Accident Lancair IV N1126V,
ASN logo
ASN Wikibase Occurrence # 148783
 
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 6 September 2012
Time:12:45
Type:Silhouette image of generic LNC4 model; specific model in this crash may look slightly different    
Lancair IV
Owner/operator:Private
Registration: N1126V
MSN: L2K289
Engine model:Continental TSIO-550-E1B
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Winnsboro Municipal Airport - F89, Winnsboro, LA -   United States of America
Phase: Landing
Nature:Test
Departure airport:Winnsboro, LA (F89)
Destination airport:Winnsboro, LA (F89)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The airline transport pilot was landing the airplane after a local test flight that involved calibrating the fuel system. According to several witnesses, they heard an increase in engine rpm consistent with the pilot adding power to perform a go-around. Several witnesses reported hearing a subsequent loss of engine power. The nose of the airplane rose and then dropped. The airplane was substantially damaged when it impacted terrain beyond the departure end of the runway. The damage to the airplane and the resultant ground scars were consistent with the airplane being in a stalled condition at the time of the accident. An examination of the airframe and engine revealed no anomalies that would have precluded normal operation. An examination of the fuel system revealed that the fuel selector was stiff and difficult to rotate. Further examination revealed that the O-rings on the fuel selector valve’s internal spindle were swollen past the plane of the shaft of the spindle, preventing easy rotation. The pilot was aware of the fuel selector valve anomaly; however, a service bulletin addressing the problem with the fuel selector O-rings had not yet been complied with. The fuel blighting evidence at the accident site and the quantity of fuel found in the right fuel tank suggest that the right wing contained fuel at the time of impact. Based on the circumstances of the accident, it is most likely that the engine lost power due to fuel starvation during the go-around with the fuel selector valve positioned to the left tank, and the pilot became distracted when he tried to switch fuel tanks and lost control of the airplane.

Toxicological testing revealed the presence of antidepressant and cardiac medications in the pilot’s system. The blood level of the antidepressant medication was higher than usual therapeutic levels, indicating a high dose and prolonged use. The antidepressant medication in the pilot’s system comes with the warning that it may impair mental and/or physical abilities required for the performance of potentially hazardous tasks. In addition, depression is associated with significant cognitive degradation.

A review of the pilot’s medical records revealed an extensive history of psychiatric and cardiac issues and subsequent difficulties obtaining a medical certificate for flight. Before the pilot’s most recent medical certification exam, he provided the Federal Aviation Administration (FAA) medical examiner with documentation indicating that he was no longer taking antidepressants. Required standardized neuropsychological testing placed the pilot at average, below average, or mildly impaired when compared with other (somewhat younger) pilots. Based on the levels of antidepressant medication in the pilot’s system, the pilot likely knowingly misreported his medication use to the FAA when he applied for his medical certificate. The pilot’s underlying depression, personality disorder, cognitive issues, and medication use likely contributed to his unwillingness to address the airplane’s fuel selector valve problem. In addition, these conditions would have adversely affected the pilot’s ability to maintain control of the airplane in an emergency.
Probable Cause: The pilot’s failure to maintain control of the airplane after a loss of engine power during a go-around. Contributing to the accident was the difficult-to-operate fuel selector valve and the pilot’s continued operation of the airplane with a known mechanical anomaly. Also contributing to the accident was the pilot’s depression, personality disorder, cognitive issues, and medication use, which adversely affected his ability to maintain control of the airplane during the emergency and likely affected his decision not to address the airplane’s fuel selector valve problem.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN12FA611
Status: Investigation completed
Duration: 1 year
Download report: Final report

Sources:

NTSB
FAA register: http://www.thenewsstar.com/article/20120907/NEWS01/209070323/1-killed-Franklin-Parish-plan-crash?odyssey=mod%7Cnewswell%7Ctext%7CFRONTPAGE%7Cp&nclick_check=1
http://www.myarklamiss.com/fulltext?nxd_id=160192
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=1126V

Location

Revision history:

Date/timeContributorUpdates
07-Sep-2012 01:39 gerard57 Added
07-Sep-2012 02:57 gerard57 Updated [Aircraft type, Source, Narrative]
07-Sep-2012 07:27 Geno Updated [Time, Registration, Cn, Location, Source, Narrative]
07-Sep-2012 14:09 Alpine Flight Updated [Destination airport, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
28-Nov-2017 13:25 ASN Update Bot Updated [Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org