings.
Piper PA44 LFFTO Registration Aircraft Wallpaper 3069
Crew: 1 Passengers: 3 Operating Weights Max T/O Weight: 3800 Lb Max Landing Weight: 3800 Lb Operating Weight: 2825 Lb Fuel Capacity: 648 Lb Payload W/Full Fuel: 327 Lb Max Payload: 975 Lb Range Service Ceiling: 15000 ft Distances Takeoff Distance: 1100 ft Balanced Field Length: 2200 ft Landing Distance: 2147 ft Performance Rate of Climb: 1340 fpm
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The Piper PA-44 Seminole is a four-seat, low-wing, twin-engine light aircraft. It is powered by two 180 horsepower Textron Lycoming O-360-E1A6D reciprocating piston engines. JQF was fitted with three-blade, constant‑speed and full-feathering aluminium propellers. The Seminole is equipped with hydraulically‑operated, retractable, tricycle.
Piper PA44180 Seminole Untitled (Air Carpatia) Aviation Photo
Piper PA-44 Seminole. SPECIFICATIONS Powerplants: (2) Lycoming O-360, counterrotating Seats: 4 Empty weight: 2,354 lb Max takeoff: 3,800 lb Fuel capacity: 110 gal (106 usable) PERFORMANCE Max speed: 168 KTAS Cruise: 162 KTAS (75 percent power) Stall: 55 KIAS (flaps, gear extended) Service ceiling: 17,100 ft .
Piper PA44180T Turbo Seminole Nortavia Aviation Photo 2413544
Serial Number: 44-7995260 Registration #: C-GMEA Total Time: 11,164.8 Number of Seats: 4 Engine 1 Notes: Left Engine 1647.3 SMOH Compressions 76/74/74/73 Right Engine 483.2 SMOH Compressions ?/78/75/. Airframe Notes: 11164.8 TTSN Avionics/Radios: Dual Garmin GNS430 (One WAAS w/Terrain and One Non-WAAS NAV/COM/GPS (#1 Displays on Slaved Compas.
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Light twin aircraft. In service since 1978. Twin engine development of PA-28 Archer with new T-tail and semi-tapered wings. Turbocharged version PA-44-180T since 1980. Production ceased in 1981, restarted in 1988 and ceased once more in 1990. PA-44-180 is back in production since 1995. Licence production by AICSA, Columbia. PA-44-180T: MTOW 1,780 kg.
Piper Aircraft Certifies 1,000 Seminole (PA44) Piper Aircraft
Everypilot's Light Twin: The Piper PA-44 Seminole October 2014- While other light twins have gone away, the PA-44 is still doing what it does so well—safely teaching pilots how to fly twins. I've set my Wayback Machine for Feb. 21, 1978. The place: Dallas, Tex. The event: Piper Aircraft's annual meeting of the North American distributors.
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The PA-44, named the Piper Seminole, was first granted FAA type approval on March 10, 1978 with the first delivery taking place in July 1978. Today the Piper Seminole is known around the world as the leading twin-engine trainer and features fuel injected engines and advanced Garmin G1000 NXi avionics.
Piper PA44180 Seminole Epic Aviation Aviation Photo 1925867
The PA-44 Seminole started life back in 1978 as a four seat twin-engined aircraft built around the well proven PA-28 Cherokee and later Warrior fuselage. The single engine was replaced with a streamlined nose section while the wings were redesigned to mount twin Lycoming O-360 four cylinder engines.
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Specifications Propeller Hartzell Scimitar 2-blade Constant Speed | Full Feathering Fuel Capacity Usable: 108 US Gal | 409 L Engine (2) Lycoming IO-360-B1G6 Flat-Rated Horsepower at 180 hp each Dimensions Wingspan: 38 ft 6 in | 11.8 m Height: 8 ft 5 in | 2.6 m Length: 27 ft 7 in | 8.4 m Avionics Additional Equipment Safety Features Aircraft Design
