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Loss of Power Results in Runway Excursion and Wing Spar Damage (N442C)

Las Cruces, NM, US

On March 24, 2000, a Stinson 108-2 (registration N442C) was involved in an aviation accident near Las Cruces, NM. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain directional control, resulting in an inadvertent ground loop/swerve. Factors were a burnt and unseated intake valve, and the tail wind. 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 experienced insufficient engine power after takeoff from runway 26, executed a 180-degree turn, and landed on runway 8 with a 5-knot tailwind. Loss of directional control led to a left skid off the runway, bending the right rear spar. Post-incident examination found a burnt No. 6 intake valve.

Incident Summary

The pilot reported that shortly after takeoff from runway 26, the engine failed to develop sufficient power. In response, the pilot made a 180-degree turn and initiated a landing on runway 8. An estimated tailwind of 5 knots was present during the landing. The pilot stated that he could not maintain directional control, causing the airplane to skid to the left and depart the runway. The right rear spar was bent as a result of the excursion.

Engine Examination

Following the incident, the engine was disassembled and inspected. The examination revealed that the No. 6 intake valve was burnt and was not seating properly. The mechanic informed the pilot that this condition would account for the observed loss of power.

Frequently asked questions

What happened in the 24 Mar 2000 Stinson 108-2 accident near Las Cruces, NM?

A pilot experienced insufficient engine power after takeoff from runway 26, executed a 180-degree turn, and landed on runway 8 with a 5-knot tailwind. Loss of directional control led to a left skid off the runway, bending the right rear spar. Post-incident examination found a burnt No. 6 intake valve.

Were there any fatalities in the 24 Mar 2000 Stinson 108-2 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 24 Mar 2000 involved a Stinson 108-2, registration N442C, at Las Cruces, NM.

What was the probable cause of the accident?

The pilot's failure to maintain directional control, resulting in an inadvertent ground loop/swerve. Factors were a burnt and unseated intake valve, and the tail wind.

More accident analyses

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20622. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.