ASN Wikibase Occurrence # 2372
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Wednesday 20 February 2008 |
Time: | 11:19 |
Type: | Raytheon Beechcraft A36 Bonanza |
Owner/operator: | Private |
Registration: | N36GJ |
MSN: | E-3020 |
Total airframe hrs: | 1250 hours |
Engine model: | Continental IO-550 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | 5 miles east of the Palm Beach County Glades Airport, Pahokee, FL -
United States of America
|
Phase: | Initial climb |
Nature: | Private |
Departure airport: | Pahokee, FL (PHK) |
Destination airport: | New Orleans, LA (NEW) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:Prior to the accident flight and shortly after departure, the airplane's engine began to "surge." The pilot was able to divert to a nearby airport, and landed uneventfully. After landing, the pilot examined the engine, and checked the fuel system for leaks or contamination. He observed no anomalies and decided to depart again, after performing a run-up inspection. After departure, when the airplane was about 9 miles from the airport, and an altitude of about 2,000 feet, the engine lost power. The pilot prepared for a forced landing, and attempted unsuccessfully to restart the engine by switching fuel tanks and turning on the fuel boost pump. The airplane touched down in a field, the landing gear "dug in," and the airplane nosed down, substantially damaging the firewall. Examination of the engine revealed the engine-driven fuel pump vane cavity displayed rust and corrosion. The cavity was rinsed with a mixture of aviation gasoline and penetrating oil, and the pump was then able to rotate. It was reassembled for a functional test, and produced both low and high-end pressures without any anomalies. The fuel pump had been documented as being overhauled and then installed about 2 months prior to the accident and had accumulated 12 hours since installation.
Probable Cause: The pilot's decision to depart with a known deficiency with the engine, which resulted in a loss of engine power. Contributing to the accident was the loss of engine power due to the failure of the engine-driven fuel pump.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | NYC08LA106 |
Status: | Investigation completed |
Duration: | 1 year and 2 months |
Download report: | Final report |
|
Sources:
NTSB
Location
Revision history:
Date/time | Contributor | Updates |
20-Feb-2008 21:05 |
Fusko |
Added |
21-Dec-2016 19:13 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
21-Dec-2016 19:14 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
21-Dec-2016 19:16 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
21-Dec-2016 19:20 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
03-Dec-2017 09:35 |
ASN Update Bot |
Updated [Other fatalities, Departure airport, Destination airport, Source, Narrative] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation