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 Variants  





3 Operators  





4 Specifications (AL-60B2)  





5 See also  





6 References  



6.1  Notes  





6.2  Bibliography  







7 External links  














Aermacchi AL-60






Deutsch
Español
فارسی
Français
Hrvatski
Bahasa Indonesia
Italiano
Polski
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
 




In other projects  



Wikimedia Commons
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


LASA-60 / AL-60 / C4M Kudu
Operational Aermacchi AL-60B-2 registered in Germany
Role Utility aircraft
Manufacturer Lockheed Corporation
Designer Al Mooney
Built by Lockheed-Azcarate
Aermacchi
Atlas Aircraft Corporation
First flight 15 September 1959[1]
Status Retired
Primary users Mexican Air Force
South African Air Force
Produced 1974-1979 South Africa
Number built ~180
Variants Northwest Ranger
Lockheed-Azacárate LASA 60

The Aermacchi AL-60 is a light civil utility aircraft of the late 1950s and early 1960s, originally designed by Al MooneyofLockheed in the United States. After the company decided not to build the aircraft in the US, it was manufactured in small quantities in Mexico, and a few were assembled in Argentina (Santa Isabel, Córdoba) by Aviones Lockheed-Kaiser Argentina. It was also built in quantity under licence by Aermacchi in Italy[2] and Atlas Aircraft Corporation in South Africa.

Design and development[edit]

In the late 1950s, the American aircraft designer Al Mooney, who had recently joined Lockheed after leaving the company that bore his name, was given the task of designing a utility aircraft, the CL-402, suitable for use in underdeveloped countries. As Lockheed could not build the design at an economic price in the United States, it was instead intended for the aircraft to be built under licence outside the United States, where labour costs were lower.[3][4] The first prototype CL-402, powered by a 250 hp (190 kW) Continental IO-470-G engine, flew for the first time at Lockheed's Marietta, Georgia on 15 September 1959, with a second prototype, powered by a turbocharged TSIO-470-B engine rated at 260 hp (190 kW) followed a few months later.[3][5]

The initial production deal was made with Mexico, where a joint venture, Lockheed-Azcarate SA (LASA) was set up to build the CL-402 as the LASA-60, with a factory being built near San Luis Potosí.[4] Type certification by the US Federal Aviation Administration was received on 5 April 1960.[6] While it was planned that 240 aircraft would be built by LASA by 1963, the type was less popular than hoped, with LASA stopping production in April 1962.[7] LASA built 41 LASA-60s, with 18 aircraft purchased by the Mexican Air Force.[6]

A second joint venture was set up with Argentina, between Lockheed and Industrias Kaiser Argentina, with the name Aviones Lockheed-Kaiser.[6][8] Production began of a batch of 16 aircraft in 1961, but was stopped after 11 had been completed.[6]

In Italy, Aermacchi purchased a licence to produce the type, first in its original configuration as the AL-60B, then in a modified version for various African customers as the AL-60C. This latter version changed from the original tricycle undercarriage to a taildragger arrangement.

The AL-60C version was built under license by Atlas Aircraft CorporationinSouth Africa. This aircraft was known as Atlas C4M Kudu. Over 40 aircraft were built and served the South African Air Force between 1974 and 1991.

A number of C4M Kudu aircraft are still flying privately and have proven well in the role of skydive release aircraft. They have been re-engined with turbine engines. This design is known as the Atlas Angel or Turbine Kudu.[9][10]

In 1968 Macchi sold the rights to the aircraft to Northwest IndustriesofEdmonton, Alberta, Canada and the design was developed into the Northwest Ranger, with development continuing until 1972.[11]

Variants[edit]

