Fletcher Hercules

Source: Wikipedia, the free encyclopedia.

Hercules
Role Ultralight trike
National origin United States
Manufacturer Fletcher's Ultralights
Designer AW Harrison
Status Production completed
Number built 25 (February 2000)

The Fletcher Hercules is an American two-seat ultralight trike that was designed by AW Harrison and produced by Fletcher's Ultralights of Turlock, California, in the late 1990s and early 2000s. The aircraft was supplied as a kit for amateur construction and was also available as a completed aircraft.[1][2][3]

Design and development

The Hercules was designed as a lightweight single-seat aircraft, with a second seat available to carry an instructor or passenger when required. Because it was intended to be flown solo most of the time it came factory-supplied with a relatively low powered engine, to reduce both the aircraft's cost and weight. Higher powered engines were available if the aircraft was to be used in the training role on a regular basis.[1]

In writing about the Hercules, reviewer Andre Cliche explained the engine choice, "Because most people usually fly alone in their two-seater, it makes for a well balanced single seater with peppy performance, low fuel burn and longer range. However, when comes the time to carry an occasional passenger, its two-seater capacity far outweighs its anemic performance with two people aboard. This is a smart compromise that gives the best of both worlds."[1]

The Hercules was designed to comply with the US

high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, tricycle landing gear and a single engine in pusher configuration.[1][3]

The aircraft is made from bolted-together

The aircraft has an acceptable installed power range of 35 to 80 hp (26 to 60 kW). The standard engine supplied was the twin cylinder

Due to its off-airport capabilities the Hercules was nicknamed "the jeep of trikes". It is noted for its ease of set-up and repair. Twenty-five had been completed and flown by February 2000.[2]

Variants

Hercules Cruiser
Version marketed circa 1998 with 35 hp (26 kW)
Cuyuna UL II-02 engine[3]
Hercules Cross Country
Version marketed circa 1998 with 50 hp (37 kW) Rotax 503 engine[3]

Specifications (version)

Data from Cliche and Kitplanes[1][2]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 9 ft (2.7 m)
  • Wingspan: 34 ft (10 m)
  • Height: 10 ft (3.0 m)
  • Wing area: 190 sq ft (18 m2)
  • Empty weight: 254 lb (115 kg)
  • Gross weight: 600 lb (272 kg)
  • Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  • Powerplant: 1 ×
    two-stroke
    , 35 hp (26 kW)

Performance

  • Cruise speed: 40 mph (64 km/h, 35 kn)
  • Stall speed: 28 mph (45 km/h, 24 kn)
  • Range: 85 mi (137 km, 74 nmi)
  • Service ceiling: 12,000 ft (3,700 m)
  • Rate of climb: 400 ft/min (2.0 m/s)

References

  1. ^
  2. ^ a b c d e Downey, Julia: 2000 Trike and 'Chute Directory, Kitplanes, Volume 17, Number 2, February 2000, page 45. Kitplanes Acquisition Company. ISSN 0891-1851
  3. ^