No fatalities

Cargo Flight Crashes After Uncontrolled Descent Near Charlotte (N182)

Goldsboro, United States of AmericaFlight

On January 15, 1980, a Rockwell Grand Commander 690 (registration N182) operated by Corporate Air - USA was involved in an aviation accident near Goldsboro, United States of America in flight. No fatalities were reported. Investigators recorded the probable cause as: Uncontrolled descent and subsequent crash due to engine structure issues. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards
Aircraft registered N182
Aircraft registered N182. Photo: Photo n. 62-8238 released by Federal Aviation Administration / Public domain, via Wikimedia Commons

A cargo flight from Hartford to Charlotte experienced technical problems at night, lost 2,000 feet, entered an uncontrolled descent, and crashed in a field. The pilot was seriously injured. Engine structure issues were the probable cause.

Summary

A cargo flight operating between Hartford and Charlotte crashed after suffering an uncontrolled descent. The pilot reported technical problems to air traffic control during night cruise. The aircraft lost 2,000 feet before entering an uncontrolled descent and impacting a field. The pilot sustained serious injuries.

Accident Details

While in normal cruise at night, the pilot informed ATC about technical problems. Shortly afterward, the aircraft lost 2,000 feet of altitude and entered an uncontrolled descent. The aircraft eventually crashed in a field. The pilot was seriously injured. The flight was a cargo operation from Hartford to Charlotte.

Probable Cause

The official probable cause is an uncontrolled descent and subsequent crash due to engine structure issues. Contributing factors reported include: engine tearaway, engine structure issues with mount and vibration isolators, material failure, separation in flight, pilot reported pitchup with autopilot off (recovered with light g load), and right engine inbound mount pulled out.

Conclusion

The investigation determined the cause of the accident was related to engine structure failures leading to an uncontrolled descent. The pilot's report of pitchup and recovery with light g load was noted. No additional contributing factors were specified beyond those listed.