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Javelin V6 STOL

From Wikipedia, the free encyclopedia
American homebuilt STOL aircraft

V6 STOL
RoleHomebuilt aircraft
Type of aircraft
National originUnited States
ManufacturerJavelin Aircraft
StatusProduction completed
Number builtAt least 25
Developed fromPiper PA-20 Pacer

TheJavelin V6 STOL is an AmericanSTOLhomebuilt aircraft that was designed and produced byJavelin Aircraft ofWichita, Kansas. When it was available the aircraft was supplied in the form of plans for amateur construction.[1]

Design and development

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The V6 STOL consists of plans to power an existingcertifiedPiper PA-20 Pacerairframe with aFord Motor Company V6 engine and moving it from theCertified Category to theExperimental Amateur-built category.[1]

The aircraft features astrut-bracedhigh wing, a four-seat enclosed cabin accessed via doors, fixedconventional landing gear and a single engine intractor configuration.[1]

Since it uses a standard Piper Pacer airframe, the aircraft is made from welded steel tubing, covered indopedaircraft fabric. Its 32.00 ft (9.8 m) span wing employs a USA 35Bairfoil, mountsflaps and has a wing area of 168.00 sq ft (15.608 m2). The standard conversion installs a 230 hp (172 kW) Ford V6 powerplant, driving a fixed pitch propeller, although engines of up to 300 hp (224 kW) can be employed. The 230 hp (172 kW) engine gives the aircraft a sea level, standard day takeoff distance of 150 ft (46 m) and a landing distance of 300 ft (91 m).[1][2]

The V6 STOL has a typical empty weight of 1,200 lb (540 kg) and a gross weight of 2,200 lb (1,000 kg), giving a useful load of 1,000 lb (450 kg). With full fuel of 36 U.S. gallons (140 L; 30 imp gal) the payload for pilot, passengers and baggage is 784 lb (356 kg).[1]

The manufacturer estimates the time to complete the conversion from the supplied plans as 400 hours.[1]

Operational history

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In January 2014, 14 examples wereregistered in the United States with theFederal Aviation Administration, but a total of 25 had been registered at one time.[3][4]

Specifications (V6 STOL)

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Data from AeroCrafter and The Incomplete Guide to Airfoil Usage[1][2]

General characteristics

  • Crew: one
  • Capacity: three passengers
  • Length: 22 ft 3 in (6.78 m)
  • Wingspan: 32 ft 0 in (9.75 m)
  • Wing area: 168.00 sq ft (15.608 m2)
  • Airfoil: USA 35B
  • Empty weight: 1,200 lb (544 kg)
  • Gross weight: 2,200 lb (998 kg)
  • Fuel capacity: 36 U.S. gallons (140 L; 30 imp gal)
  • Powerplant: 1 ×Ford Motor Company V6 six cylinder, liquid-cooled,four stroke automotive conversion engine, 230 hp (170 kW)
  • Propellers: 2-bladed fixed pitch

Performance

  • Maximum speed: 140 mph (230 km/h, 120 kn)
  • Cruise speed: 130 mph (210 km/h, 110 kn)
  • Stall speed: 52 mph (84 km/h, 45 kn)
  • Range: 700 mi (1,100 km, 610 nmi)
  • Service ceiling: 18,000 ft (5,500 m)
  • Rate of climb: 1,800 ft/min (9.1 m/s)
  • Wing loading: 13.1 lb/sq ft (64 kg/m2)

References

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  1. ^abcdefgPurdy, Don:AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 182. BAI Communications, 15 July 1998.ISBN 0-9636409-4-1
  2. ^abLednicer, David (2010)."The Incomplete Guide to Airfoil Usage". Archived fromthe original on April 20, 2010. RetrievedJanuary 5, 2014.
  3. ^Federal Aviation Administration (January 5, 2014)."Make / Model Inquiry Results". Archived fromthe original on January 6, 2014. RetrievedJanuary 5, 2014.
  4. ^Federal Aviation Administration (January 5, 2014)."N-Number Inquiry Results". Archived fromthe original on March 5, 2016. RetrievedJanuary 5, 2014.

External links

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Javelin aircraft
Homebuilt aircraft
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