Casualties unknown

Aerial Application Aircraft Substantially Damaged After Wind Shear Encounter (N701Y)

Alligator, MS, US

On June 3, 1983, a Grumman G-164 (registration N701Y) was involved in an aviation accident near Alligator, MS. Investigators recorded the probable cause as: The pilot's inability to arrest the descent due to encountering wind shear during a turn to reverse direction on an aerial application flight, which resulted in a collision with the terrain. 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 2026-06-20Data APIEditorial standards

An aircraft sustained substantial damage after colliding with terrain during a turn while conducting aerial application operations, attributed to wind shear preventing the pilot from arresting descent.

What happened

The aircraft was engaged in an aerial application flight when it collided with the terrain. The incident occurred specifically during a maneuver intended to reverse the direction of the flight path. According to the pilot's account, the crew encountered a wind shear event while executing this turn. This sudden change in wind conditions prevented the pilot from arresting the descent rate effectively.

The aircraft impacted the ground, striking first on the main landing gear. The collision resulted in substantial damage to the airframe and components. At the time of the accident, the nearest weather reporting station was located in Memphis. Reports from that station indicated winds blowing from 180 degrees at a speed of 9 knots. No unusual weather phenomena were reported by the station.

The investigation

The investigation focused on the mechanical condition of the aircraft following the impact. Examination revealed that the damage was concentrated around the main gear area where the initial contact with the terrain occurred. The extent of the damage was classified as substantial, indicating significant structural compromise to the airframe.

Findings

Contributing factors included the encounter with wind shear during a critical phase of flight. The pilot's inability to maintain altitude or arrest descent due to this meteorological condition led directly to the loss of control and subsequent impact with the ground. The weather conditions at the nearby reporting station did not reflect the localized intensity experienced by the aircraft.

Safety message

Pilots conducting low-level aerial application operations should remain vigilant for wind shear, particularly during turns or direction changes. Sudden shifts in wind speed or direction can rapidly degrade performance and make it difficult to maintain safe flight parameters.

Probable cause

The pilot's inability to arrest the descent due to encountering wind shear during a turn to reverse direction on an aerial application flight, which resulted in a collision with the terrain.

Frequently asked questions

What happened in the 3 Jun 1983 Grumman G-164 accident near Alligator, MS?

An aircraft sustained substantial damage after colliding with terrain during a turn while conducting aerial application operations, attributed to wind shear preventing the pilot from arresting descent.

What aircraft was involved and where did it happen?

The accident on 3 Jun 1983 involved a Grumman G-164, registration N701Y, at Alligator, MS.

What was the probable cause of the accident?

The pilot's inability to arrest the descent due to encountering wind shear during a turn to reverse direction on an aerial application flight, which resulted in a collision with the terrain.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X43203. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.