PIPER PA-28-140 near Guthrie, OK — 2011-10-16
- Date
- 2011-10-16
- Location
- Guthrie, OK, USA
- Aircraft
- PIPER PA-28-140
- Registration
- N6085W
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Descent
Probable cause
The pilot’s inadequate fuel planning, which resulted in a total loss of engine power due to fuel exhaustion.
NTSB narrative
The airplane was fueled to capacity and flew for 3 hours and 15 minutes to its destination, where it was not refueled. Two days later, the airplane flew for 3 additional hours. During that flight, a passenger said that he heard the pilot say that they were low on fuel. Shortly thereafter, the engine lost power and the airplane collided with power lines and impacted a storage shed in a residential area. The airplane was equipped with two 25-gallon fuel tanks (50 gallons total, of which 48 gallons were useable). The airplane had been aloft for about 6 hours, 13 minutes. Depending on the power setting, the airplane would have burned between 38 and 52 gallons for the two flights.
Analysis
- Primary failure mode
- Fuel management
- First missed decision gate
- Pilot did not refuel before departing K3MO, leading to low fuel situation.
NTSB coding
Evidence available
- Photos
- 18 docket documents
Docket documents18
- NTSB Form 6120.15, Release of Aircraft Wreckageform
- Performance Chartsform
- Record of Telephone Interviewinterview
- Certification of Party Representativesother
- Map 1 - Over view of the accident site.other
- Map 2 - Guthrie Airport was 2-3 miles southwest of the accident site.other
- Map 3 - Close-up view of the accident site and the storage shed struck by N6085W.other
- Photo 1 - Repaired powerlines and poles that were struck by N6085Wphotos
- Photo 2 - N6085W at the accident and minor damage to the storage shedphotos
- Photo 3 - There was minor damage to the parked pick-up truckphotos
- Photo 4 - Propeller spinner exhibiting crushing damage on one side and the absenceof spiralling striationsphotos
- Photo 5 - Ascending propeller blade exhibiting faint 45-degree striations on the cambered surface of the polished aluminum alloy bladephotos
- Photo 6 - Descending propeller blade is bent slightly aftphotos
- Photo 7 - Pilot's instrument panel with electric fuel boost pump (red switch) in the ON positionphotos
- Photo 8 - Fuel selector was positioned on left fuel tankphotos
- Photo 9 - Flap handle was in the retracted positionphotos
- Toxicology Reports, Darrell A. Smittlereport
- Weather Reports and Recordsreport
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