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|
Attributes | |
ACN | 1326435 |
Time | |
Date | 201601 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Baron 55/Cochise |
Operating Under FAR Part | Part 91 |
Flight Phase | Descent |
Route In Use | Vectors |
Flight Plan | IFR |
Component | |
Aircraft Component | Fuel Selector |
Person 1 | |
Function | Pilot Flying Single Pilot |
Qualification | Flight Crew Instrument Flight Crew Multiengine |
Experience | Flight Crew Last 90 Days 300 Flight Crew Total 22000 Flight Crew Type 800 |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Published Material / Policy Inflight Event / Encounter Fuel Issue |
Narrative:
During practice approach; was receiving vectors on the downwind for ILS. Knowing fob [fuel on board] to be limited (checked visually and measured with shading prior to flight); selected auxiliary tanks in downwind cruise to optimize burn. After approximately 3 minutes; the right (#2) engine began losing power; with fuel flow fluctuations. Based on previous experience; I immediately selected main tank; expecting the engine to not lose power at all. However; the #2 did not regain power; and after about 20 seconds; I elected to land from the downwind; [after notifying ATC]. On base leg; was switched to tower; and feathered the #2 engine. Turned final; completed an uneventful single engine landing and taxied clear of [the runway]. As I suspected; the auxiliary tank; upon fueling was empty. However; the main tank had approximately 17 gallons; with a total of 34 (1hour 30 min endurance) gallons on board. I am having my mechanic check the fuel valve.
Original NASA ASRS Text
Title: The pilot of a BE-55 reported a loss of power to one engine after switching fuel tanks. After switching back to the main tank; engine did not recover; so it was feathered; followed by a successful landing.
Narrative: During practice approach; was receiving vectors on the downwind for ILS. Knowing FOB [fuel on board] to be limited (checked visually and measured with Shading prior to flight); selected AUX tanks in downwind cruise to optimize burn. After approximately 3 minutes; the right (#2) engine began losing power; with fuel flow fluctuations. Based on previous experience; I immediately selected main tank; expecting the engine to not lose power at all. However; the #2 did not regain power; and after about 20 seconds; I elected to land from the downwind; [after notifying ATC]. On base leg; was switched to Tower; and feathered the #2 engine. Turned final; completed an uneventful single engine landing and taxied clear of [the runway]. As I suspected; the AUX tank; upon fueling was empty. However; the main tank had approximately 17 gallons; with a total of 34 (1hour 30 min endurance) gallons on board. I am having my mechanic check the fuel valve.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.