Emergency Landing Following Main Rotor Blade Damage in North Sea

Casualties unknown • Southwest of Stavanger Airport Sola (ENZV), NO

A Eurocopter AS 332L2 helicopter was forced to make an emergency landing on a vessel after a vibration absorber component failure caused severe rotor vibrations.

What happened

On November 5, 2002, a Eurocopter AS 332L2 helicopter, registration LN-ONI, was performing a routine offshore passenger flight from the Sleipner oil field toward Stavanger Airport Sola. The aircraft was carrying 14 passengers and 2 crew members. During the descent through 1,200 feet, the helicopter experienced intense vibrations that made it difficult for the crew to read flight instruments.

The crew issued a MAYDAY call and identified a nearby vessel to facilitate an emergency landing. To mitigate the vibrations, the pilot reduced the airspeed from 158 knots to 100 knots. The helicopter successfully performed a controlled landing on the helideck of the M/T Navion Anglia, approximately 17 nautical miles southwest of Sola. There were no injuries to the passengers or crew.

The investigation

The Norwegian Safety Investigation Authority (NSIA) examined the aircraft and found that a pendulum weight from the vibration absorber on one of the main rotor blades had detached. This lost weight had struck another rotor blade, penetrating the blade behind the main spar and causing significant structural damage. This impact destroyed the blade's rigidity and created a massive mass imbalance of 5,500 N.

Investigators analyzed the mechanical failure of the vibration absorber assembly and the fatigue characteristics of the component shaft. The investigation also reviewed maintenance records, manufacturer certification data, and the manufacturer's emergency procedures regarding severe rotor vibrations.

Probable cause

The direct cause of the accident was the failure of the vibration absorber shaft due to fatigue, which led to the loss of a pendulum weight that subsequently damaged a main rotor blade. This fatigue was initiated by fretting on the shaft surface, driven by pivoting and bending of the spacer and potential loss of installation torque.

Frequently asked questions

What happened in the 2002-11-05 Eurocopter AS 332L2 accident near Southwest of Stavanger Airport Sola (ENZV), NO?

A Eurocopter AS 332L2 helicopter was forced to make an emergency landing on a vessel after a vibration absorber component failure caused severe rotor vibrations.

What aircraft was involved and where did it happen?

The accident on 2002-11-05 involved a Eurocopter AS 332L2, registration LN-ONI, at Southwest of Stavanger Airport Sola (ENZV), NO.

What was the probable cause of the accident?

The direct cause of the accident was the failure of the vibration absorber shaft due to fatigue, which led to the loss of a pendulum weight that subsequently damaged a main rotor blade. This fatigue was initiated by fretting on the shaft surface, driven by pivoting and bending of the spacer and potential loss of…

Investigation report by the Norwegian Safety Investigation Authority (NSIA). Original record: https://nsia.no/Aviation/Aviation/Published-reports/2005-27. This page is a structured re-presentation; facts and quotes are in the Norwegian Safety Investigation Authority (NSIA) / Statens havarikommisjon, Norway.

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