PIPER PA-44 “SEMINOLE”€/ “TURBO SEMINOLE”€

1978’€“ Present

Gemini Sparkle

Key Takeaways:

  • The Piper Seminole, a dominant light-twin aircraft, incorporated design elements from other Piper models like the Arrow III, notably being the first aircraft to develop the T-tail, and utilizes counter-rotating propellers for balanced thrust.
  • Intended as an inexpensive alternative to high-performance singles, the standard Seminole boasts a cruise speed of 191 mph and a range of 898 miles.
  • A turbocharged version was introduced in 1980, offering improved performance, and although production ceased in 1990 due to financial issues, it resumed in 1995 by New Piper Aircraft as their only remaining T-tail model.
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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. Takeoff distance (50′) 1,400. Landing distance (50′) 1,190.

STANDARD DATA: (Turbo) Seats 4. Gross wt. 3,925. Empty wt. 2,430. Fuel capacity 110. Engines two 180-hp turbocharged Lycomings.
PERFORMANCE: Top mph 224. Cruise mph 211. Stall mph 64. Initial climb rate 1,290. Ceiling 20,000+. Range 903. Takeoff distance (50′) 1,500. Landing distance (50′) 1,190.

In the light-twin field, Piper has always dominated the industry with the Apache, Twin Comanche, and Senecas. While the Seminole was more than a simple homogenization of existing Piper components, it did borrow most of its fuselage from the Arrow III, from what would be the forward firewall to the aft cabin bulkhead. The T-tail was actually developed on the Seminole first, but introduced on the Lance II. The wings are basically beefed-up versions of the semi-tapered Arrow III to within four feet of the tip. Like the Seneca II and the Navajo C/R, the Seminole uses counter-rotating propellers for balanced thrust, and optional three-blade propellers in 1979 provided a quieter ride. Also in the same year, a propeller synchrophaser further reduced cabin noise levels.

Two 54-gallon fuel tanks are fitted in the engine nacelles. At 75% power and 7,000 feet, the Seminole cruises at 191 mph. When leaned to 65%, best-economy power cruise speed is 181 mph, and range is 898 miles with a 45-minute reserve. At 3,800 pounds gross, the Seminole weighs the same as Gulfstream American’s Cougar, which flies between a pair of 160-hp engines; thus, each Seminole horsepower must heft only 10.6 pounds compared to the Cougar’s 11.9 pounds/hp loading. From the beginning, Piper intended the Seminole as a relatively inexpensive alternative to high-performance singles.

In the middle of 1980, Piper introduced a turbocharged version of the Seminole powered by twin Lycoming TO-360 counter-rotating engines. At 65-percent power economy cruise, the Turbo Seminole can travel at 194 mph over a distance of 920 miles burning fuel at a rate of 19 gph. Standard equipment includes a built-in oxygen system that consists of a rear-mounted bottle with easy-to-reach overhead outlets, night-lighted pressure gauge, oxygen masks, and a control-wheel mike button. Piper’s financial troubles brought Seminole production to an end in 1990. Five years later, New Piper Aircraft resumed making the entry-level twin, the only remaining T-tail aircraft in the line.

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