2 Jan 2013: EUROCOPTER EC130 B4 (N334AM) — AIR METHODS CORP — Seminole, OK

No fatalitiesSeminole, OK, United States

A Eurocopter EC130 B4 experienced a loss of engine power during climb, resulting in a hard landing and four serious injuries.

What happened

On January 2, 2013, a Eurocopter EC1ly30 B4 helicopter, registration N334AM, departed from Seminole Regional Airport (KSRE) in Oklahoma, en route to Okemah. Shortly after takeoff, while climbing through approximately 1,600 to 1,700 feet mean sea level, the pilot heard an impact sound and the engine stopped producing power.

The pilot initiated an autorotation toward an open field. During the descent, the crew identified power lines and a previously undetected barbed-wire fence obstructing the landing area. The pilot maneuvered the aircraft to clear the fence, which resulted in a hard landing. The accident resulted in 4 serious injuries and no fatalities. The helicopter sustained substantial damage.

The investigation

Investigators examined the engine and found that four axial compressor blades exhibited significant deformation on the outboard tips of their leading edges. The direction of the deformation was opposite to normal rotation, which was consistent with the ingestion of soft body debris, such as ice.

Weather records indicated that for the three days preceding the accident, the aircraft was exposed to drizzle, rain, mist, and fog. While the engine inlet cover had been installed the day before the flight, the aircraft had been parked outside in freezing temperatures. Examination of the engine air intake duct showed no blockages or large debris, and the air filter was undamaged. An engine run conducted on a test stand later produced a distinct whining noise at idle, consistent with the damage found on the compressor blades.

Probable cause

The loss of engine power was caused by the ingestion of ice. Contributing factors included the delayed installation of the engine inlet cover after the aircraft had been exposed to moisture and freezing temperatures, as well as inadequate preflight inspections that failed to detect ice formation in the engine air intake.

Contributing factors

Causes

Nacelles/pylons structure

Other contributing factors

Effect on equipmentInadequate inspectionEffect on operationMaintenance personnel