Two-seat single engine trainer aircraft, developed immediately after WWII. It had a buttload of operators, and 1,284 were built between 1947 and 1956 (including license-built models in Britain and Portugal).
https://en.wikipedia.org/wiki/De_Havilland_Canada_DHC-1_Chipmunk
https://www.flugzeuginfo.net/acdata_php/acdata_dhc1_en.php
GENERAL STATS (DHC-1A-1 Chipmunk T.1)
Crew: 2 (student + instructor)
Length: 25 feet 5 inches (7.75 meters)
Wingspan: 34 feet 4 inches (10.46 meters)
Height: 7 feet 1 inch (2.16 meters)
Wing area: 172 square feet (16 meters squared)
Max takeoff weight: 2,200 pounds (998 kilograms)
Powerplant: x1 De Havilland Gipsy Major 1C four-cylinder piston engine, 145 HP
Max speed: 138 MPH (222 KMH, 120 knots) at sea level
Range: 259 miles (417 kilometers, 225 nautical miles)
Service ceiling: 15,800 feet (4,800 meters)
The de Havilland Canada DHC-1 Chipmunk is a tandem, two-seat, single-engined primary trainer aircraft designed and developed by Canadian aircraft manufacturer de Havilland Canada. It was developed shortly after the Second World War and sold in large numbers during the immediate post-war years, being typically employed as a replacement for the de...
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