Casualties unknown

1991-11-06: Grumman G-164A (N4546) — Faye Pillars — Epps, LA

Epps, LA, US

On November 6, 1991, a Grumman G-164A (registration N4546) operated by Faye Pillars was involved in an aviation accident near Epps, LA. Investigators recorded the probable cause as: The in-flight separation of approximately one half of a propeller blade, which caused severe engine vibrations and led to a forced landing where the engine separated from the airframe and ignited a fire that destroyed the forward fuselage. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A propeller blade separation caused severe engine vibrations, forcing a landing in a cotton field where the engine detached and ignited a fire that destroyed the forward fuselage.

What happened

During flight operations, approximately one half of a propeller blade separated from the airplane. The loss of balance resulted in severe engine vibrations that compromised the structural integrity of the propulsion system. Recognizing the critical nature of the mechanical failure, the pilot initiated an emergency procedure to execute a forced landing.

The aircraft touched down in a cotton field. During the subsequent landing roll, the intense stress caused the engine to separate completely from the airframe. This separation ruptured fuel lines, leading to a fire that started forward of the firewall. The blaze rapidly consumed the area, resulting in total destruction of all components located ahead of the firewall.

The investigation

Post-accident examination confirmed the initial failure mode involved the propeller assembly. The separation of the blade half was identified as the primary event triggering the chain of mechanical failures. Investigators noted the violent nature of the engine detachment during the ground roll, which facilitated the fuel leak and subsequent ignition source.

Findings

The sequence of events began with propeller failure, specifically the in-flight separation of a blade segment. This mechanical defect led to severe engine vibrations that necessitated an emergency landing. The final outcome was determined by the fuel-fed fire that destroyed the forward section of the aircraft after the engine separated from the airframe during the landing roll.

Probable cause

The in-flight separation of approximately one half of a propeller blade, which caused severe engine vibrations and led to a forced landing where the engine separated from the airframe and ignited a fire that destroyed the forward fuselage.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18450. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.