Thirty of these tandem two-seat primary training gliders have been built by 1961, since August 1953, when the prototype made its first flight.
Construction is conventional, with a fabric-covered steel-tube fuselage nacelle and fabric-covered two-spar braced wooden wing.
Horikaw A H-22B-3
Span: 40 ft l in
Length: 23 ft
Wing area: 181 sq.ft
Gross weight: 661 lb
Empty weight: 375 lb
Max L/D: 14.2 at 41,5 mph
Min sink: 3.8 ft/sec at 34 mph