CEN15LA062

Factual narrative

On November 30, 2014, about 1740 central standard time, a Piper PA-28R-201T, N533MC, was damaged during a hard landing at the Addison Airport, near Dallas, Texas. The pilot and his three passengers were not injured. The airplane incurred damage to the wings and fuselage. The aircraft was registered to Metroplex Flight Services, LLC. and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not on a flight plan. The flight originated from the Eppley Airfield, Omaha, Nebraska about 1700.The pilot reported that during landing, a gust of wind encountered just prior to touchdown pushed the airplane sideways into the grass adjacent to the 100- foot wide runway. The airplane subsequently landed hard and received substantial damage to the wing and fuselage. The weather conditions reported at the accident airport included wind from 50 degrees left of runway heading at 9 knots gusting to 19 knots. The pilot reported no abnormalities with regard to the flight control system of the airplane. The pilot reported that during the cruise portion of the flight, smoke was entering the cockpit from behind the instrument panel. He reported that he opened the vent window and the smoke cleared and that there was no obstruction to vision during the landing. Examination of the airplane after the accident revealed that three of the four screws attaching the valve cover on the right rear cylinder were missing. Evidence of oil leaking from the valve cover onto the exhaust was evident. The private pilot reported that, just before touchdown while conducting a personal flight, the airplane encountered a wind gust that pushed it sideways toward the grass adjacent to the runway. The airplane subsequently landed hard, which resulted in substantial damage to the wings and fuselage. The weather conditions reported at the airport included wind from 50 degrees left of the runway heading at 9 knots gusting to 19 knots. The pilot reported no abnormalities with the flight control system. Based on the available information, it is likely that the pilot failed to maintain airplane control while landing with a gusting crosswind. The pilot reported that, during the cruise portion of the flight, smoke entered the cockpit from behind the instrument panel. He said that opening the vent window cleared the smoke in the cockpit and that his vision was not obstructed during the landing. Examination of the instrument panel revealed that three of the four screws that secure the right rear rocker panel cover were missing and that oil was leaking onto the engine's exhaust. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

• C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
• C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
• C Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation - C
• C Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on operation - C
• — Aircraft-Aircraft systems-Indicating/recording systems-Instrument panel-Not specified
• — Aircraft-Fluids/misc hardware-Fluids-Oil-Not specified