On March 26, 2016, about 1345 central daylight time, a Piper PA-24-250 airplane, N8154P, was substantially damaged during a forced landing near Kentland, Indiana. The flight instructor and private rated pilot receiving instruction sustained minor injuries. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, which operated without a flight plan. The local flight originated from the Kentland Municipal Airport (50I), Kentland, Indiana.According to the flight instructor, following air work he demonstrated how to use the single fuel gauge and the momentary selector buttons to display how much fuel was in each tank. He then demonstrated the gauge using the fuel selector. The instructor could not recall which position he left the fuel selector in. He reduced power and descended from 3,000 ft mean sea level through 1,500 ft and set up for a 500 ft per minute descent towards runway 09 with approximately 14 inches manifold pressure, fuel pump on, and carburetor heat on. At an undetermined time, the private pilot began flying the airplane. About ½ mile from the approach end of the runway 9, the airplane's descent rate increased so the instructor called for the private pilot to add engine power. When the engine did not respond, the instructor took control of the airplane and turned right to land in a field. He checked the engine instruments and fuel quantities and could not get the engine to respond. The airplane stalled about 10-15 ft above ground level and the airplane landed hard. The instructor turned off the cockpit switches to include the fuel selector and both pilots exited the airplane. The responding Federal Aviation Administration inspectors examined that wreckage and found substantial damage to the fuselage and both wings. In addition, each fuel tank contained an unmeasured amount with the exception of the right auxiliary tank which was found empty. No anomalies were discovered which would have precluded normal operation of the engine. After the accident, the instructor recalled that during the air work portion of the flight, the right wings seemed to be "a bit heavy" but he was not surprised since most of the indicated fuel was contained in the right main and right auxiliary tanks. A review of the Carburetor Icing Probability Chart located in the FAA's Special Airworthiness Information Bulletin CE-09-35, Carburetor Icing Prevention, dated June 30, 2009, found that the airplane was operated in an area conducive to the formation of serious icing while operating at glide power.