Weather (Other) · NTSB CEN15FA268
PIPER PA 32 — Cuba, MO
| Date | June 14, 2015 |
| Location | Cuba, MO |
| Aircraft | PIPER PA 32 |
| Purpose of flight | Personal |
| Conditions | Day · Instrument Meteorological Cond |
| Phase / occurrence | Enroute-cruise Windshear or thunderstorm |
| Pilot age | 54 |
| Pilot total time | 1,203 hrs · Experienced |
| Time in type | Unknown |
| Fatalities | 1 |
Probable cause
NTSB findings
- Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- Aircraft-Aircraft structures-Wing structure-(general)-Capability exceeded - C
- Environmental issues-Conditions/weather/phenomena-Convective weather-Thunderstorm-Effect on operation - C
- Environmental issues-Conditions/weather/phenomena-Convective weather-Thunderstorm-Decision related to condition - C
- Aircraft-Aircraft structures-Empennage structure-(general)-Capability exceeded - C
- Environmental issues-Conditions/weather/phenomena-Convective weather-Thunderstorm-Accuracy of related info - F
- Aircraft-Aircraft systems-Indicating/recording systems-Instrument panel-Capability exceeded - F
What happened
The private pilot was conducting a personal cross-country flight and had filed an instrument flight rules flight plan. The flight was en route to the destination airport, and the pilot was in radar and radio contact with air traffic control (ATC) personnel. While the airplane was in cruise flight at 5,000 ft mean sea level, the pilot checked in with an air traffic controller who alerted the pilot of "moderate to extreme precipitation" 50 miles ahead and about 30 miles in diameter. The pilot acknowledged the information and stated that he would maintain communications with ATC and that he had "a scope onboard." About 30 minutes later, the pilot reported to the controller that he was in the middle of the precipitation and was not experiencing any bumps. He also stated that his weather scope was showing some returns right of his position. About 1 minute later, radar contact with the airplane was lost, and despite multiple attempts, the controller was unable to make radio contact with the pilot. One witness reported that the airplane emerged from the clouds and that one wing had separated from the airplane before impact. Another witness reported observing the airplane above the tree line with pieces of the airplane falling toward the ground as the airplane spun and descended until impact.
Postaccident examination of the engine and airframe revealed no preimpact mechanical malfunctions or anomalies that would have precluded normal operation. The wreckage distribution and signatures and the witnesses' reports were consistent with an in-flight breakup. A review of the weather and radar data showed that, during the final moments of the flight, the airplane made a right, descending turn near an area of moderate-to-high thunderstorm activity, which can include extreme updrafts and downdrafts. Although the turn did not occur within a convective storm cell, it occurred in an area that would have been very dynamic and surrounded by hazardous weather conditions. This encounter with thunderstorm activity likely led to the pilot's loss of airplane control and the exceedance of the airplane's design limits and its subsequent in-flight breakup. Further, based on the pilot's communication with the air traffic controller, he was attempting to use onboard weather radar to maneuver through an area of storms that he should not have been flying through in the first place.