Loss of Engine Power During IMC Flight

Casualties unknown • Cotulla, TX, US

A pilot reported a loss of left engine power and an inability to maintain altitude during a cross-country flight in instrument meteorological conditions.

What happened

During a daytime cross-country flight conducted in instrument meteorological conditions (IMC), the pilot reported that the left engine had lost power. Following this report, the pilot stated he was unable to maintain the airplane's altitude. Air traffic control provided the pilot with vectors toward the nearest airport.

As the aircraft descended, the pilot reported transitioning into visual meteorological conditions and indicated that the airport was in sight. However, no further communications were received from the pilot following that transmission.

The investigation

Initial measurements of the ground scar at the accident site were consistent with the dimensions of the nose, the right engine cowling, and the length of the right wing. The impact resulted in the nose and the leading edge of the right wing being crushed upward, to the right, and aft.

Investigators examined the fuel system and found that the main fuel tank capacity was 72 gallons. A maintenance entry indicated that auxiliary fuel cells had been disconnected, with lines capped and plugged, and placards were placed stating "DO NOT FILL AUX TANKS" and "AUX FUEL NOT AVAILABLE." An examination of the aircraft confirmed these auxiliary tanks were unusable.

The integrity of the fuel system was found to be intact, with confirmed continuity from the main tanks to both engines. Investigators found approximately 2 ounces of blue-colored fuel in the left main fuel sump, while five and one-half quarts of blue-colored fuel were drained from the right main fuel tank.

Mechanical inspections of the engines included manually rotating the crankshaft, which confirmed continuity from the crankshaft flange to the rear accessory case gears; thumb compression was present on all cylinders for both engines. The left propeller blades were found in the non-feather position against the stop locks and showed no evidence of rotation. A test run of the left engine revealed no discrepancies that would have prevented the engine from producing power prior to the accident.

Frequently asked questions

What happened in the 2000-10-10 Piper PA-23-160 accident near Cotulla, TX?

A pilot reported a loss of left engine power and an inability to maintain altitude during a cross-country flight in instrument meteorological conditions.

What aircraft was involved and where did it happen?

The accident on 2000-10-10 involved a Piper PA-23-160, registration N3390P, operated by Mesquite Flight Center, Inc.,, at Cotulla, TX.

What was the probable cause of the accident?

The pilot's failure to refuel the airplane which resulted in fuel exhaustion and subsequent loss of engine power. Also contributing to the accident was the pilot's failure to feather the engine.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22149. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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