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Barracuda Jeffair Aircraft Plans 200mph Retract Tri-gear2 Pl.44gal31pages24x36" on 2040-parts.com

US $179.00
Location:

Prescott Valley, Arizona, United States

Prescott Valley, Arizona, United States
BARRACUDA JEFFAIR Aircraft PLANS 200MPH RETRACT TRI-GEAR2 PL.44GAL31pages24X36", US $179.00, image 1
“The plans are in clean clear, unused condition BUT WITH A FEW TEARS ON THE EDGES.”
Warranty:No Compatible Make:THORP Country/Region of Manufacture:United States Compatible Model:T- 18

This auction is for BARRACUDA JEFFAIR 200MPH CRUISE, HIGH PERFORMANCE Aircraft PLANS,31 pages 24X36"  options for quick-build.are available at AIRCRAFT SPRUCE AND WICKS AIRCRAFT PARTS...

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STANDARD DATA: Gross wt. 2,200. Empty wt. 1,495. Fuel capacity 44. Wingspan 24'9". Length 21'6". Engine 220-hp Lycoming.
PERFORMANCE: Top mph 218. Cruise mph 200. Stall mph 62. Climb rate 2,200.

The Barracuda is a sophisticated enclosed-cabin two-seater in the image of the Thorp T-18 but with tricycle landing gear, all-wood construction, and a three blade controllable pitch propeller. It was designed by former RAF fighter pilot Geoffrey Siers. The landing gear features electro-hydraulic retraction. The cabin is fitted with dual controls, gull-wing doors, and two armchair- type seats. Siers Flight Systems owns the rights
to the Barracuda.

The Jeffair Barracuda is a high-performance sporting monoplane that was developed in the United States in the 1970s and is marketed for homebuilding. Designed and built by Geoffrey Siers, the prototype won the prize for "Most Outstanding New Design" at the EAA Fly-in in 1976.[1] It was a low-wing cantilever monoplane of wooden construction with retractable tricycle undercarriage and side-by-side seating for two. Around 150 sets of plans had sold by 1977.

Development

Geoffrey Siers was a former RAF pilot and engineer for Boeing in 1967. He set out to design an aircraft that was fast, aerobatic, two place, and had range to fly long cross-country flights. The aircraft was refined after a full size cockpit mockup was made. The lightweight construction of the plywood-covered wooden de Havilland Mosquito was the inspiration for the materials choice. The retractable landing gear came from a Piper PA-24 Comanche. The wings were a three-piece design[2]

Operational history

Test flights were performed in 1975. The aircraft takes off at 70 mph (113 km/h) and climbs at 2000 feet per minute (10.2 m/s). Full flap stalls were recorded as low as 54 mph (87 km/h).

Specifications[edit]

General characteristics

  • Crew: one pilot
  • Capacity: one passenger
  • Length: 21 ft 6 in (6.55 m)
  • Wingspan: 24 ft 9 in (7.54 m)
  • Wing area: 120 ft2 (11,15 m2)
  • Empty weight: 1,495 lb (678 kg)
  • Gross weight: 2,300 lb (1,043 kg)
  • Powerplant: 1 × Lycoming GO-435-2, 220 hp (164 kW)

Performance

  • Maximum speed: 218 mph (351 km/h)
  • Range: 450 miles (724 km)
  • Rate of climb: 2,200 ft/min (11.2 m/s)




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