Engine failure and loss of control during initial climb

Casualties unknown • Opa-locka, FL, US

An aircraft experienced engine roughness and a sudden loss of control during its initial climb, resulting in a ground impact.

What happened

The aircraft had been parked for at least 16 days with the inboard fuel tanks approximately one-third full. On the day of the accident, the tanks were refilled. Shortly after departure, the flight returned to the airport, reporting that the flaps were non-operational and the landing gear would not retract.

During the initial climb following the subsequent departure, the pilot notified the air traffic controller of a rough running engine. The aircraft was then observed to bank to the left and pitch its nose downward before impacting the ground. There were no injuries reported.

The investigation

Investigators found water at the fuel injector nozzles and the fuel manifold assembly of several cylinders within the left engine. However, inspections of other aircraft fueled from the same source showed no evidence of water contamination.

A mechanic who had recently performed work on the hydraulic system had operationally checked the flaps more than 10 times without noting any discrepancies. Notably, the aircraft was not placed on jacks for an operational test of the landing gear following this maintenance. Post-accident examination of the wreckage revealed that the landing gear was fully extended, the flaps were partially extended, and the left propeller had not been feathered.

Probable cause

The presence of water in the fuel injector nozzles and fuel manifold assembly of the left engine caused engine roughness and subsequent loss of control.

Frequently asked questions

What happened in the 1995-06-01 Piper PA-23-250 accident near Opa-locka, FL?

An aircraft experienced engine roughness and a sudden loss of control during its initial climb, resulting in a ground impact.

What aircraft was involved and where did it happen?

The accident on 1995-06-01 involved a Piper PA-23-250, registration N5832Y, at Opa-locka, FL.

What was the probable cause of the accident?

The presence of water in the fuel injector nozzles and fuel manifold assembly of the left engine caused engine roughness and subsequent loss of control.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03764. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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