No fatalities

17 May 2024: CESSNA 190 (N1500D) — San Luis Obispo, CA

San Luis Obispo, CA, United States

On 17 May 2024, a CESSNA 190 (registration N1500D) was involved in an aviation accident near San Luis Obispo, CA. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain directional control during the landing roll, which resulted in a failure of the right main landing gear and subsequent ground loop. This summary draws on records from NTSB; 4 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On May 17, 2024, a Cessna 190 (N1500D) experienced a ground loop during landing roll at San Luis Obispo County Regional Airport after the right main landing gear axle attachment bolts fractured, causing substantial damage to the right wing; the pilot was uninjured.

Accident Overview

On May 17, 2024, about 1500 Pacific daylight time, a Cessna 190 airplane, registration N1500D, was substantially damaged during a ground loop while landing at San Luis Obispo County Regional Airport (SBP) in San Luis Obispo, California. The pilot, who was the sole occupant, was uninjured. The flight was operated under Title 14 Code of Federal Regulations Part 91 as a personal flight.

Sequence of Events

The pilot reported that during the landing roll on runway 29, the airplane's right main landing gear began to track under the fuselage. As the airplane slowed, directional control was lost, resulting in a ground loop. The right wing sustained substantial damage during the event.

Post-Accident Examination

After the accident, the pilot inspected the right main landing gear and discovered that the bolts attaching the axle to the main gear spring had fractured. The fractured bolts allowed the right main wheel assembly to separate from the main gear spring. The axle, tapered shim, and attachment bolt were collected and sent to the National Transportation Safety Board's Materials Laboratory in Washington, DC, for examination.

Laboratory Findings

The two fractured lower bolt shafts were retained within the axle. The tapered shim was bent and buckled outboard, downward, and slightly aft. Two curved witness marks were found near the lower edge of the tapered shim, aligned with hole features on the mating axle collar surface. The fractured bolt shafts exhibited a rough, matte gray fracture surface morphology. Radial features were observed emanating from a thread root at the upper edge of both bolts over a relatively flat fracture surface through approximately 40% of the bolt cross section. From that point, the fracture continued downward along an outboard and slightly aft slanted plane through the remainder of the bolt. The flat fracture surface at the top of the bolt was consistent with overstress fracture from a downward bending load before the final fracture in downward and slightly aft bending.

Contributing factors

PilotDirectional control — Not attained/maintained