Casualties unknown

Helicopter Strikes Tree During External Load Operation, Causing Engine Overspeed (N814CE)

Running Springs, CA, US

On September 21, 2005, an Eurocopter AS350B3 (registration N814CE) operated by Southern California Edison was involved in an aviation accident near Running Springs, CA. Investigators recorded the probable cause as: Main rotor impact with trees, which caused the engine-to-transmission drive shaft to twist apart, resulting in an engine overspeed and over temperature condition. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

A helicopter performing external load operations struck a tree with the main rotor, causing the engine drive shaft to fail and the engine to overspeed and overheat, leading to a nose-first descent into the ground.

Accident Overview

A helicopter engaged in external load operations collided with a tree, resulting in a loss of control and a nose-first descent into the ground. The incident occurred while the helicopter was maneuvering near tall trees with a 78.8-foot-long external load line.

Sequence of Events

The helicopter was conducting external load operations in the vicinity of trees ranging from 80 to 90 feet in height. During the operation, the main rotor impacted a tree. Following the impact, the helicopter descended nose first into the ground.

Engine and Rotor System Data

Data from the Vehicle Engine Monitoring Display (VEMD) recorded a high torque measurement of 146 percent and a low engine drive speed of 184 rpm at the moment of rotor impact. Subsequently, the VEMD recorded a low torque of 5.7 percent, a high engine speed of 511 rpm, and a high temperature of 999°C.

Cause of Engine Overspeed

The main rotor impact with the trees caused the engine's torque to twist apart the engine-to-transmission drive shaft. This failure led to an engine overspeed and over temperature condition.

Operational Context

The operator was using a 78.8-foot-long line for the external load operations. In some cases, this line length placed the main rotor of the helicopter below the treetops of the 80- to 90-foot trees.

Post-Accident Examination

Examination of the helicopter revealed no evidence of a preimpact malfunction or failure of the control system or power plant.

Probable cause

Main rotor impact with trees, which caused the engine-to-transmission drive shaft to twist apart, resulting in an engine overspeed and over temperature condition.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20050927X01537. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.