4 fatalities

Nighttime Crash Due to Propeller Failure and Loss of Engine (NC14599)

Gilmer, United States of AmericaFlight

On August 14, 1935, a Stinson Model A (registration NC14599) operated by Delta Airlines was involved in an aviation accident near Gilmer, United States of America in flight. 4 people were killed. Investigators recorded the probable cause as: The accident was caused by the pilot losing control of the aircraft due to the absence of the left outboard engine and disturbed airflow over the wing, which resulted from a propeller blade breaking and causing the engine to detach. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-08-27Data APIEditorial standards

A four-engine aircraft crashed into a desert area at night after a propeller blade broke, causing the left engine to detach. The loss of control resulted in the deaths of all four occupants on board.

What happened

During a southbound cruise near Gilmer, a blade from the left engine propeller assembly detached while the aircraft was in flight. In response to this mechanical failure, the crew initiated an emergency procedure by reducing altitude to attempt a landing. As the aircraft approached for a nighttime touchdown, the left engine separated completely from the airframe. This sudden structural loss rendered the airplane uncontrollable, leading to a crash in a remote desert region. All four occupants on board were killed in the accident.

Findings

The investigation determined that the initial failure was caused by an unbalanced condition resulting from the breaking of a propeller blade. Physical evidence supported this conclusion, as the detached engine was recovered approximately one mile southwest of the main wreckage site, while fragments of the broken propeller blade were found about 300 yards west of the engine. The final loss of control during the emergency landing attempt is attributed to the absence of the left outboard engine's weight and the subsequent disruption of airflow over the wing.

Probable cause

The accident was caused by the pilot losing control of the aircraft due to the absence of the left outboard engine and disturbed airflow over the wing, which resulted from a propeller blade breaking and causing the engine to detach.

Frequently asked questions

What happened in the 14 Aug 1935 Stinson Model A accident near Gilmer, United States of America?

A four-engine aircraft crashed into a desert area at night after a propeller blade broke, causing the left engine to detach. The loss of control resulted in the deaths of all four occupants on board.

Were there any fatalities in the 14 Aug 1935 Stinson Model A accident?

The accident was fatal, resulting in 4 fatalities.

What aircraft was involved and where did it happen?

The accident on 14 Aug 1935 involved a Stinson Model A, registration NC14599, operated by Delta Airlines, at Gilmer, United States of America.

What was the probable cause of the accident?

The accident was caused by the pilot losing control of the aircraft due to the absence of the left outboard engine and disturbed airflow over the wing, which resulted from a propeller blade breaking and causing the engine to detach.