Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Design and development  





2 Operational history  





3 Variants  





4 Specifications (tandem dual control, landplane)  





5 References  














CNA Eta






Тоҷикӣ
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Eta
Role One/two seat light aircraft
National origin Italy
Manufacturer Compagnia Nazionale Aeronautica (CNA)
First flight 1933
Number built 1 or 2

The CNA Eta was a single engine Italian light aircraft, flown in the mid-1930s, that set one and two seat world records as both a landplane and a seaplane. Only one or two were built.

Design and development[edit]

During the 1920s the Compagnia Nazionale Aeronautica (CNA) were best known for their flying school in Rome, though they also manufactured experimental aircraft for the government. When they moved their Roman base from CerveteritoLittorio in 1928, they built a factory in which they could produce both aircraft and aircraft engines; some were designed by other companies, some by themselves. The Eta was both CNA designed and powered.[1]

The Eta was a conventional parasol wing light aircraft that could be configured as a single seater or with two seats in tandem; it could also be fitted with either a fixed conventional undercarriage or floats. It was originally powered by an uncowled, 9-cylinder CNA C-7 supercharged radial engine but later flew with an inverted 6-cylinder air-cooled supercharged inline, the CNA C.VI. The slightly tapered wing was mounted on tall faired parallel struts from the mid-fuselage, assisted by lighter diagonal struts and shorter, forward leaning supports from the upper fuselage. The single seat model placed the open cockpit just behind the wing trailing edge. The tail was conventional, with the tailplane on top of the fuselage and braced from below. The vertical surfaces were rounded. In keeping with the rest of the design, the fixed wheeled undercarriage was very simple, with unfaired wheels mounted on slender V-form struts attached to the lower fuselage.[1]

Operational history[edit]

The Eta was chiefly distinguished by setting three lightplane world records. At the time the FAI divided the lightest aircraft between to categories: C.II, single seats with empty weights less than 200 kg (41 lb) and C.I, two seaters weighing less than 400 kg (882 lb). These categories were then each sub-divided into landplane and seaplane.[2] A 130 kW (170 hp) CNA C-7 engine had enabled a Fiat AS.1 to gain the Category I altitude record in December 1932 and on 6 November 1933 the single seat Eta, with the same motor and fitted with floats, set a new C.II record of 8,411 m (27.595 ft). It was then fitted with its wheeled undercarriage and flown to a new C.II landplane record of 10,008 m (32,835 ft) in December 1933. On both occasions the Eta was flown by Furio Niclot Doglio.[3]

By 1936 the Eta was flying as a two-seat seaplane, powered by the in-line, 112 kW (150 hp) CNA C-VI engine and on 15 May it set a new world C.I 100 km (62 mi) circuit speed record of 192.62 km/h (119.7 mph), flown by Gian Giacomo Chiesi with Domenico Rossetti.[3]

Variants[edit]

It is not known if these were different aircraft or the same one modified.

Category II
single seat, CNA C-7 engine, both landplane and seaplane.
Category I
two seat, CNA C.VI engine, both landplane seaplane.

Specifications (tandem dual control, landplane)[edit]

Data from Italian Civil and Military Aircraft 1930-1945[1]

General characteristics

Performance

References[edit]

  1. ^ a b c Thompson, Jonathan (1963). Italian Civil and Military Aircraft 1930-1945. Fallbrook, California: Aero Publishers, Inc. pp. 131–2.
  • ^ "WORLD'S RECORDS FOR LIGHT 'PLANES". Flight. 31 March 1927. p. 189.
  • ^ a b "FAI records". Archived from the original on 11 June 2007. Retrieved 20 March 2012.
  • Companies
  • Aviation

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=CNA_Eta&oldid=1132208874"

    Categories: 
    1930s Italian sport aircraft
    Compagnia Nazionale Aeronautica
    Parasol-wing aircraft
    Single-engined tractor aircraft
    Aircraft first flown in 1933
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
    Aircraft specs templates using more performance parameter
     



    This page was last edited on 7 January 2023, at 19:52 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki