Casualties unknown

2018-06-27: Bell 412 (EC-KVC) — Soto del Real (Madrid), ES

Soto del Real (Madrid), ES

On June 27, 2018, a Bell 412 (registration EC-KVC) was involved in an aviation accident near Soto del Real (Madrid), ES. Investigators recorded the probable cause as: The probable cause of the accident was the decision to land in an area whose dimensions were smaller than those indicated in the Operations Manual. This summary draws on records from the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC).

Sourcesthe Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC)Primary reportUpdated 1785075856Data APIEditorial standards
Aircraft registered EC-KVC
Aircraft registered EC-KVC. Photo: Jose Antonio Moreno Monge from Eivissa, Spain / CC BY-SA 2.0, via Wikimedia Commons

A Bell 412 EP helicopter sustained main rotor blade damage after contacting tree branches during a medical emergency landing. The crew continued the mission but later detected significant damage upon return to base.

Incident Overview

On 27 June 2018, a Bell 412 EP helicopter, registration EC-KVC, operated by Babcock International Group PLC, was dispatched for a medical emergency service to evacuate a person injured in a traffic accident in Soto del Real, Madrid. The aircraft departed at approximately 11:05 UTC for the HEMS mission.

Sequence of Events

The crew initially landed in a nearby clearing around 11:30 UTC but could not transport the injured person to the helicopter due to terrain conditions. They then decided to land at the traffic accident site on a road. During the landing at 11:50 UTC, the main rotor blades contacted tree branches. A visual inspection revealed only superficial marks, so the operation continued.

During the subsequent flight, vibrations were felt in the rotor system. The crew performed a precautionary landing to transfer the patient to a ground ambulance. After inspecting the blades and finding no significant damage, they decided to return to base. Vibrations persisted during the return flight. After landing at base at 13:38 UTC, substantial damage to the main rotor blades was discovered, and the helicopter was taken out of service.

Damage and Injuries

The main rotor blades sustained detachment of fiberglass, damage to trim tabs, and deformities at the blade tips on both the extrados and intrados of four blades. No damage to the leading edges or other parts of the aircraft was observed. All six crew members and one passenger on board were uninjured. No other damage occurred.

Probable Cause

The investigation determined that the probable cause of the accident was the decision to land in an area whose dimensions were smaller than those indicated in the Operations Manual.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/comodin/recursos/2018_027_a.pdf. This page is a structured re-presentation; facts and quotes are in the Comision de Investigacion de Accidentes e Incidentes de Aviacion Civil (CIAIAC), Spain - Ministerio de Transportes y Movilidad Sostenible.