from the April, 1935 Aero Digest:
• Two-place high-wing monoplane. A TC 449. Szekely SR-3 engine, 45 horsepower.
Span 37 feet 9.5 inches. Length overall 21 feet 8.5 inches. Height overall 5 feet 8.5 inches. Wing area 175 square feet. Chord 60 inches.
Power loading 25.3 pounds per horsepower. Wing loading 5.5 pounds per square foot.
Empty weight 589 pounds. Useful load 399 pounds. Payload 173 pounds. Gross weight 962 pounds.
Fuel capacity 7 gallons. Oil capacity 1.5 gallons.
Maximum speed 93 miles per hour. Cruising speed 77 miles per hour. Landing speed 30 miles per hour. Service ceiling 13,000 feet. Rate of climb 700 feet per minute. Cruising range 165 miles.
Fuselage: welded steel tubing, Warren truss type, fabric covered; Pyralin windows; side-by-side seating; dual controls; cabin dimension 5 feet long X 2 feet 6 inches wide X 3 feet 5 inches high; luggage compartment is behind seats; fuel tanks are installed behind the fireproof bulkhead; quickly removable engine mount. Wings: fabric covered wood construction, NACA M-6 section, fabric covered; rigidly-braced; supported above fuselage by system of steel tubular struts; two spruce box spars, I-section ribs, single drag wire bracing; narrow chord ailerons hinged to auxiliary spars. Tail group: steel tubular construction, fabric covered; wire braced; stabilizer adjustable in flight; fixed fin braced from stabilizer by a pair of streamlined wires on either side, the stabilizer being braced to fuselage by steel tube struts. Fixed divided-type landing gear consisting of two pyramids; equipped with Goodyear 16 X 7.3 airwheels. Swivelling spring steel tailskid with hardened steel shoe.
Standard equipment includes wiring for navigation lights, cabin heater, large sliding windows, California or Supreme wood propeller, switch.
Instruments: tachometer, oil pressure gauge, oil temperature gauge, compass, altimeter.
Aircraft Mechanics, Inc., is continuing the work of the former Alexander Aircraft Co.