Plane Crash List

North American AT 6C N13372

4 June 2014 · Buckley, Washington, United States · Fatal

Summary

On 4 June 2014 at about 22:30 local time, a North American AT 6C registered N13372 was involved in an accident near Buckley, Washington, United States. 2 people were on board and 2 died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:30
Classification
Accident
Location
Buckley, Washington, United States
Nearest airport
Cawleys South Prairie (02WA)
Coordinates
47.1753, -122.0858
Aircraft
North American AT 6C
Registration
N13372
Category
Airplane
Year built
1956
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Buckley → Buckley
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR14FA226

People

2 people died.

On board Died Serious Minor Uninjured
2 2 0 0 0

Probable cause

The loss of engine power during takeoff initial climb for reasons that could not be determined during a postaccident examination of the airplane.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The two airline transport pilots, one of whom had recently purchased the airplane from the other, departed for the local personal flight to familiarize the new owner, who was seated in the front seat, with the airplane. The airplane was equipped with dual flight controls; however, it could not be determined which pilot was manipulating the controls at the time of the accident. Review of a video provided by a witness showed the airplane take off, and the engine sounded normal. A witness reported that, shortly after the airplane passed the departure end of the runway, the engine began to "sputter." The airplane then initiated a right turn. Throughout the turn, the engine seemed to power up but then lose power shortly thereafter several times. As the airplane completed the turn to a heading toward the departure airport, the engine lost total power. The airplane then descended into trees. Postaccident examination of the airplane revealed that the right wing fuel line was connected to the fuel selector valve outlet port and that the engine fuel supply line was connected to the right fuel tank position of the fuel selector valve. The fuel selector valve was removed, disassembled, and found in the left tank position, slightly away from the detent; however, it could not be determined if the fuel selector valve was moved during the impact sequence. With the right wing fuel tank line and the engine supply fuel line installed as found and with the fuel selector valve positioned to either the left main or left reserve fuel tank positions, fuel could not flow from the left fuel tank to the engine, which would have resulted in a loss of engine power; however, fuel could flow from the left to the right fuel tank. If the selector valve was positioned to the right fuel tank position, fuel could flow to the engine. Examination of the fuel tanks at the accident site revealed that the left fuel tank contained fuel to a level that corresponded to the location of where the fuel tank was breached, and no fuel was observed within the right fuel tank. Based on the available evidence, it could not be determined if the incorrect installation of the selector valve fuel lines prevented fuel flow to the engine and the loss of engine power. The fuel selector valve position at the time of the accident could not be determined because it is possible that the valve moved during the impact sequence. Examination of the carburetor revealed that one of the carburetor floats was partially filled with liquid and that the other float was impact-damaged and separated from the carburetor; it could not be determined if the floats were filled with liquid before the accident. Although a float filled with liquid would allow the fuel flow into the carburetor float bowl to increase and one partially filled float would result in a slightly rich condition, if a rich fuel to air mixture had existed, additional signatures would have been present within the engine exhaust and spark plugs, all of which exhibited normal operating signatures. No additional anomalies were found that would have precluded normal operation of the engine. Autopsy and toxicology findings for the front seat pilot revealed that his heart was heavier than average, likely due to the effects of high blood pressure. However, it is unlikely that this condition or the medications that he was taking to treat it contributed to the accident. Autopsy and toxicology findings for the aft seat pilot revealed that he had significant coronary artery disease with up to 80 percent occlusion of the left anterior descending coronary artery, which would have increased his risk of impairment due to sudden onset symptoms, such as chest pain or irregular heart rhythms. However, the investigation was unable to determine if the aft seat pilot was having any such symptoms at or around the time of the accident. In addition, the aft seat pilot had been using sertraline to treat depression for 2 months before the accident, but the investigation was unable to determine the full extent of the pilot's depression or side effects from the medication. Although the aft seat pilot had coronary artery disease and depression, it is unlikely that these conditions contributed to the accident.

Quoted verbatim from the NTSB record.

Other North American AT-6C accidents

Date Aircraft Location Operator Outcome Died
11 Jun 2012 North American AT-6C
N7055K
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20 Feb 2010 North American AT-6C
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7 Dec 2006 North American AT-6C
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14 Apr 2005 North American AT-6C
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26 Mar 2005 North American AT-6C
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All 10 records for this type

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All 170,864 records in United States