Jump to content

Funk F-23

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 178.121.236.184 (talk) at 08:26, 5 February 2016. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Role Agricultural aircraft
Manufacturer Funk
Designer Donald Funk
First flight November 1962
Number built 15

The Funk F-23 was an agricultural aircraft produced in the United States during the 1960s. It was designed by Donald Funk using the fuselage frame of military surplus Fairchild PT-19 trainers as a starting point. The resulting aircraft was a low-wing cantilever monoplane with fixed, tailwheel undercarriage and all-metal construction. The main structural changes were in the wing, which had all-new outer panels. The space occupied by the forward cockpit of the PT-19 was used to accommodate a 200 U.S. gallon (757 litre) hopper for chemicals. Production continued until 1970, when manufacturing rights to the design were purchased by Cosmic Aircraft. The new owner, however, produced no further examples of the type.

Variants

  • F-23 - prototype (1 built)
  • F-23A - production version with Continental W670-M engine (11 built)
  • F-23B - production version with Jacobs R-755 engine (3 built)

Specifications (F-23A)

Data from Jane's All The World's Aircraft 1969–70[1]

General characteristics

  • Crew: One pilot
  • Capacity: 215 US Gallons (814 Litres) of chemicals

Performance

References

  1. ^ Taylor 1969, p. 327.
  • Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 421.
  • Taylor, John W. R. (1969). Jane's All The World's Aircraft 1969–70. London: Sampson Low, Marston & Company. ISBN 0-354-00051-9.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 269.


See also