Casualties unknown

Aircraft Impacts Ground After Takeoff at High Density Altitude (N8631K)

Gallup, NM, US

On September 8, 1990, a Stinson 108-1 (registration N8631K) operated by Mcdonald, Rick L. was involved in an aviation accident near Gallup, NM. Investigators recorded the probable cause as: The pilot's failure to account for high density altitude and the aircraft's proximity to maximum gross weight, which resulted in inadequate climb performance. 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 2026-06-19Data APIEditorial standards

An aircraft operating under high density altitude conditions and near maximum gross weight failed to climb adequately after takeoff, resulting in a ground impact with no survivors.

What happened

The pilot attempted to depart from an airport where the prevailing environmental conditions presented significant performance challenges. At the time of the operation, the density altitude was recorded at 9,100 feet, indicating that the air was significantly less dense than standard sea-level conditions. This reduced air density directly impacts engine power output and aerodynamic lift generation.

In addition to the high density altitude, the aircraft was loaded to within 25 pounds of its maximum gross weight limit. The combination of heavy loading and thin air created a scenario where the aircraft's performance capabilities were severely compromised from the moment it began its ground roll.

Following takeoff, the aircraft managed to climb to an altitude of approximately 100 feet above the departure surface. However, it was unable to maintain positive rate of climb. The aircraft subsequently began to lose altitude and entered a steep bank. It impacted the ground in a near-vertical attitude, suggesting a loss of control or inability to sustain flight.

The investigation

Investigation into the mechanical condition of the aircraft revealed no evidence of pre-impact mechanical failure that would have contributed to the accident. The focus of the inquiry remained on the operational parameters and environmental factors present during the flight.

Findings

The primary factors contributing to this accident were the high density altitude and the aircraft's weight configuration. The density altitude of 9,100 feet significantly degraded the aircraft's climb performance. Operating within 25 pounds of maximum gross weight further reduced the margin for error. These conditions combined to prevent the aircraft from achieving or sustaining a safe climb gradient after takeoff.

high density altitude was the critical environmental factor that limited the aircraft's ability to gain altitude. The near maximum gross weight exacerbating the performance deficit meant the aircraft lacked the necessary power-to-weight ratio to overcome the aerodynamic penalties of the thin air. The result was an inability to climb out of ground effect or sustain level flight, leading to the fatal impact.

Safety message

Pilots operating at high elevation airports must carefully calculate density altitude and its effect on performance. Taking off near maximum gross weight in these conditions can lead to catastrophic performance loss. Adequate runway length and favorable weather are essential for safe operations under such demanding circumstances.

Probable cause

The pilot's failure to account for high density altitude and the aircraft's proximity to maximum gross weight, which resulted in inadequate climb performance.

Frequently asked questions

What happened in the 8 Sept 1990 Stinson 108-1 accident near Gallup, NM?

An aircraft operating under high density altitude conditions and near maximum gross weight failed to climb adequately after takeoff, resulting in a ground impact with no survivors.

What aircraft was involved and where did it happen?

The accident on 8 Sept 1990 involved a Stinson 108-1, registration N8631K, operated by Mcdonald, Rick L., at Gallup, NM.

What was the probable cause of the accident?

The pilot's failure to account for high density altitude and the aircraft's proximity to maximum gross weight, which resulted in inadequate climb performance.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X24240. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.