Summary
On July 07, 2003, a Piper PA-38-112 (N569RA) was involved in an accident near Fort Smith, AR. The accident resulted in 1 minor injury. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this accident to be: The loss of engine power for undetermined reasons during the climb out. A factor was the ditch encountered during the forced landing.
On July 7, 2003, at 1745 central daylight time, a Piper PA-38-112, N569RA, piloted by a private pilot, sustained substantial damage during a forced landing after a reported in-flight loss of engine power, during initial climb from runway 25 (8,000 feet by 150 feet, asphalt) at Fort Smith Regional Airport, Fort Smith, Arkansas. The 14 CFR Part 91 personal flight was not on a flight plan. Visual meteorological conditions prevailed. The pilot reported minor injuries. The local personal flight was originating at the time of the accident.
The pilot reported: 1. Normal run up 2. Cleared for takeoff 3. Took off reached [approximately] 400 [feet above ground level] runway 25 4. Engine stopped no noticeable loss of power before engine stopped 5. Told tower aborting takeoff 6.
This accident is documented in NTSB report CHI03LA200. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N569RA.
Accident Details
Probable Cause and Findings
The loss of engine power for undetermined reasons during the climb out. A factor was the ditch encountered during the forced landing.
Aircraft Information
Registered Owner (Historical)
Analysis
On July 7, 2003, at 1745 central daylight time, a Piper PA-38-112, N569RA, piloted by a private pilot, sustained substantial damage during a forced landing after a reported in-flight loss of engine power, during initial climb from runway 25 (8,000 feet by 150 feet, asphalt) at Fort Smith Regional Airport, Fort Smith, Arkansas. The 14 CFR Part 91 personal flight was not on a flight plan. Visual meteorological conditions prevailed. The pilot reported minor injuries. The local personal flight was originating at the time of the accident.
The pilot reported:
1. Normal run up
2. Cleared for takeoff
3. Took off reached [approximately] 400 [feet above ground level] runway 25
4. Engine stopped no noticeable loss of power before engine stopped
5. Told tower aborting takeoff
6. Landed plane in field
7. Slid 300-350 ft swerved to miss berm
8. Nosed into ditch
9. Exited aircraft
10. Walked from aircraft and waited for help
A Federal Aviation Administration Inspector examined the wreckage. He stated that both fuel tanks were full. Both magnetos produced a spark when they were rotated. Engine continuity was established. He reported that no anomalies were detected.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI03LA200