from Aero Digest, April, 1935:
Kinner Airplane & Motor Corporation, Ltd., Glendale, California
• Two-place open low-wing monoplane. ATC 522. Kinner B-5 engine, 125 horsepower. Span 34 feet 5 inches. Length overall 24 feet 2 inches. Height overall 7 feet. Chord 6 feet. Wing area 199 square feet. Power loading 16.0 pounds per horsepower. Wing loading 10.0 pounds per square foot.
Empty weight 1333 pounds. Useful load 667 pounds. Payload 268 pounds. Gross weight 1950 pounds. Fuel capacity 35 gallons. Oil capacity 2.5 gallons.
Maximum speed 122 miles per hour. Cruising speed 110 miles per hour. Landing speed 45 miles per hour. Service ceiling 14,500 feet. Rate of climb 800 feet per minute. Cruising range 440 miles.
Fuselage: welded chrome molybdenum, steel tubing, rectangular structure, fabric covered; side-by-side seating arrangement. Wing: spruce spars and ribs, double drag truss, fabric covered; Clark Y airfoil section; wings are attached to short stubs built integral with the fuselage and braced to the top fuselage longerons by inverted Vee struts. Tail group: monoplane type, welded chrome molybdenum steel tube, fabric covered, tabs on elevators; adjustable stabilizer. Fixed type landing gear, enclosed in streamlined fairings; equipped with Goodyear 6.50 X 10 semi airwheels, Autofan wheels and brakes, and oleo type shock absorbers; swiveling tail wheel with 8 X 3 streamline tire. Conventional bearings for engine and plane controls.
Standard equipment includes a Hotspot battery, navigation lights, Eclipse air starter, removable dual controls, shatter-proof glass windshield, shielding and bonding, parking brake, fire extinguisher, chrome plated exhaust collector, baggage compartment, wood propeller.
Instruments: tachometer, altimeter, air speed indicator, compass, oil pressure gauge, oil temperature gauge.
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