No fatalities

23 Jul 2021: CESSNA 150 F (N3059X) — Arden, NC

Arden, NC, United States

On 23 Jul 2021, a CESSNA 150 F (registration N3059X) was involved in an aviation accident near Arden, NC. No fatalities were reported. Investigators recorded the probable cause as: The inadequate inspection of the throttle control cable assembly, which resulted in a partial loss of engine power during cruise flight. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On July 23, 2021, a Cessna 150F (N3059X) experienced an engine power loss due to a separated throttle cable, leading to a forced landing in a coal ash pit where it nosed over.

Accident Overview

On July 23, 2021, at approximately 1830 eastern daylight time, a Cessna 150F, registration N3059X, sustained substantial damage during a forced landing near Arden, North Carolina. The student pilot, the sole occupant, was not injured. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight.

Flight and Engine Power Loss

The pilot departed Asheville Regional Airport (AVL) in Asheville, North Carolina. While climbing through 5,100 feet mean sea level, the engine power dropped to idle. The pilot attempted to adjust the throttle setting, but the tachometer continued to indicate 740 rpm. After establishing best glide speed and declaring an emergency, the pilot turned back toward AVL. When it became clear that the airport could not be reached, the pilot executed a forced landing into a coal ash pit. During the landing roll, the airplane nosed over.

Post-Accident Examination

A Federal Aviation Administration inspector examined the accident site and found substantial damage to the left wing, rudder, and fuselage. The engine throttle cable had separated from the carburetor throttle control lever. The securing hardware—a bolt, washer, and cotter pin—was not located, and there was no evidence of impact damage to the lever or carburetor. After the airplane was recovered, examination of the carburetor revealed the throttle control lever was in the full forward (wide-open) position, matching the cockpit control position. The throttle control cable was separated from the intact lever. Further inspection showed that a spring was not installed on the throttle control lever.

Maintenance History

Review of maintenance records and the tachometer indicated that the accident occurred 15 hours after the airplane's most recent annual inspection.

Contributing factors

Not serviced/maintainedFuel controlling system — FailureMaintenance personnel