|Engines||1*50hp Walter-Micron||1*80hp Pobjoy||1*65hp M-23|
|Wing Load (kg/m2)||32.5||-||-|
|Power load (kg/hp)||6.5||-||-|
|Maximum Speed at 0m||165km/h||190km/h||170km/h|
Aerobatic single-seater with open cockpit. G-22 was built in 1936 and dedicated to X Congress of VLKSM. All project (from first drawings to aircraft roll-out) was done in 2 months - January 7 to March 7.
Wing had removable automatic leading edge slats. G-22 was re-engined few times.
|Created January 6, 1999||Back to|