Summary
On May 17, 1994, a Rockwell 112A (N1349J) was involved in an incident near Henderson, NV. All 3 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: THE PARTIAL LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.
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According to the pilot, he departed runway 18 and a shallow right climbing turn was initiated after the gear was retracted.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.
This incident is documented in NTSB report FTW94LA162. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1349J.
Accident Details
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.
Aircraft Information
Registered Owner (Historical)
Analysis
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According to the pilot, he departed runway 18 and a shallow right climbing turn was initiated after the gear was retracted.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.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA162