In-flight breakup of aircraft near Salisbury

Casualties unknown • Libertytown, MD, US

An aircraft experienced an in-flight breakup while encountering heavy thunderstorms and severe weather conditions near Salisbury.

What happened

Prior to takeoff, the pilot, who was not instrument rated, was advised that VFR flight was not recommended. While en route at 9,500 feet, the pilot reported encountering heavy rain and requested vectors to avoid a storm. The air traffic control controller informed the pilot that weather information could not be provided due to the limitations of the ATC radar.

Following this exchange, the pilot reported being in trouble while passing through very heavy thunder. The controller suggested a right turn to 180 degrees to reverse course, which the pilot acknowledged. After this communication, there was no further radio contact with the aircraft. An in-flight breakup occurred, resulting in wreckage being scattered over an area of approximately one mile.

Witnesses near the accident site reported hearing an aircraft flying in weather characterized by heavy rain, strong winds, and low clouds. Additionally, witnesses noted that the sound of the engine was oscillating prior to the crash. At a location approximately 11 miles west, the Salisbury weather included broken clouds at 500 feet, an overcast ceiling at 1,000 feet, and visibility of 1/2 mile with rain and fog.

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Frequently asked questions

What happened in the 1989-07-16 Piper PA-32-300 accident near Libertytown, MD?

An aircraft experienced an in-flight breakup while encountering heavy thunderstorms and severe weather conditions near Salisbury.

What aircraft was involved and where did it happen?

The accident on 1989-07-16 involved a Piper PA-32-300, registration N83HA, operated by Powell Aviation Inc, at Libertytown, MD.

What was the probable cause of the accident?

CONTINUED VFR FLIGHT BY THE NON-INSTRUMENT RATED PILOT INTO INSTRUMENT METEOROLOGICAL CONDITIONS (IMC), WHICH RESULTED IN THE PILOT'S LOSS OF AIRCRAFT CONTROL DUE TO DISORIENTATION, AND OVERLOAD FAILURE OF THE WINGS AND STABILATOR DUE TO THE PILOT EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRCRAFT. FACTORS RELATED TO…

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X28731. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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