ASN Wikibase Occurrence # 167755
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: | Thursday 3 July 2014 |
Time: | 18:46 |
Type: | Cessna 336 Skymaster |
Owner/operator: | Mobile County Health Department |
Registration: | N3804U |
MSN: | 336-0104 |
Year of manufacture: | 1964 |
Total airframe hrs: | 3151 hours |
Engine model: | Continental IO-360 SER |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | McDuffie Island, south Mobile, AL -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Agricultural |
Departure airport: | St. Elmo, AL (2R5) |
Destination airport: | St. Elmo, AL (2R5) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot reported that he was performing mosquito control spraying operations at 100 ft above ground level (agl) when the rear engine began to sputter and lose power. He switched to the auxiliary fuel tank; however, this did not remedy the situation. He then climbed the airplane to 500 ft agl and continued to troubleshoot the problem by again switching fuel tanks and turning the electric boost pumps on. Shortly thereafter, the front engine began to lose power. Unable to regain full power on both engines, the pilot chose to perform a forced landing in an open field. The airplane touched down on soft soil and stopped abruptly, which resulted in extensive damage to the airplane.
Both fuel selectors were found in the right main fuel tank positions. An examination of the fuel system revealed that the main fuel tanks contained only residual fuel and that the auxiliary tanks contained an adequate amount of fuel. Examination of the fuel lines revealed that both supply lines from the gascolators to the engine-driven fuel pumps were contaminated and obstructed with a granular, powder-like substance. The engines ran normally when operated in a test cell after the accident.
The auxiliary fuel tanks were designed for level, cruise flight only. The auxiliary tanks fed directly to the fuel selector and had no boost pumps available. It is likely that, due to the fuel system’s design, adequate fuel pressure could not be regained once the main tanks were depleted and the pilot switched to the auxiliary tanks. The contamination in the fuel lines might have further restricted fuel flow to the engines. The loss of engine power might have been prevented if the pilot had maintained an adequate amount of fuel in the main tanks.
Probable Cause: The pilot’s inadequate preflight fuel planning during which he did not ensure that there was adequate fuel in the main tanks for the flight, which resulted in a loss of engine power.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | ERA14TA326 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB
FAA register:
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=3804U Location
Revision history:
Date/time | Contributor | Updates |
04-Jul-2014 05:02 |
Geno |
Added |
24-Jul-2014 23:03 |
Geno |
Updated [Time, Departure airport, Destination airport, Source, Narrative] |
21-Dec-2016 19:28 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
30-Nov-2017 18:52 |
ASN Update Bot |
Updated [Operator, 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