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 Australia Aircraft

CA25 Winjeel

 

Despite its detail difference, the CA-25 Winjeel present a strong sense of similarity with the Percival Provost in its proportions, fixed tail wheel landing gear, and two/three seat cockpit enclosure. This type was also used for communications and the training of forward air controllers. The last aircraft was delivered during 1958. Despite its overall popularity by the Aerospace CT-4A Air-trainer by 1975.

 

TECHNICAL DATA

Description Specifications
Manufacturer:  Commonwealth Aircraft Corporation Length: 38 ft 7.5 in.
First Flight: February 1951 Height: 9 ft. 1 in.
Model: CA-25 Wing Span: 38. ft 7.5 in.
Crew: Two or three Wing Area: 249.0 sq ft.
Nickname: Winjeel Empty Weight: 3,323 lb
Basic Role:  Basic trainer. Max. Take Off Weight: 4,265 lb.
Principal Versions: Ca-25 Production Model. Armament: None

Performance

Propulsion

Range: 550 miles

Power Plant: Pratt & Whitney
Max. Speed: 186 mph at 4,500 ft. Horsepower: 445-hp
Ceiling: 18,000 ft. No. Of Engines: One
Climb Rate: 15,000 ft. per minute. Photo: Coil B. Thouanel

 

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