No fatalities

11 Jun 2015: BEECH E33A (N8401N) — Tucson, AZ

Tucson, AZ, United States

On 11 Jun 2015, a BEECH E33A (registration N8401N) was involved in an aviation accident near Tucson, AZ. No fatalities were reported. Investigators recorded the probable cause as: A loss of left braking action for reasons that could not be determined because postaccident examination did not reveal any evidence of preimpact mechanical failures or malfunctions that would have precluded normal operation, which resulted in a loss of… This summary draws on records from NTSB; 2 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On June 11, 2015, a Beech E33A (N8401N) exited the runway during landing rollout at La Cholla Airpark, Tucson, Arizona, and collided with a drainage ditch. The pilot reported left brake failure; inspection found no mechanical malfunction but a sheared bleeder valve.

Accident Overview

On June 11, 2015, at approximately 0840 mountain standard time, a Beech E33A aircraft, registration N8401N, was involved in a runway excursion during landing at La Cholla Airpark in Tucson, Arizona. The aircraft subsequently collided with a drainage ditch. The commercial pilot, who was also the owner, was operating the airplane under 14 Code of Federal Regulations Part 91 for a local personal flight. The flight had departed Tucson around 0800. Visual meteorological conditions prevailed, and no flight plan was filed. The pilot was not injured, but the airplane sustained substantial damage.

Pilot Report

According to a written statement from the pilot, the landing touchdown was smooth with power nearly off. During the landing roll, the pilot applied gentle pressure to the brakes to slow down. However, the left-side braking action was non-existent, while the right-side brake held. The pilot was unable to maintain directional control, causing the airplane to depart the narrow runway and collide with a drainage ditch and a low cement wall.

Post-Accident Examination

The wreckage was recovered to a secured facility, where a Federal Aviation Administration Inspector from the Scottsdale, Arizona, Flight Standards District Office examined the brake system. The inspector reported no evidence of a mechanical malfunction or failure. However, the hydraulic system was almost empty because the bleeder valve on the brake caliper had been sheared off.

Contributing factors

Contributed to outcome