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Frankenmuth, MI
WHILE IN CRUISE FLIGHT, THE ENGINE SUSTAINED LOSS OF POWER. AN EMERGENCY LANDING WAS MADE IN A CROP FIELD, WHERE THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. THE PILOT INDICATED THAT HE MAY HAVE ACTIVATED THE MIXTURE INSTEAD OF THE CARBURETOR HEAT. SUBSEQUENT EXAMINATION REVEALED THAT THE CONTROL KNOBS FOR THE MIXTURE AND CARBURETOR HEAT WERE THE SAME SHAPE, SIZE, AND COLOR.
IMPROPER USE OF THE MIXTURE CONTROL BY THE PILOT. FACTORS RELATED TO THE ACCIDENT WERE: THE SIMILARITY OF SHAPE, SIZE, AND COLOR OF THE MIXTURE AND CARBURETOR HEAT CONTROLS AND THE TERRAIN CONDITION (WITH CROP) IN THE EMERGENCY LANDING AREA.
On October 24, 1993, at 1714 eastern daylight time, a Cessna 140, N73003, registered to Ronald C. Thompson of Saginaw, Michigan, and operated by a private rated pilot, experienced a total loss of engine power while in cruise flight. A forced landing was conducted to a crop field. The airplane impacted the terrain on landing and sustained substantial damage. The pilot and one passenger reported no injuries. The personal 14 CFR Part 91 flight was operating in visual meteorological conditions. No flight plan was on file. The local flight departed Frankenmuth, Michigan at 1630. On initial contact the pilot-in-command stated that he might have pulled the mixture instead of the carburetor heat. An examination of the airplane subsequent to the accident did not find any mechanical anomalies which would have contributed to the accident; however the instrument panel arrangement of mixture and carburetor heat are non-standard according to modern industry accepted standards. The shape, size, and color of the knobs is the same. Verification of the function of the control is not identifiable by tactile or visual identification.