Clinger CL-1

In 1934, American engineer W.R. Clinger from Grandville, Michigan, designed and built a light aircraft named the Clinger CL-1. This unique aircraft was a two-seat, single-strut biplane.

Design and Technical Specifications

It was equipped with a 90 hp Curtiss OX-5 piston engine, featuring a pusher propeller configuration. Only one instance of this aircraft, serial number 14149, was ever built.

Seaplane Capability

A notable aspect of the Clinger CL-1’s design was its capability to take off from water, making it a versatile light aircraft for its time.

Technical Specifications

Modification CL-1
Engine type 1 Piston engine Curtiss OX-5
Power, hp 1 x 90
Maximum speed, km/h 145
Cruising speed, km/h 121
Crew, crew 1

Image gallery of the Clinger CL-1