PIPER PA-32R-300 near New Site, MS — 2012-07-08
- Date
- 2012-07-08
- Location
- New Site, MS, USA
- Aircraft
- PIPER PA-32R-300
- Registration
- N4386F
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 3
- Phase of flight
- Descent
Probable cause
The pilot's decision to operate into a known area of adverse weather, which resulted in the inadvertent penetration of a severe thunderstorm, a subsequent loss of control, and in-flight breakup of the airplane.
NTSB narrative
Before departing on the accident flight, the pilot filed three instrument flight rules flight plans but had not requested nor received a weather briefing. A witness near the accident site reported a thunderstorm in the vicinity and observed the airplane enter a cloud followed shortly by a "loud pop." The witness then observed pieces of the airplane coming out of the cloud. The left wing and vertical stabilizer were located about 1,500 feet away from the main wreckage. Examination of the fracture surfaces revealed signatures consistent with tensile overload failure. No preimpact mechanical malfunctions were noted that would have precluded normal operation of the airplane. Review of radar and weather data indicated the presence of thunderstorms along the route of flight, as well as in the vicinity of the accident site, with the potential for some of them to be severe. The satellite datalink weather product in the airplane cockpit uploaded weather data every 5 minutes and likely would have shown a thunderstorm cell increasing in severity to the highest intensity level near the time of the in-flight breakup. According to Federal Aviation Administration publication “General Aviation Pilot’s Guide to Preflight Weather Planning, Weather Self-Briefings, and Weather Decision Making,” datalink weather products are not as accurate or current as onboard weather radar, which provide real-time weather radar images in the cockpit. It is likely that the pilot attempted to maneuver around the weather hazard and inadvertently encountered a thunderstorm cell, which resulted in an in-flight breakup of the airplane due to overstress of the structure.
Analysis
- Primary failure mode
- Controlled flight into terrain
- First missed decision gate
- Pilot could have chosen to circumnavigate thunderstorms instead of entering them.
NTSB coding
Evidence available
- ATC audio
- ADS-B / radar
- Photos
- 18 docket documents
Docket documents18
- ATC Transcripts (Partial)atc
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Interview Summaryinterview
- Corinith, Mississippi Weatherother
- DUATS Flight Planother
- Fuel Receiptother
- Lockheed Martin Flight Services Emailother
- Tupelo, Mississippi Weatherother
- XM WX Satellite Weather Depictionsother
- Photo 1: Overview of Main Wreckagephotos
- Photo 2: View of Trees Above Main Wreckagephotos
- Photo 3: View of Left Wing at Restphotos
- Photo 4: View of Engine After Recoveryphotos
- FlightAware Flight Trackradar
- Radar Over Google Earth with Weather Overlayradar
- Meteorology 5 - Weather Study Report of Group Chairmanreport
- Toxicological Reportreport
- Wreckage Plot (Google)wreckage
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