Casualties unknown

Pilot Loses Contact After Thunderstorm Encounter (N7917D)

Jackson, AL, US

On July 5, 1994, a Beech H-35 (registration N7917D) was involved in an aviation accident near Jackson, AL. Investigators recorded the probable cause as: THE PILOT'S FAILURE TO AVOID AN AREA OF THUNDERSTORM ACTIVITY, WHICH RESULTED IN A LOSS OF CONTROL AND THE DESIGNED STRUCTURAL LIMITS OF THE AIRFRAME BEING EXCEEDED. THE THUNDERSTORMS WERE A FACTOR IN THE ACCIDENT. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A VFR-only pilot, who received a preflight briefing forecasting thunderstorms, entered thunderstorm activity, requested ATC assistance, then transmitted a mayday before losing contact. Wreckage was scattered over a wooded area.

Introduction

According to air traffic, the pilot, operating under visual flight rules (VFR), received a preflight weather briefing. Thunderstorm activity was forecasted along the intended route of flight.

Sequence of Events

While en route, the pilot entered an area of thunderstorm activity and requested air traffic control assistance. The air traffic controller attempted to provide radar vectors but never received a response from the pilot. The pilot's last transmission was, "MAYDAY, MAYDAY, WE'RE GOING DOWN." Seconds later, radio and radar contact were lost. An emergency locator transmitter (ELT) signal was received by another aircraft in the vicinity of the last radar hit.

Wreckage Examination

The aircraft wreckage was scattered over a wooded area measuring 2,500 feet long and 300 feet wide. Examination of the wreckage path revealed that the left and right wing assemblies were located 600 feet apart north of the main wreckage. Examination of the main wing spar fracture revealed that the overload failure occurred in an upward direction. Flight components from the empennage were located south of the main wreckage. Examination of the left ruddervator assembly disclosed that it separated from the airframe in an upward direction.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X01655. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.