from April, 1935 Aero Digest:
• President: Taylor Stanley. Vice-president: H. V. Fetick, General Manager: C. S. McKenzie, Jr., Sales Manager: J. c. Welsch. Chief Engineer: Roger E. Schlemmer. Export representatives: Howard T. Byler, Edificio A. Noite, Rio de Janeiro, Brazil, S. A. Messrs. Strachan & MacMurray, Iloilo, Philippine Islands.
Two-place high-wing monoplane. A TC 396. Aeronca E-113B engine, 36 horsepower.
Span 36 feet. Length overall 20 feet. Height’ 7 feet 6 inches. Wing area 142.2 square feet. Chord 50 inches.
Power loading 25.1 pounds per horsepower. Wing loading 7.06 pounds per square foot.
Empty weight 569 pounds. Useful load 437 pounds. Payload 190 pounds. Gross weight 1006 pounds. Fuel capacity 8 gallons. Oil capacity .75 gallon.
Maximum speed 93 miles per hour. Cruising speed 85 miles per hour. Landing speed 35 miles per hour. Service ceiling 12,000 feet. Rate of climb 450 feet per minute. Cruising range 200 miles.
Fuselage: welded steel tubing frame, integral engine mount, wood fairing, fabric covering; three 1ongerons, with single longeron on top side; fin integral with fuselage. Wings: solid spruce spars with built-up spruce ribs, double drag wire bracing, fabric covered; supported by 4 lift wires on each side and 2 landing wires on top side; ailerons of dural corrugated sheet. Tail group: welded steel tubing, fabric covered; stabilizers and elevators interchangeable between right and left sides. Oleo type single-strut landing gear, equipped with 16 X 7 Goodyear tires, Goodyear wheels, and Aeronca oleo shock absorbers.
Standard equipment includes navigation lights, landing lights, cabin heater, compass, brakes and extra fuel tank.
Instruments: tachometer, oil pressure gauge, oil temperature gauge, altimeter, choke, throttle and ignition switch, automatic spark control, and first aid kit, fire extinguisher.