ASN Wikibase Occurrence # 45034
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: | Tuesday 28 October 2003 |
Time: | 14:50 |
Type: | North American T-28B |
Owner/operator: | Private |
Registration: | N28AF |
MSN: | 138321 |
Total airframe hrs: | 15120 hours |
Fatalities: | Fatalities: 1 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | Hornbrook, CA -
United States of America
|
Phase: | Approach |
Nature: | Training |
Departure airport: | Montague, CA (SIY) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The airplane collided with trees during a forced landing following a loss engine power. Witnesses reported that smoke was trailing from the airplane just before it hit the trees. One witness said that the engine was sputtering, and he heard a couple of "bangs." As the airplane turned to line up with a clear landing area it clipped the tops of some trees and crashed on an embankment adjacent to a dirt road. The owner of a fixed base operator received flight instruction from the certified flight instructor (CFI) in the accident airplane immediately before the accident flight, and noted no mechanical discrepancies. Fifteen minutes later, witnesses watched the airplane takeoff on the accident flight, and reported that the airplane and engine looked and sounded normal. A Federal Aviation Administration (FAA) inspector examined the wreckage on scene and found a significant amount of oil on the right side of the airplane aft of the firewall. The engine separated from the airplane, and came to rest about 15 feet upslope from the wreckage. He noted heavy oil deposits on the bottom cylinders and accessories; the top cylinders were clean. Oil coated the accessory section of the engine. The area around the pre-oil port fitting on the accessory section of the engine was saturated in oil, and the B-nut for that oil line to fitting connection was only finger tight. An examination of the engine revealed damage and thermal distress signatures consistent with an oil starvation catastrophic failure, with no oil present inside the engine. A maintenance logbook entry noted that maintenance technicians had replaced all flexible engine hoses 21 hours prior to the accident.
Probable Cause: a catastrophic engine failure from oil exhaustion due to inadequate maintenance installation of the lubricating system hoses.
Sources:
NTSB:
https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20031110X01880&key=1 Location
Revision history:
Date/time | Contributor | Updates |
28-Oct-2008 00:45 |
ASN archive |
Added |
21-Dec-2016 19:24 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
08-Dec-2017 20:01 |
ASN Update Bot |
Updated [Operator, Source, Narrative] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation