Potez 58

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Pibwl (talk | contribs) at 21:30, 29 June 2007 (Created page with '<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. -->{{infobox A...'). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)

Template:Infobox Aircraft

The Potez 58 was a family of French light utility and touring aircraft, developed in mid-1930s. They were three-seat single-engine high wing monoplanes.

Design and development

The plane was a further development of Potez 43 family, tracing its roots from Potez 36. An airframe changed little from Potez 43, main difference were stronger engines. A prototype Potez 58 first flew on 7 March 1934. In September 1934 the first serial variant Potez 580 was flown, powered with 120 hp radial engine Potez 6B. There were built 80 of this variant. An air ambulance variant was also evaluated.

There were next built several small-series variants, differing with the last digit in designation. The second variant built in a significant series was Potez 585 - 108 built, of which 99 served in the French Air Force as liaison aircraft.

Variants

  • Potez 58 - prototype.
  • Potez 580 - first series variant of 1934, 120 hp Potez 6B engine, 80 built.
  • Potez 582 ?
  • Potez 584 - variant with 120 hp de Havilland Gipsy Major I straight engine, 4 built in 1935.
  • Potez 585 - liaison and utility aircraft, 130 hp Potez 6Ba engine, 108 built.
  • Potez 586 - four-seater variant, 10 built in 1936-1937.

Specifications (Potez 585)

Mixed construction strutted high-wing monoplane. Rectangular two-spar wing, with rounded ends, supported with V-shaped spars. Wings were equipped with slats on 1/3 span. Closed cabin with three seats. Radial engine in front, with a Townend ring, two-blade propeller. Conventional fixed landing gear, with a rear skid, wheels in teardrop covers.

General characteristics

  • Crew: 1
  • Capacity: 2 passengers

Performance

References

External links

Related content

Related development

Aircraft of comparable role, configuration, and era