Casualties unknown

Bell 206B Helicopter Emergency Landing Incident in Venezuela (YV3004)

FECHA: 22/11/2025, VE

On November 22, 2025, a BELL HELICOPTER 206 B (registration YV3004) operated by LUGAR: was involved in an aviation accident near FECHA: 22/11/2025, VE. Investigators recorded the probable cause as: Failure in the power regulation system, specifically an internal failure within the N2 Turbine Governor mechanism, leading to a drop in main rotor RPM during takeoff. This summary draws on records from the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela).

Sourcesthe Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela)Primary reportUpdated 2026-09-08Data APIEditorial standards

A Bell 206B helicopter (YV3004) suffered a main rotor RPM drop during takeoff from Uruyen, Venezuela. The pilot executed an emergency landing, resulting in total airframe destruction but no injuries to the two occupants.

Incident Overview

On November 22, 2025, a Bell Helicopter Textron 206B, registration YV3004, departed from the Uruyen Camp with a destination of Canaima. During the initial climb, the aircraft experienced a significant decrease in main rotor RPM. The pilot initiated an emergency landing procedure. Upon impact with the terrain, the tail boom separated from the fuselage, and the helicopter lost control, resulting in the total destruction of the airframe. Two individuals were on board: the pilot and a mechanic. Both occupants remained uninjured.

Aircraft and Maintenance Status

The aircraft was powered by a Rolls-Royce 250B-C20B engine and held a valid Certificate of Airworthiness issued by INAC, expiring in July 2027. At the time of the incident, the airframe had approximately 7,052.2 total flight hours. The last scheduled maintenance inspections (100-hour, 300-hour, and 24-month) were completed on September 24, 2025, by OMAC N° 568 Coqui Flight Services Center in Maracay. Records indicated the aircraft was airworthy prior to the flight.

Investigation Findings

Investigative analysis revealed that the tail boom fractured due to shear stress at its root during impact, with no evidence of contact from main rotor blades. The landing gear skids failed catastrophically under excessive load, and the cross-tube penetrated the fuselage floor, indicating the structure absorbed the full kinetic energy of the impact. Main rotor blades remained structurally intact with only superficial scarring, consistent with low RPM conditions at ground contact.

Probable Cause Analysis

The investigation identified a failure in the power regulation system, specifically a drop in RPM during takeoff. Physical evidence and operational data point to an internal failure within the N2 Turbine Governor mechanism. The pneumatic lines connecting the Governor to the Fuel Control Unit (FCU) were found to be in good condition, with no leaks or cracks. No fuel contaminants were detected in filters. The investigation is ongoing, with bench tests of the N2 Governor pending to confirm the causal factor.

Investigation report by the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela). Original record: https://www.mppt.gob.ve/download/189139/. This page is a structured re-presentation; facts and quotes are in the Junta de Investigacion de Accidentes de Aviacion Civil (JIAAC), Venezuela - MppT.