ASN Wikibase Occurrence # 178174
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: | Friday 30 November 2007 |
Time: | 09:17 LT |
Type: | Aero Commander 500B |
Owner/operator: | Hicks & Lawrence Limited |
Registration: | C-GETK |
MSN: | 500B-1093-56 |
Year of manufacture: | 1961 |
Engine model: | Avco Lycoming IO-540-B1A5 |
Fatalities: | Fatalities: 0 / Occupants: 3 |
Aircraft damage: | Substantial |
Location: | 20 nm SW Armstrong, Ontario -
Canada
|
Phase: | En route |
Nature: | Passenger - Non-Scheduled/charter/Air Taxi |
Departure airport: | Dryden, Ontario |
Destination airport: | Geraldton, Ontario |
Investigating agency: | TSB |
Confidence Rating: | Information verified through data from accident investigation authorities |
Narrative:The flight was conducted under visual flight rules at 5500 feet above sea level with ambient temperatures aloft of -33°C. Approximately 40 minutes into the flight, the crew observed an abnormal right engine fuel flow indication. While troubleshooting the right engine, the engine rpm and fuel flow began to decrease and the crew diverted toward Armstrong, Ontario. A short time later, the left engine rpm and fuel flow began to decrease and the crew could no longer maintain level flight. At 0917 central standard time, the crew made a forced landing 20 nautical miles southwest of Armstrong, into a marshy wooded area. The captain sustained serious injuries and the co-pilot and passenger sustained minor injuries. The aircraft was substantially damaged. The crew and passenger were stabilized and transported to Thunder Bay, Ontario, for medical assistance.
Findings as to Causes and Contributing Factors
1.Suspended water in the fuel system precipitated out of solution and froze in the fuel distributor valve. This blocked the fuel supply to the fuel nozzles and led to the loss of engine power.
2.The aircraft was being operated without a fuel additive icing inhibiter. Use of such an additive would have inhibited ice formation in the aircraft's fuel system and would likely have prevented the fuel system blockage.
Findings as to Risk
1.The fuel distributor valve on the Aero Commander 500B is exposed directly to the cooling blast of the outside air, which under extremely cold conditions, can lead to the freezing of super-cooled water droplets present in the fuel stream.
2.The operator did not have procedures to describe how fuel additive icing inhibiter should be used during winter operations.
Accident investigation:
|
| |
Investigating agency: | TSB |
Report number: | A07C0225 |
Status: | Investigation completed |
Duration: | 6 months |
Download report: | Final report |
|
Sources:
http://www.tsb.gc.ca/eng/rapports-reports/aviation/2007/a07c0225/a07c0225.asp Revision history:
Date/time | Contributor | Updates |
01-Aug-2015 12:23 |
Aerossurance |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation