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WPR14FA226 · North American AT 6C

4 Jun 2014 · Buckley, WA, United States

North American AT 6C · Accident: loss of engine power (total) while maneuvering

From Cawleys South Prairie Airport (02WA) to Cawleys South Prairie Airport (02WA)

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Event

NTSB case
WPR14FA226
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
2 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

North American AT 6C

Aircraft type
North American AT-6
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N13372
Operator
Unknown
Onboard fatalities
Unknown
Route
From Cawleys South Prairie Airport (02WA), Buckley, WATo Cawleys South Prairie Airport (02WA), Buckley, WA
Aircraft age
About 58 years (built 1956)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of engine power (total)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Not determined › Not determined

Approximate · Coordinates from the NTSB case API, not marked as estimated; no uncertainty radius is established.

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.

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.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR14FA226
Event ID
20140604X00747
Case number
WPR14FA226
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: c8046e91d2536df2d4653fa06d59896866d18752925dddeba1380cccca746ec9; retrieved 2026-09-14T17:18:51.811Z.