Pitch Trim Anomaly Leads to Crash During Banner Towing Operation

Casualties unknown • Fort Lauderdale, FL, US

A light aircraft crashed during a banner towing operation after the pitch trim was found in the full nose-up position. The pilot and two passengers were killed.

What happened

The accident occurred during a banner towing flight. The pilot's father, who served as a senior captain for Pan Am, and the pilot's fiancee were present on the ground to assist with the banner pickup. According to the father, the aircraft began flying in a very erratic manner immediately after the banner towing hook was released. The plane exhibited significant banking and pitching movements before entering a steep descending right turn.

Two additional witnesses observed the aircraft's behavior and believed it acted as if it were experiencing a cross-control or accelerated stall condition. The flight ended with a crash, resulting in fatalities for the pilot and two passengers on board.

The investigation

A thorough examination of the accident site and available data revealed a critical mechanical anomaly. Investigators found that the pitch trim was set to the full nose-up position at the time of the crash. Despite this finding, no reason could be determined for why the trim was in that specific configuration.

Mechanical inspections also covered the propulsion system. No problems were found with the engine during the investigation. Witnesses reported that the engine operated at constant power throughout the final moments of the flight, indicating that engine failure or loss of power was not a contributing factor to the accident sequence.

Findings

The primary finding was the unexplained full nose-up pitch trim setting. This configuration likely contributed to the aircraft's erratic behavior and subsequent loss of control. The lack of a discernible reason for the trim position remains an unresolved aspect of the investigation. The engine performance was confirmed to be normal, ruling out mechanical failure as a cause.

Safety message

Pilots should ensure that all flight controls, including pitch trim, are properly set and secured before and during flight operations. Regular pre-flight checks and post-flight inspections can help identify unexpected control surface positions.

Probable cause

The unexplained full nose-up pitch trim position, which contributed to the aircraft's erratic behavior and loss of control.

Frequently asked questions

What happened in the 1983-03-20 Piper J3C-65 accident near Fort Lauderdale, FL?

A light aircraft crashed during a banner towing operation after the pitch trim was found in the full nose-up position. The pilot and two passengers were killed.

What aircraft was involved and where did it happen?

The accident on 1983-03-20 involved a Piper J3C-65, registration N3618K, at Fort Lauderdale, FL.

What was the probable cause of the accident?

The unexplained full nose-up pitch trim position, which contributed to the aircraft's erratic behavior and loss of control.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X42515. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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