Casualties unknown

2021-09-27: EMBRAER 190-100 IWG (YV2964) — CONVIASA. — PISTA 10/28 DEL AEROPUERTO INTL. “SIMÓN BOLÍVAR”,, VE

PISTA 10/28 DEL AEROPUERTO INTL. “SIMÓN BOLÍVAR”,, VE

On September 27, 2021, an EMBRAER 190-100 IWG (registration YV2964) operated by CONVIASA. was involved in an aviation accident near PISTA 10/28 DEL AEROPUERTO INTL. “SIMÓN BOLÍVAR”,, VE. Investigators recorded the probable cause as: The loss of engine power was caused by a mechanical failure in the high-pressure compressor's Variable Stator Vane (VSV) mechanism, specifically involving jammed vanes that led to the bending of the actuator rods and subsequent sensor discrepancies. This summary draws on records from the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela)Primary reportUpdated 1781150548Data APIEditorial standards

A Conviasa Embraer ERJ 190-200 experienced a significant power reduction in its right engine during takeoff from Maiquetia, forcing an aborted departure.

What happened

On September 27, 2021, at 15:24 UTC, a Conviasa Embraer ERJ 190-200 (registration YV2964) was performing a commercial flight from Maiquetia International Airport in Venezuela to Viru Viru International Airport in Bolivia. During the takeoff roll, the right engine failed to reach required performance parameters. The engine's power automatically reduced, limiting the high-temperature turbine RPM to 40%. In response to this loss of thrust, the pilot decided to abort the takeoff and return to the terminal.

The aircraft was carrying 124 passengers and a crew of five. There were no injuries reported, and the aircraft sustained no damage during the incident. Weather conditions at the time were favorable, with unlimited visibility and light winds.

The investigation

Investigators from JIAAC conducted a technical examination of the aircraft and its engines. The inspection included a review of maintenance records, crew interviews, and a physical examination of the engine's internal components.

Technicians analyzed the aircraft's fault recording computer, which revealed error codes indicating a discrepancy of more than 5% in the position sensors of the Variable Stator Vanes (VSV) within the high-pressure compressor. Further disassembly of the assembly revealed that two rods responsible for moving the ring that rotates the vane linkages were bent. The investigation also noted that the flight data recorder (FDR) and cockpit voice recorder (CVR) could not be downloaded at the time because the operator's maintenance organization lacked the necessary recovery capacity.

Findings

  • The right engine experienced an automatic power reduction due to a failure in the high-pressure compressor's Variable Stator Vane (VSV) system.
  • Bent actuator rods were discovered, which had been forced into a deformed state due to the jamming of the vane axes.
  • This mechanical seizure caused the sensors to provide inconsistent position readings, triggering the engine control system to limit RPM to prevent further damage.

Probable cause

The loss of engine power was caused by a mechanical failure in the high-pressure compressor's Variable Stator Vane (VSV) mechanism, specifically involving jammed vanes that led to the bending of the actuator rods and subsequent sensor discrepancies.

Investigation report by the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela). Original record: https://www.mppt.gob.ve/download/153146/. This page is a structured re-presentation; facts and quotes are in the Junta de Investigacion de Accidentes de Aviacion Civil (JIAAC), Venezuela - MppT.