Kaiser-built L-402 at Don Torcuato near Buenos Aires in 1972
An Atlas C4M Kudu at the South African Air Force Museum
CL-402
Lockheed prototypes powered by a turbocharged 260 hp (194 kW) Continental TSIO-470-B engine.[12]
CL-402-2
As CL-402 but powered by a 250 hp (186 kW) Continental IO-470-R engine.[12]
LASA-60
CL-402 and CL-402-2 built by Lockheed-Azcarate in Mexico. 44 built. Production in Argentina by Lockheed-Kaiser was canceled.[12]
AL-60B-1 Santa Maria
Original Aermacchi-built version with tricycle landing gear and powered by a 250 hp (186 kW) Continental IO-470-R engine. Four built.[12]
AL-60B-2 Santa Mari
Production Aermacchi version tricycle landing gear and powered by a turbocharged 260 hp (194 kW) Continental TSIO-470-B. 81 built.[12]
AL-60C-4
Version with conventional landing gear, a separate pilot's door, a larger vertical stabilizer, and powered by a geared 340 hp (254 kW) Lycoming GSO-480-B1 engine. One prototype built.[12]
AL-60C-4M Kudu
Built by Atlas for the South African Air Force with a geared 340 hp (254 kW) Lycoming GSO-480-B1B3 engine. 43 total built; three prototypes and 40 production aircraft.[12]
AL-60C-5 Conestoga
Production version of the AL-60C-4 with a strengthened airframe and powered by a 400 hp (298 kW) Lycoming IO-720-A1A engine. 13 built.[12]
AL-60D-3
As AL-60B-2 but powered by a geared Continental GIO-470-R. One built.[12]
AL-60F-5 Trojan
As AL-60C-5 but with tricycle landing gear. One built.[12]

Operators[edit]

 Central African Republic
 Italy
 Mexico
 Mauritania
 Rhodesia
 South Africa
 Tunisia
 Zimbabwe

Specifications (AL-60B2)[edit]

Data from Jane's All The World's Aircraft 1966–67[15]

General characteristics

Performance

270 km/h (170 mph; 150 kn) at 4,800 m (15,700 ft)
206 km/h (128 mph; 111 kn) at 3,000 m (9,800 ft) at 63% power

See also[edit]

Related development

Aircraft of comparable role, configuration, and era

References[edit]

Notes[edit]

  1. ^ Taylor 1961, p. 272.
  • ^ Flying: 8. December 1969.{{cite journal}}: CS1 maint: untitled periodical (link)
  • ^ a b Simpson 2023, p. 19
  • ^ a b Flores, Kuhn & Davis 2001, p. 51
  • ^ Flores, Kuhn & Davis 2001, pp. 51–52
  • ^ a b c d Simpson 2023, p. 20
  • ^ Flores, Kuhn & Davis 2001, p. 52
  • ^ Taylor 1961, p. 7.
  • ^ World Airnews - Kudu with a Turboprop - Birth of an Angel Archived March 30, 2012, at the Wayback Machine
  • ^ "Lockheed Atlas Angel Skydiving Aircraft".
  • ^ Plane and Pilot: 1978 Aircraft Directory, page 58. Werner & Werner Corp, Santa Monica CA, 1977. ISBN 0-918312-00-0
  • ^ a b c d e f g h i j Simpson, R. W. (1991). Airlife's General Aviation (2nd ed.). Airlife Publishing. pp. 15–16. ISBN 1853105775.
  • ^ "Italian Air Force". aeroflight. Retrieved 3 June 2019.
  • ^ "Air Force of Zimbabwe Aircraft Types".
  • ^ Taylor 1966, pp. 88–89.
  • Bibliography[edit]

    External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Aermacchi_AL-60&oldid=1229419559"

    Categories: 
    Atlas Aircraft Corporation aircraft
    1960s Italian civil utility aircraft
    Lockheed aircraft
    Macchi aircraft
    1950s United States civil utility aircraft
    Single-engined tractor aircraft
    High-wing aircraft
    Aircraft first flown in 1959
    Hidden categories: 
    CS1 maint: untitled periodical
    Webarchive template wayback links
    Articles needing additional references from August 2011
    All articles needing additional references
    Articles with short description
    Short description is different from Wikidata
    Aircraft specs templates using more performance parameter
    Commons category link from Wikidata
     



    This page was last edited on 16 June 2024, at 18:19 (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