Casualties unknown

1995-06-24: Piper J3 (N41105) — York, SC

York, SC, US

On June 24, 1995, a Piper J3 (registration N41105) was involved in an aviation accident near York, SC. Investigators recorded the probable cause as: The pilot's inability to maintain control following an in-flight loss of engine power during takeoff, which resulted in a forced landing attempt that failed and led to impact with terrain and water. 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 1781061362Data APIEditorial standards

A pilot experienced sudden engine power loss during takeoff from a sod airfield. Unable to reach a nearby field, the aircraft crashed into a swampy area where the engine became submerged in water.

What happened

The incident occurred during the initial climb phase of flight following takeoff from a sod surface airfield. The pilot reported that the aircraft engine suddenly lost power without prior indication. Attempting to execute a forced landing, the pilot directed the aircraft toward a nearby open field but was unable to reach it due to insufficient altitude or distance.

The aircraft subsequently impacted trees and terrain in a swampy area. Upon impact, the engine compartment became submerged in water. After the accident, maintenance personnel drained the water from the carburetor. Following this procedure, the engine was tested and operated normally at all power settings, indicating that the mechanical failure was likely temporary or related to fluid ingestion rather than internal mechanical damage.

The investigation

Post-acc examination revealed that the engine had been submerged in water following the crash into the swampy terrain. The primary investigative finding focused on the condition of the carburetor after water removal. Testing confirmed that the engine restored full functionality once the ingested water was cleared, suggesting the power loss was not due to a permanent mechanical defect.

Findings

The sequence of events indicates that an in-flight engine power loss occurred during takeoff. The inability to reach a suitable forced landing site resulted in a crash into difficult terrain. The restoration of normal engine operation after draining water from the carburetor points to fuel system interruption or hydrolock as the likely cause of the initial power failure.

Probable cause

The pilot's inability to maintain control following an in-flight loss of engine power during takeoff, which resulted in a forced landing attempt that failed and led to impact with terrain and water. The subsequent normal operation of the engine after draining water from the carburetor suggests the power loss was likely due to fuel system interruption or ingestion.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03618. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.