No fatalities

2 Aug 2012: BEECH E-55 (N3644A) — Houston, TX

Houston, TX, United States

On 2 Aug 2012, a BEECH E-55 (registration N3644A) was involved in an aviation accident near Houston, TX. No fatalities were reported. Investigators recorded the probable cause as: A damaged ignition harness, which resulted in a partial loss of engine power. This summary draws on records from NTSB; 8 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On August 2, 2012, a Beech E-55 (N3644A) struck a road embankment after an aborted takeoff due to left engine power loss at West Houston Airport; pilot and passenger uninjured, substantial damage to left wing.

Accident Overview

On August 2, 2012, at approximately 1028 central daylight time, a Beech E-55, registration N3644A, sustained substantial damage when it struck a road embankment following an aborted takeoff. The incident occurred at West Houston Airport in Houston, Texas. The pilot and his passenger were not injured. The airplane sustained substantial damage to the left wing.

Flight Details

The aircraft was owned and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and the flight was not operated on a flight plan. The local flight was originating at the time of the accident.

Pilot Report

The pilot reported that during the initial portion of the takeoff, the engines accelerated smoothly and all systems and gauges indicated normal operation. As the airplane accelerated, the pilot noticed roughness in performance and verified that the throttle, mixture, and propeller controls for both engines were forward. Due to the roughness and a perceived loss of engine power on one engine, the pilot aborted the takeoff. There was insufficient runway remaining to stop the airplane; it went off the end of the runway and struck an embankment that bordered the airport perimeter road.

Postaccident Examination

Postaccident examination of the airplane's left engine revealed damage to two of the six spark plug leads. The engine was mounted on a test stand, and during a subsequent test run, it exhibited rough operation. The damaged ignition harness was replaced with the harness from the right engine, and the test run was repeated. During the second test run, the engine started immediately and ran through various power settings with no hesitations, stumbling, or interruptions in power. The reason for the damage to the ignition harness could not be determined.

Maintenance History

The most recent annual inspection of the airplane was completed on July 16, 2012.

Contributing factors

Damaged/degraded