Supriya Ghosh (Editor)

Keystone–Loening Air Yacht

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
210 km/h

Length
  
11 m

Wingspan
  
14 m

Designer
  
Grover Loening

Keystone–Loening Air Yacht httpsuploadwikimediaorgwikipediacommonsthu

Manufacturers
  
Loening Aeronautical Engineering, Keystone Aircraft

The Loening C-4C, later the Keystone-Loening K-85 Air Yacht following the merger of the Loening and Keystone companies, was an amphibious utility biplane built in the United States in the late 1920s. It was developed by Grover Loening from the C-1 that he had created together with Leroy Grumman, incorporating a new fuselage design. This departed from the characteristic Loening design feature of having a slender, "shoehorn" float projecting from the underside of the fuselage with an engine mounted tractor-fashion above it. Instead, the C-4C had a conventional flying-boat hull, with an enclosed cabin for passengers. The engine was mounted in a separate nacelle on the leading edge of the upper wing.

Two C-4Cs were built in 1928, shortly before the corporate merger. In 1931, Keystone-Loening built two examples of a revised version, but no further production ensued.

Specifications (K-85 Air Yacht)

General characteristics

  • Crew: One pilot
  • Capacity: 7 passengers
  • Length: 37 ft 2 in (11.33 m)
  • Wingspan: 46 ft 8 in (14.22 m)
  • Powerplant: 1 × Wright Cyclone, 525 hp (390 kW)
  • Performance

  • Maximum speed: 130 mph (210 km/h)
  • Range: 500 miles (800 km)
  • References

    Keystone–Loening Air Yacht Wikipedia