ASN Wikibase Occurrence # 173450
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Date: | Saturday 24 January 2015 |
Time: | 17:44 |
Type: | Cessna 150E |
Owner/operator: | Brian Vowell |
Registration: | N4017U |
MSN: | 15061417 |
Year of manufacture: | 1965 |
Total airframe hrs: | 8769 hours |
Engine model: | Continental O-200 SERIES |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Near Silver Springs Airport (KSPZ), Silver Springs, AZ -
United States of America
|
Phase: | Landing |
Nature: | Private |
Departure airport: | San Carlos, CA (SQL) |
Destination airport: | Silver Springs, NV (SPZ) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot reported that, before takeoff for the cross-country flight, the airplane had been topped off with fuel and had a total of 24 gallons onboard. During the descent for landing, the engine lost power. The pilot adjusted the mixture and throttle controls, and the engine regained power. About 10 to 15 minutes later, while continuing the descent, he noted that both fuel gauges indicated about one-quarter of a tank of fuel. Shortly after, the engine again lost power. The pilot’s attempts to restart the engine were unsuccessful. The airplane was unable to reach the runway, and the pilot landed the airplane in an open field adjacent to the airport. During the landing roll, the airplane struck the airport perimeter fence and came to rest upright.
Immediately following the accident, no evidence of any fuel leaks was observed. The airplane was left unattended until the following day, at which time, about 2 quarts of fuel was removed from the left wing fuel tank, and about 1 quart of fuel was removed from the right wing fuel tank. No fuel was present within the airframe fuel strainer. Performance calculations indicated that, if proper leaning procedures were used, the flight would have required about 17.5 gallons of fuel and that about 5 gallons of usable fuel should have been remaining after the airplane reached its destination. The investigation was unable to determine why so little fuel remained in the airplane after the accident. After the airplane was recovered, an alternate fuel source was plumbed to the left wing inlet line. The engine successfully started; due to damage sustained to the propeller, the engine was run at a reduced power setting, and it ran for 5 minutes. The reason for the loss of engine power could not be determined.
Probable Cause: The loss of engine power for reasons that could not be determined during a postaccident examination of the airplane.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | WPR15LA090 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB
FAA register:
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N4017U Location
Revision history:
Date/time | Contributor | Updates |
30-Jan-2015 23:47 |
Geno |
Added |
21-Dec-2016 19:28 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
01-Dec-2017 11:48 |
ASN Update Bot |
Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative] |
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