What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Engine quit on climbout. Tried return. Crashed half mile short. Report shows fuel depletion or fuel contamination. (.4) the airplane's engine lost power during the initial climb after departure, and the pilot performed a 180-degree turn back towards the airport, but landed short of the runway. The airplane was equipped with a hand operated emergency fuel pump, which was part of the fuel selector valve. The emergency procedures section of the POH states that the emergency hand pump should be used to restore fuel pressure in the event of an engine driven pump failure. The pilot stated that he never attempted to use the emergency hand fuel pump. An on-scene examination revealed fuel in both main tanks. Examination of the engine driven lear-romec fuel pump coupling found it had sheared and separated. Internal examination of the pump revealed bluing of the steel pump vane tips and galling of the pump liner. According to the manufacturer, the pump at some time had been operated without fuel, which cools the vanes, and had overheated. Metallurgical examination of the failed fuel pump coupling revealed that it separated due to ductile torsional overstress at a designed location. Ac cording to records available, the pump had accumulated about 619 hours since overhaul with an unknown total time. (-23) on climbout acft engine started to run rough before it quit. Attempted to return to field and crashed 1/2 mile west of Auburn airport.
As the FAA filed it
ENGINE QUIT ON CLIMBOUT. TRIED RETURN. CRASHED HALF MILE SHORT. REPORT SHOWS FUEL DEPLETION OR FUEL CONTAMINATION. (.4) THE AIRPLANE'S ENGINE LOST POWER DURING THE INITIAL CLIMB AFTER DEPARTURE, AND THE PILOT PERFORMED A 180-DEGREE TURN BACK TOWARDS THE AIRPORT, BUT LANDED SHORT OF THE RUNWAY. THE AIRPLANE WAS EQUIPPED WITH A HAND OPERATED EMERGENCY FUEL PUMP, WHICH WAS PART OF THE FUEL SELECTOR VALVE. THE EMERGENCY PROCEDURES SECTION OF THE POH STATES THAT THE EMERGENCY HAND PUMP SHOULD BE USED TO RESTORE FUEL PRESSURE IN THE EVENT OF AN ENGINE DRIVEN PUMP FAILURE. THE PILOT STATED THAT HE NEVER ATTEMPTED TO USE THE EMERGENCY HAND FUEL PUMP. AN ON-SCENE EXAMINATION REVEALED FUEL IN BOTH MAIN TANKS. EXAMINATION OF THE ENGINE DRIVEN LEAR-ROMEC FUEL PUMP COUPLING FOUND IT HAD SHEARED AND SEPARATED. INTERNAL EXAMINATION OF THE PUMP REVEALED BLUING OF THE STEEL PUMP VANE TIPS AND GALLING OF THE PUMP LINER. ACCORDING TO THE MANUFACTURER, THE PUMP AT SOME TIME HAD BEEN OPERATED WITHOUT FUEL, WHICH COOLS THE VANES, AND HAD OVERHEATED. METALLURGICAL EXAMINATION OF THE FAILED FUEL PUMP COUPLING REVEALED THAT IT SEPARATED DUE TO DUCTILE TORSIONAL OVERSTRESS AT A DESIGNED LOCATION. AC CORDING TO RECORDS AVAILABLE, THE PUMP HAD ACCUMULATED ABOUT 619 HOURS SINCE OVERHAUL WITH AN UNKNOWN TOTAL TIME. (-23) ON CLIMBOUT ACFT ENGINE STARTED TO RUN ROUGH BEFORE IT QUIT. ATTEMPTED TO RETURN TO FIELD AND CRASHED 1/2 MILE WEST OF AUBURN AIRPORT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N8597A · 1
Matched to the same aircraft by N-number and date.