N7884DPiper PA-18S-150 · 1954

The pilot stated that after the approximate one hour flight, she configured the airplane for a 3-point, short field landing. She was planning to land on the airstrip that slopes uphill towards the east, with shallow ditches on either side. After touchdown, the airplane rolled about 90 feet and began to veer to the left of the center. Despite her attempts to correct with right rudder, the airplane did not respond. The pilot added engine power in an effort to increase the airflow over the tail and the airplane immediately veered right to about a 70 degree angle across the narrow strip. She subsequently added full power in an effort to abort the landing since the airplane was nearing the down slope of the ditch. The right main gear hit the far side of the ditch and she retarded the throttle and brought the airplane to a stop. During the accident sequence, the airplane incurred structural damage to the gearbox.

The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

The pilot reported that after a normal touchdown the airplane drifted toward the right side of the runway. He attempted to correct for the right drift with a left rudder input, but the wind suddenly changed direction and airplane veered to the left. He applied full brakes to stop the airplane from leaving the runway, but in the process the airplane nosed over. The vertical stabilizer, rudder, both wings, and cabin structure were substantially damaged. The pilot reported that there were no pre-impact mechanical malfunctions or failures that would have precluded normal operation of the airplane. About 4 minutes before the accident, a local weather station reported that the prevailing wind was out of the southwest at 4 knots. About 16 minutes after the accident, the same weather station reported that the wind speed had increased to 8 knots, with 14 knot wind gusts.