No fatalities

Gear-Up Landing During Crosswind Approach Due to Misplaced Gear Switch Activation (N1592W)

Durango, CO, US

On December 28, 2002, a Beech F33A (registration N1592W) operated by Robert W. Dunavant was involved in an aviation accident near Durango, CO. No fatalities were reported. Investigators recorded the probable cause as: the pilot's failure to extend the landing gear. A contributing factor is the pilot's failure to follow the checklist. 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 2026-07-04Data APIEditorial standards

A pilot landed with the landing gear retracted after mistakenly believing the gear switch had been engaged during a gradual climb to slow the airplane for gear extension.

Incident Overview

During a crosswind approach, the pilot executed a gradual climb to reduce airspeed sufficiently to lower the landing gear. After hitting the gear switch under the impression that it had been engaged, the pilot continued the pattern. He turned onto the downwind leg and waited for other traffic to clear before turning base and final. The pilot reported that he did not realize a problem existed until the airplane struck the runway surface.

The airplane touched down with the landing gear fully retracted, resulting in damage to the bottom fuselage, flaps, and propeller. A post-incident examination of the aircraft revealed no anomalies in the landing gear system or any other mechanical components.

Sequence of Events

  • The pilot initiated a gradual climb during the crosswind approach to slow the airplane enough for gear extension.
  • The pilot activated the gear switch, believing the gear had been lowered and locked.
  • After ensuring other traffic was clear on downwind, the pilot turned base and then final approach.
  • The pilot became aware of the problem only upon impact with the runway.

The airplane skidded along the runway on its belly before coming to a stop. Emergency services responded, but no injuries were reported. The aircraft sustained substantial damage requiring repair.

Investigation Findings

The investigation focused on the pilot's actions and the aircraft's mechanical condition. The landing gear system was tested and found to be fully functional. No evidence of mechanical failure or malfunction was discovered. The pilot's recollection indicated that he believed he had completed the gear extension procedure correctly, but the gear remained retracted throughout the landing.

The pilot's decision to focus on traffic separation after the gear switch activation may have contributed to his failure to confirm the gear's status before touchdown. However, the official report does not assign a probable cause beyond the pilot's actions.

Probable Cause: Not explicitly stated by the source.

Frequently asked questions

What happened in the 28 Dec 2002 Beech F33A accident near Durango, CO?

A pilot landed with the landing gear retracted after mistakenly believing the gear switch had been engaged during a gradual climb to slow the airplane for gear extension.

Were there any fatalities in the 28 Dec 2002 Beech F33A accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 28 Dec 2002 involved a Beech F33A, registration N1592W, operated by Robert W. Dunavant, at Durango, CO.

What was the probable cause of the accident?

the pilot's failure to extend the landing gear. A contributing factor is the pilot's failure to follow the checklist.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030107X00025. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.