Aviation Accident Summaries

Aviation Accident Summary FTW94LA162

HENDERSON, NV, USA

Aircraft #1

N1349J

Rockwell 112A

Analysis

A GRADUAL DETERIORATION OF ENGINE POWER WAS EXPERIENCED DURING INITIAL TAKEOFF CLIMB. THE PILOT ATTEMPTED TO LAND ON A BUSY HIGHWAY, BUT WAS UNABLE DUE TO VEHICULAR TRAFFIC. THE AIRPLANE CONTINUED ALONGSIDE THE HIGHWAY AND TOUCHED DOWN ON THE SHOULDER OF THE ROADWAY WITH THE LANDING GEAR EXTENDED. THE REASON FOR THE LOSS OF ENGINE POWER COULD NOT BE DETERMINED.

Factual Information

On May 17, 1994, at 1645 Pacific daylight time, a Rockwell Commander 112A, N1349J, was substantially damaged during a forced landing near Henderson, Nevada. The private pilot and his two passengers were not injured. Visual meteorological conditions prevailed for the personal flight. According to the pilot, he departed runway 18 and a shallow right climbing turn was initiated after the gear was retracted. A 200 rpm loss was experienced and a gradual degradation of engine power was observed without any sign of vibration, detonation, backfiring or sputtering. The loss of power continued to the point where the airplane could not maintain altitude. The pilot elected to turn towards a busy highway, but had to veer away to avoid colliding with vehicles on the highway. The airplane touched down on the left shoulder of the roadway with the landing gear extended. Prior to coming to a stop on the desert floor, both main landing gears collapsed after impacting a drainage ditch. The reason for the loss of engine power could not be determined.

Probable Cause and Findings

THE PARTIAL LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

 

Source: NTSB Aviation Accident Database

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