Fuel exhaustion Accident American Aviation AA-1A Trainer N6343L,
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ASN Wikibase Occurrence # 193746
 
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Date:Tuesday 21 February 2017
Time:00:20
Type:Silhouette image of generic AA1 model; specific model in this crash may look slightly different    
American Aviation AA-1A Trainer
Owner/operator:Private
Registration: N6343L
MSN: AA1A-0343
Year of manufacture:1972
Engine model:Lycoming O-235-C2C
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Gainesville Municipal Airport (KGLE), Gainesville, TX -   United States of America
Phase: Landing
Nature:Private
Departure airport:Sherman/denison, TX (GYI)
Destination airport:Gainesville, TX (GLE)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The private pilot was conducting a familiarization flight with the non-pilot-rated passenger, who had recently purchased the airplane. They flew to a nearby airport to practice touch-and-go landings. After completing about 15 landings, they proceeded to another airport to get fuel. About 5 minutes before reaching the airport, the passenger noticed that the fuel pressure gauge indicated 0 psi, but the engine was operating smoothly. The pilot turned on the electric fuel boost pump and the fuel pressure gauge returned to 5 psi. The boost pump remained on for the remainder of the flight. Upon arrival at the airport, a go-around was performed. The engine experienced a loss of power during the climb about 200 ft above ground level and he performed a forced landing to a field short of the runway.  
Postaccident fuel consumption calculations revealed that the airplane likely contained about 1 gallon of fuel at the time of the accident, which would have been unusable. Examination of the fuel tanks revealed less than 1 cup of fuel in the left tank and no fuel remaining in the right tank. The fuel spill observed at the accident site by first responders was likely the 1 gallon of unusable fuel from the right tank, because the right wing was separated at the fuselage and its fuel line was fractured. No anomalies were noted with the engine and the propeller blades did not show any rotational signatures.
Although the pilot reported that he flew the airplane during the final approach and go-around, there were discrepancies in his statements that suggested that the non-pilot rated passenger was actually manipulating the airplane controls during the loss of engine power.

Probable Cause: The pilot’s inadequate preflight and inflight fuel planning, which resulted in a total loss of engine power due to fuel exhaustion and subsequent forced landing in a field. Contributing to the accident was the pilot’s delayed action in taking control of the airplane following the loss of engine power.  

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN17LA105
Status: Investigation completed
Duration: 1 year and 4 months
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?nNumberTxt=6343L

Location

Images:


Photo: NTSB

Revision history:

Date/timeContributorUpdates
22-Feb-2017 04:09 Geno Added
08-Jul-2018 13:16 ASN Update Bot Updated [Time, Total occupants, Nature, Departure airport, Destination airport, Source, Narrative]
08-Jul-2018 13:52 harro Updated [Source, Narrative, Photo, ]

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