covered with canvas and aluminium in engine part. Rectangular three-section wings with rounded tips, two-spar, were covered with plywood in forward part and canvas in a rear part. A central part of wings was some distance above the canopy, supported with struts. Side sections of wings were supported with V struts and folds rearwards. The aircraft can seat two, sitting side by side in a covered cockpit. A luggage compartment was behind a cockpit, that could fitted with a 3rd seat. The PWS-52 had a fixed conventional landing gear, with a rear skid. The aircraft used 4-cylinder air-cooled straight engine de Havilland Gipsy I in front, 85/95 hp nominal/take-off power, later replaced with de Havilland Gipsy III, 120 hp, with two-blade wooden propeller of a fixed pitch. Fuel tank (170 L capacity) is placed in a central wing section (normal amount of fuel - 90 L). Fuel consumption rate is 25 L/hour (Gipsy I) or 28 L/hour (Gipsy III). Specifications See also References External links Photos and drawings at Ugolok Neba PWS-52 PWS-52 Single-engined tractor aircraft High-wing aircraft Aircraft first flown in 1930