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 Development  



1.1  Production  







2 Operational history  





3 Variants  





4 Operators  





5 Surviving aircraft  





6 Specifications (Klemm Kl 35D)  





7 See also  





8 References  





9 Bibliography  














Klemm Kl 35






Čeština
Deutsch
Español
Français
Italiano
Nederlands
Polski
Português
Română
Svenska
Українська
Tiếng Vit
 

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
 




In other projects  



Wikimedia Commons
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 

(Redirected from Klemm Kl 106)

Kl 35
Klemm Kl 35D
Role Two-seat sports and training aircraft
Manufacturer Klemm Leightflugzeugbau Gmbh
Designer Friedrich Fecher
First flight 1935
Introduction 1935
Status out of service
Primary users Luftwaffe
Czechoslovakian Air Force
Royal Hungarian Air Force
Royal Romanian Air Force
Produced 1937-1944
Number built c.2,000?

The Klemm Kl 35 is a German sporting and training aeroplane developed as a successor to the Kl 25. A product of Klemm Leichtflugzeugbau Gmbh it shared the same single-engine, cantilever low-wing configuration as the earlier machine, the major difference being the introduction of an inverted gull wing.

Probably Klemm's most important type,[1] the fully aerobatic aeroplane was shown for the first time publicly in October 1935 at the international Air Show in Milan and soon found many private buyers. Powered initially by an 80 hp (60 kW) Hirth HM60R inline,[1] it had fixed undercarriage,[1] mixed wood and fabric covering,[1] and the choice of open or closed cockpit.[1] Powered by the Hirth 60R, it became the Kl 35A (with floats, Kl 35AW),[1] while with the 105 hp (78 kW) Hirth, it was the Kl 35A (with floats, Kl 35AW).[1]

An improved Kl 35D, designed as a Luftwaffe trainer, with 105 hp (78 kW) Hirth HM 504A-2 engine and the option of ski or float landing gear, appeared in 1938.[1] It was the most numerous, with over three thousand built.[1]

A number of air forces purchased copies, including the Romanian, Hungarian, and Slovak.[1] The Swedish Air Force bought several,[1] designated Sk 15, for training use (at least five of those were seaplanes) and in 1941 began licence production, building about 74 more,[1] with some remaining in service until 1951.[1] The Lithuanian air force flew three.[1]

Development

[edit]

The Kl 35 was designed in 1934 under the auspices of the Reichsluftfahrtministerium (RLM). Dipl. Ing. Friedrich Fecher had overall responsibility for the construction. The so-called Gemischtbauweise construction was used: steel for fuselage, wood for wings and tail units and only small quantities of light alloy for linings were used. This became a preferred building method with the RLM around this time, because from considerations of strategic material availability.

Production

[edit]

Klemm suffered a setback in 1935 when the prototype Kl 35 crashed during testing at Rechlin. The results of further trial must have been satisfactory, because in July 1936, 23 aircraft were ordered for delivery between July and September 1937, with production planned to increase to 3 per month. Klemm was at the time manufacturing the Fw 44 under licence from Focke-Wulf.

By this time the RLM was already looking for a sub-contractor to build the Kl 35A under licence, choosing Fieseler which was already undertaking licence production of the He 72 and Fw 58 alongside Storchs at its Kasseler plant.

Further orders, to a total of 1,386, followed and new variants came on line, beginning with the Kl 35B with a new engine.

Manufacture at Fieseler ceased in November 1939, after 365 aircraft, when the RLM transferred licence production to Zlin in occupied Czechoslovakia.

Production ended in May 1943 with total production for the Luftwaffe having reached 1,302. The balance of production was for private and export customers, though since these would have to number nearly 700 to reach the oft-quoted total of around 2,000 this may be exaggerated.

Operational history

[edit]

Variants

[edit]
Kl 35a
The first prototype, powered by a 60-kW (80-hp) Hirth HM60R piston engine.
Kl 35b
Second prototype.
Kl 35A
Initial production version, powered by a 60-kW (80-hp) Hirth HM60R piston engine
Kl 35B
Version, powered by an 80-kW (105-hp) Hirth HM 504 A2 piston engine. Covered single-strut landing gear
Kl 35BW
Floatplane version.
KL 35C
Version with wooden fuselage soon renamed as Kl 106, intended for production under licence in the United States, just one built
Kl 35D
Improved version with triangle landing gear.
Kl 35E
Version powered by an improved 80-kW (105-hp) Hirth HM 500 engine
Sk 15
Swedish military designation for the Kl 35D.

Operators

[edit]
 Czechoslovakia
 Germany
 Hungary
 Lithuania
 Slovakia
 Romania
 Spain
 Sweden

Surviving aircraft

[edit]
Klemm Kl35

No Luftwaffe machine is known to survive, but a number of ex-Flygvapnet machines have been preserved.

Specifications (Klemm Kl 35D)

[edit]

Data from The Concise Guide to Axis Aircraft of World War II[5]

General characteristics

Performance

See also

[edit]

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]
  1. ^ a b c d e f g h i j k l m n Ketley, Barry, and Rolfe, Mark. Luftwaffe Fledglings 1935-1945: Luftwaffe Training Units and their Aircraft (Aldershot, GB: Hikoki Publications, 1996), p.12.
  • ^ "Klemm 35 D "D-EQXD" | QUAX-Flieger". Archived from the original on 2013-10-21. Retrieved 2013-08-16.
  • ^ Klemm Kl 35 start up
  • ^ Sterntakt
  • ^ Mondey1996, p.149-150
  • ^ Smith and Kay 1990, p. 461.
  • Bibliography

    [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Klemm_Kl_35&oldid=1210514440"

    Categories: 
    Klemm aircraft
    Inverted gull-wing aircraft
    1930s German sport aircraft
    Aerobatic aircraft
    Single-engined tractor aircraft
    Low-wing aircraft
    Aircraft first flown in 1935
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
    Articles to be expanded from May 2017
    All articles to be expanded
    Articles using small message boxes
    Commons category link is on Wikidata
     



    This page was last edited on 27 February 2024, at 00:39 (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