The Pazmany PL-9 Stork is an American single-engined high-wing monoplane designed by Ladislao Pazmany as a ¾ scale variant of the Second World War Fieseler Storch for the home builder market.[1][2][3][4]

PL-9 Stork
Role Single-engined homebuilt monoplane
National origin United States
Manufacturer Pazmany Aircraft Corporation
Designer Ladislao Pazmany
Status Plans available (2015)

Design and development

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The PL-9 Stork features a strut-braced high-wing, a two-seats-in-tandem enclosed cockpit, fixed conventional landing gear, and a single engine in tractor configuration.[2][3]

The aircraft fuselage is made from welded steel tubing, while the wings are constructed from aluminum sheet. Its 10.97 m (36.0 ft) span wing has an area of 15.44 m2 (166.2 sq ft) and mounts flaps. The standard engine used is the 150 to 160 hp (112 to 119 kW) Lycoming O-320 four-stroke powerplant.[2][3]

Specifications

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Data from Taylor[1]

General characteristics

  • Crew: Tandem
  • Capacity: 2
  • Length: 23 ft 3.5 in (7.4 m)
  • Wingspan: 36 ft 0 in (10.97 m)
  • Empty weight: 1,132 lb (513 kg)
  • Gross weight: 1,673 lb (759 kg)
  • Powerplant: 1 × Lycoming O-320 , 150 hp (112 kW)

Performance

  • Maximum speed: 116 mph (187 km/h, 101 kn)
  • Cruise speed: 95 mph (153 km/h, 83 kn)
  • Range: 332 mi (534 km, 289 nmi)
  • Rate of climb: 1,400 ft/min (7.1 m/s)

See also

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Aircraft of comparable role, configuration, and era

References

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Notes

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  1. ^ a b Taylor 1996, p. 498
  2. ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 114. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  3. ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 121. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  4. ^ Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 355. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1

Bibliography

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Note 2