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Contents

   



(Top)
 


1 Variants  





2 Specifications  





3 References  





4 External links  














Pitcairn PAA-1






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From Wikipedia, the free encyclopedia
 


PAA-1
This Pitcairn PAA-1 autogiro was flown at Langley for the NACA investigation of an experimental cantilevered three-bladed rotor. June 1943.
Role Sport autogyro
National origin United States
Manufacturer Pitcairn-Cierva Autogiro Company
First flight 1931
Number built 25

The Pitcairn PAA-1 was an autogyro developed in the United States in the early 1930s.[1] Of similar configuration to Pitcairn's earlier machines, the PAA-1 had an airplane-like fuselage with two open cockpits in tandem and a tractor-mounted engine in the nose.[2] It was also equipped with small wings, which carried control surfaces, rather than using the rotor for flight control.[2] It was a smaller and lighter machine than its predecessors and was designed specifically with private pilots in mind.[1][2]

Variants[edit]


Specifications[edit]

Data from "Pitcairn, A G A, Pitcairn-Cierva, Pitcairn-Larsen"

General characteristics

Performance

References[edit]

Notes
  1. ^ a b Taylor 1989, p.734
  • ^ a b c d e f The Illustrated Encyclopedia of Aircraft, p.2739
  • Bibliography

    External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Pitcairn_PAA-1&oldid=1145178209"

    Categories: 
    1930s United States sport aircraft
    Pitcairn aircraft
    Single-engined tractor autogyros
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Commons category link is on Wikidata
     



    This page was last edited on 17 March 2023, at 17:15 (UTC).

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