Summary
On May 01, 2013, a Beech A36 (N1568Y) was involved in an incident near Ingalls, IN. All 1 person aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's improper fuel management, which resulted in a loss of engine power due to fuel starvation.
The pilot departed on a 1 hour and 50 minute cross country flight with approximately 30 gallons of fuel in each wing tank (approximately 27 gallons usable fuel per side). The flight was uneventful until he started a descent to land from 8,000 feet to 3,000 feet, when the engine made "two pops" and "quit." The pilot said there was no engine roughness "it just stopped." He made several attempts to re-start the engine, but was unsuccessful. The pilot declared an emergency and landed in a field. Upon landing, the nose gear dug into the dirt and separated from the airplane. The right wing rear spar had also fractured during the landing; however, both wing fuel tanks were undamaged.
This incident is documented in NTSB report CEN13CA250. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1568Y.
Accident Details
Probable Cause and Findings
The pilot's improper fuel management, which resulted in a loss of engine power due to fuel starvation.
Aircraft Information
Registered Owner (Historical)
Analysis
The pilot departed on a 1 hour and 50 minute cross country flight with approximately 30 gallons of fuel in each wing tank (approximately 27 gallons usable fuel per side). The flight was uneventful until he started a descent to land from 8,000 feet to 3,000 feet, when the engine made "two pops" and "quit." The pilot said there was no engine roughness "it just stopped." He made several attempts to re-start the engine, but was unsuccessful. The pilot declared an emergency and landed in a field. Upon landing, the nose gear dug into the dirt and separated from the airplane. The right wing rear spar had also fractured during the landing; however, both wing fuel tanks were undamaged. Approximately one-quart of fuel was drained from the left wing tank, and the right wing tank contained approximately 30 gallons of fuel. The pilot could not recall what the position of the fuel selector was at the time of the power loss. Examination of the engine and fuel system revealed no mechanical anomalies.
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13CA250