Casualties unknown

1982-09-24: Beech 58P (N2027C) — Louisiana Dept. OF Corrections — Midland, TX

Midland, TX, US

On September 24, 1982, a Beech 58P (registration N2027C) operated by Louisiana Dept. OF Corrections was involved in an aviation accident near Midland, TX. 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 1781061362Data APIEditorial standards

An aircraft executing an intersection takeoff from the middle of Runway 25 experienced a left engine power loss during initial climb. The pilot attempted to restore power and maneuvered to avoid an apartment building but struck the roof, then impacted a parking lot and burned. No mechanical defects were found.

Accident Sequence

The aircraft began an intersection takeoff from near the middle of Runway 25, with 2,096 feet of runway remaining. The pilot stated that the takeoff was normal until he began an initial power reduction to 34 inches of manifold pressure and 2,400 RPM. At that time, the left engine reportedly continued to lose power and manifold pressure. The pilot attempted to restore power momentarily, then moved all handles forward and lowered the nose as long as he could to build up speed.

As the aircraft approached an apartment building, the pilot pulled up, but the airplane struck the roof, then impacted in a parking lot and burned. The pilot, a passenger, and a resident of the apartment were burned.

Investigation Findings

During the investigation, no mechanical defects were found that would cause a loss of power. The weather at 1419 CDT was: temperature 85°F, wind from 070° at 8 knots, altimeter 30.07 inches of mercury. The elevation was 2,805 feet.

Weight and Performance Considerations

The distance from the intersection to the apartment building was 2,477 feet. The distance required to clear a 50-foot obstacle would have been 4,000 feet at the maximum gross weight limit. The estimated gross weight was 195 pounds over the 6,100-pound limit. The maximum weight to achieve a single-engine rate of climb at liftoff would have been 5,050 pounds.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X04584. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.