Casualties unknown

1998-07-15: COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. A109K2 (HB-XWF) — Lodrino, TI, CH

Lodrino, TI, CH

On July 15, 1998, a COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. A109K2 (registration HB-XWF) was involved in an aviation accident near Lodrino, TI, CH. Investigators recorded the probable cause as: The accident was caused by the helicopter striking an unmapped transport cable, which led to the destruction of the nose gear and tail rotor drive shaft, necessitating a forced autorotation and resulting in a high-impact landing. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards
Aircraft registered HB-XWF
Aircraft registered HB-XWF. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A medical rescue mission ended in tragedy when an Agusta A-109K2 struck a transport cable, leading to a violent forced landing and the death of the pilot.

What happened

On July 15, 1998, an Agusta A-109K2 helicopter, registration HB-XWF, was conducting a medical evacuation near a quarry in Lodrino, Switzerland. The mission began after a worker sustained a leg injury at the Sangiorgio quarry. After several successful rotations to deliver medical personnel and equipment, the crew attempted a final approach to pick up the patient.

During this final approach, the pilot attempted to stabilize the aircraft against the wind by maneuvering from the north. During this maneuver, the helicopter struck a 200-meter-long transport cable. The impact caused the cable to snag the nose wheel, which was subsequently sheared off. The sudden loss of stability caused the main rotor blades to strike the tail boom, breaking the tail rotor drive shaft. Left without anti-torque control, the aircraft entered a spin and the pilot was forced to execute an autorotation. Due to nearby power lines and a crane, the pilot landed in a dry torrent bed. The impact was extremely violent, resulting in one fatality and one serious injury.

The investigation

The investigation focused on the sequence of events leading to the collision and the subsequent impact. Investigators examined the wreckage and found that the helicopter's nose wheel fork had been severed by the cable. The investigation also reviewed the status of the transport cable, which had been in place since 1981 but was notably absent from official aeronautical obstacle charts.

Medical examinations revealed that the pilot died from internal injuries and brain swelling caused by the vertical force of the crash. The survivor, a rescuer, sustained severe spinal and leg injuries but survived, likely because their metal seat deformed and absorbed some of the impact energy, unlike the more rigid pilot seat.

Findings

  • The primary cause of the accident was a collision with a transport cable which triggered an autorotation and a subsequent hard landing.
  • The aircraft was not equipped with cable-cutting devices, which could have prevented the snagging of the nose wheel.
  • The transport cable was not recorded on official navigation obstacle maps.
  • The pilot's seat lacked an energy-absorbing system, contributing to the fatal nature of the vertical impact forces.

Probable cause

The accident was caused by the helicopter striking an unmapped transport cable, which led to the destruction of the nose gear and tail rotor drive shaft, necessitating a forced autorotation and resulting in a high-impact landing.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1699f.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.