No fatalities

2013-07-05: Rockwell Sabreliner 65 (XB-RSC) — Eseasa Construcciones — Las Vegas-Harry Reid (McCarran), United States of America

Las Vegas-Harry Reid (McCarran), United States of AmericaLanding (descent or approach)

On July 5, 2013, a Rockwell Sabreliner 65 (registration XB-RSC) operated by Eseasa Construcciones was involved in an aviation accident near Las Vegas-Harry Reid (McCarran), United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilots' failure to follow the airplane manufacturer's emergency procedures for a hydraulic system failure and emergency braking, which resulted in the loss of braking action upon landing and the subsequent loss of directional control while turning off the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781194111Data APIEditorial standards

During approach, main hydraulic system lost pressure. Pilots used auxiliary system and emergency gear extension but did not follow proper procedures, leading to brake accumulator depletion, loss of braking and steering, and collision with a metal beam after turning off the runway.

Incident Overview

During the approach, the main hydraulic system lost pressure. The pilots selected the auxiliary hydraulic system on, continued the approach, and extended the landing gear using the emergency landing gear extension procedures. During the landing roll, about two-thirds down the runway, the pilots noticed abnormal brake operation and then turned onto a taxiway to clear the runway. Once on the taxiway, the captain was unable to stop or steer the airplane. It proceeded across a parallel runway and into an adjacent field, where it struck a metal beam.

Postaccident Examination

Postaccident examination revealed brake system continuity with cockpit controls. Tires, brake assemblies, and brake pads were intact and undamaged. Hydraulic lines from the pump to wheel brakes were intact. No hydraulic fluid leaks were observed. The hydraulic fluid reservoir was about one-quarter full. Testing of the two hydraulic pumps showed they were functional, and no mechanical failures or anomalies that would preclude normal operation were noted.

Hydraulic System Emergency Procedures

The airplane's hydraulic system failure emergency procedures state that if hydraulic pressure is lost, the electrically driven hydraulic pump should be reset. If pressure is not restored, the primary hydraulic system should be disengaged and the landing gear lowered using emergency extension procedures. After gear extension, the auxiliary hydraulic system should be selected on for landing. However, the pilots stated they did not attempt to reset the electric hydraulic pump and performed the emergency gear extension with the auxiliary hydraulic pump engaged. It is likely that failing to select the auxiliary system off before gear extension caused hydraulic pressure in the auxiliary system to dissipate, leaving only the emergency brake accumulator for braking. The number of emergency brake applications depends on accumulator charge, which may deplete quickly.

Emergency Braking and Runway Exit

The emergency braking procedures state that as soon as the airplane is safely stopped, pilots should request towing assistance. However, the pilots did not stop on the runway despite about 3,900 ft remaining; instead, they turned off at an intersection, resulting in loss of directional control.

Probable cause

The pilots' failure to follow the airplane manufacturer's emergency procedures for a hydraulic system failure and emergency braking, which resulted in the loss of braking action upon landing and the subsequent loss of directional control while turning off the runway. Contributing to the accident was the loss of hydraulic pressure for reasons that could not be determined because postaccident testing and examination of the hydraulic system revealed no mechanical failures or anomalies that would have precluded normal operation.