from the April, 1935 Aero Digest:
• President and Chief Engineer: P. W. Nichols. Vice-president: W. F. Theis. General Manager: V. A. Cheever. Sales Manager: U. H. Burfeind. Export representative: Aircraft Mechanics, Inc., Export Department, 44 Whitehall St., New York City, N. Y.
Three-place open biplane: Approval number 2-103. Wright J6-5 engine, 170 horsepower.
Span 36 feet 8 inches. Length overall 25 feet 7.5 inches. Height overall 9 feet 10 inches. Wing area 287 square feet.
Power loading 15.7 pounds per horsepower. Wing loading 7.85 pounds per square foot.
Weight empty 1651 pounds. Useful load 937 pounds. Payload 340 pounds. Gross weight 2588 pounds. Fuel capacity 65.5 gallons. Oil capacity 5 gallons.
Maximum speed 115 miles per hour. Cruising speed 95 miles per hour. Service ceiling 16,000 feet. Rate of climb 925 feet per minute. Cruising range 700 miles.
Fuselage: steel tubular welded, fabric covered; tandem seating arrangement with two persons in front; dual controls. Wings: spruce spars and ribs; fabric covered; no flaps; metal trailing edge; ailerons are boxbeamed and wood-ribbed construction, fabric covered. Tail group: steel tubular construction, fabric covered; stabilizer adj ustable in flight; fin is fixed. Landing gear: fixed split-type with 8.50 X 10 airwhee1s, Warner brakes and rubber cord shock absorbers.
Standard equipment includes wiring for navigation lights, opening on instrument board for compass, fuel cut-off, left or right throttle, baggage compartment, streamlined head rest, inspection windows, starter bracket, fire extinguisher, tie down ropes, first aid kit, cockpit covers, removable throttle handle, safety belts, adjustable stabilizer, Hamilton Standard propeller.
Instruments: altimeter, oil gauge, fuel gauge, temperature gauge, tachometer.