Casualties unknown

Engine Power Loss Results in Forced Landing and Wing Damage (N56118)

Flamingo, FL, US

On May 25, 1991, a Piper PA-28-140 (registration N56118) was involved in an aviation accident near Flamingo, FL. Investigators recorded the probable cause as: PARTIAL LOSS OF ENGINE POWER DUE TO FAILURE OF THE NO. 3 CYLINDER EXHAUST VALVE FOR UNDETERMINED REASONS. CONTRIBUTING TO THE ACCIDENT WAS LACK OF SUITABLE TERRAIN DURING THE FORCED LANDING. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

During cruise, engine RPM dropped from 2,400 to 1,900. Unable to maintain altitude, pilot landed in a field; left wing was severed by a tree, aircraft rolled inverted. Examination revealed No. 3 cylinder exhaust valve failure; cause undetermined due to fracture surface damage. Engine had 1,400 hours since October 1979 overhaul.

Incident Overview

During a normal cruise flight, the engine RPM decreased from 2,400 to 1,900. The pilot attempted to correct the power loss but was unsuccessful. Unable to maintain altitude, the pilot executed a forced landing in a field. During the landing roll, the left wing was severed after impacting a tree. The aircraft subsequently rolled inverted and came to rest.

Engine Examination

Post-incident examination of the engine revealed that the No. 3 cylinder exhaust valve had failed. Due to damage to the fracture surface, the cause of the valve failure could not be determined.

Maintenance History

Review of the engine logbooks indicated that in October 1979, the engine had been overhauled, which included replacement of the exhaust valves. Since that overhaul, the engine had accumulated approximately 1,400 hours of operation.

Frequently asked questions

What happened in the 25 May 1991 Piper PA-28-140 accident near Flamingo, FL?

During cruise, engine RPM dropped from 2,400 to 1,900. Unable to maintain altitude, pilot landed in a field; left wing was severed by a tree, aircraft rolled inverted. Examination revealed No. 3 cylinder exhaust valve failure; cause undetermined due to fracture surface damage. Engine had 1,400 hours since October…

What aircraft was involved and where did it happen?

The accident on 25 May 1991 involved a Piper PA-28-140, registration N56118, at Flamingo, FL.

What was the probable cause of the accident?

PARTIAL LOSS OF ENGINE POWER DUE TO FAILURE OF THE NO. 3 CYLINDER EXHAUST VALVE FOR UNDETERMINED REASONS. CONTRIBUTING TO THE ACCIDENT WAS LACK OF SUITABLE TERRAIN DURING THE FORCED LANDING.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X17082. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.