|Loaded weight (normal)||1230kg|
|Loaded weight (maximum)||1310kg|
|Wing Load (kg/m2)||56|
|Power load (kg/hp)||8.5|
|Speed at 0m||245km/h|
|Rate at 0m||4.2m/sec|
Low-wing 3-4 seat liaison monoplane with enclosed cockpit, built in November 1944. Designation Yak-12 fas replaced by Yak-13 after design stage was completed. Yak-13 was equipped by VISh-327 variable-pitch propeller designed by G.M.Zaslavskij. Construction - mostly wood/plywood, with aluminum skin on tailplane and fin, fabric - on ailerons and tail controls.
Aluminum landing flaps installed under the fuselage and wing roots. Main landing gear - retractable, tailwheel - fixed.
|Created January 25, 1996
Modified February 16, 1999