No fatalities

30 Jun 2019: BEECH C23 C23 (N24580) — Tiger Capital, LLC — Ludlow, CA

Ludlow, CA, United States

On 30 Jun 2019, a BEECH C23 C23 (registration N24580) operated by Tiger Capital, LLC was involved in an aviation accident near Ludlow, CA. No fatalities were reported. Investigators recorded the probable cause as: Maintenance personnel’s failure to properly tighten an oil line fitting, which resulted in a total loss of engine power. 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

A Beechcraft C23 sustained substantial damage during an emergency landing near Ludlow, California, after the engine lost power. The pilot and passenger were uninjured. Post-accident examination revealed a loose oil cooler fitting as the likely source of oil loss.

Accident Overview

On June 30, 2019, at about 1134 Pacific daylight time, a Beechcraft C23 airplane, registration N24580, was substantially damaged in an accident near Ludlow, California. The pilot and passenger were not injured. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight.

Flight and Engine Failure

According to the pilot, the preflight inspection revealed no anomalies. One quart of oil was added, bringing the total to 7.5 quarts. While cruising at 6,000 feet above ground level, the pilot detected a faint smell of burning paint. Within 10 seconds, the oil pressure gauge dropped to zero and engine RPM decreased to about 2,100. A few seconds later, the engine lost power completely.

Emergency Landing

The pilot executed an emergency landing. Upon touchdown, the three landing gear separated, the engine cowling was forced aft, and the firewall sustained deformation at the mounting points. Oil residue was observed on the lower left side of the fuselage, and the dipstick showed no oil, though it was properly secured.

Post-Accident Examination

The engine had been recently overhauled and had accumulated approximately 4 hours of operating time since returning to service. A certified mechanic, under the oversight of a Federal Aviation Administration inspector, examined the engine in Chino, California. The inspection found that the AN hose fitting on the oil cooler was loose, with oil residue present in that area. No other pre-impact mechanical anomalies were detected that could have precluded normal operation.

Contributing factors

Fluid levelIncorrect service/maintenance