No fatalities

Landing Gear Malfunction Leads to Gear Collapse for Cessna 210B in Bullhead City (N9578X)

Bullhead City, AZ, United States

On November 8, 2014, a CESSNA 210B (registration N9578X) operated by TRISTATE CAREFLIGHT LLC was involved in an aviation accident near Bullhead City, AZ. No fatalities were reported. Investigators recorded the probable cause as: The failure of the landing gear actuator housing during landing for reasons that could not be determined based on the available evidence. This summary draws on records from NTSB; 13 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

On November 7, 2014, a Cessna 210B experienced a landing gear malfunction after takeoff from Bullhead City, Arizona. The pilot and three passengers were uninjured, but the aircraft sustained substantial damage to the horizontal stabilizer during the subsequent landing.

Introduction

On November 7, 2014, at 1730 mountain standard time, a Cessna 210B (registration N9578X) experienced a landing gear malfunction shortly after departing from Laughlin/Bullhead International Airport in Bullhead City, Arizona. The flight, operated by Tristate Careflight LLC under 14 Code of Federal Regulations Part 91, was conducted in visual meteorological conditions without a filed flight plan.

Sequence of Events

The pilot reported that after takeoff, while moving the landing gear handle to the UP position, a loud bang was heard. The landing gear indication lights did not illuminate. The pilot cycled the landing gear handle, but no effect was observed. Additionally, the flaps became inoperative. During a low pass over the airport, the tower informed the pilot that the landing gear were in a transit position—neither fully retracted nor locked down. The pilot attempted the emergency gear extension procedure, but it was unsuccessful.

Upon landing, the gear completely collapsed. The airplane slid to a stop on its belly and tipped to the left, resulting in damage to the left horizontal stabilizer.

Damage and Examination

The aircraft sustained substantial damage to the horizontal stabilizer during the landing. The pilot stated that an airframe and power plant mechanic visually examined the landing gear actuator and noted that the actuator housing had split, which allowed the loss of hydraulic system pressure. No further examination was conducted, and the reason for the housing failure was not determined.

Contributing factors

Landing gear actuator — Failure