Casualties unknown

2019-09-29: EMBRAER E-190 (LV-CIG) — Aviación Comercial — Aeropuerto Aeroparque Jorge Newbery (Sabe) (Buenos Aires), AR

Aeropuerto Aeroparque Jorge Newbery (Sabe) (Buenos Aires), AR

On September 29, 2019, an EMBRAER E-190 (registration LV-CIG) operated by Aviación Comercial was involved in an aviation accident near Aeropuerto Aeroparque Jorge Newbery (Sabe) (Buenos Aires), AR. Investigators recorded the probable cause as: A manufacturing deficiency in the high-pressure turbine disk's geometric profile created uneven load distribution and stress concentration, resulting in the separation of turbine blades during normal engine operation. This summary draws on records from the Argentine Transportation Safety Board (JST); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Argentine Transportation Safety Board (JST)Primary reportUpdated 1785037245Data APIEditorial standards
Aircraft registered LV-CIG
Aircraft registered LV-CIG. Photo: User:Leonardob0880 / CC BY-SA 3.0, via Wikimedia Commons

A manufacturing defect in a high-pressure turbine disk led to the failure of the left engine during a commercial flight departing from Buenos Aires.

What happened

On September 29, 2019, an Embraer ERJ190-100IGW, registration LV-CIG, operated by Austral Líneas Aéreas, departed Aeroparque Jorge Newbery in Buenos Aires for Salta. During the initial climb phase of the flight, while passing through 3,800 feet, the aircraft experienced a failure of the left engine.

Upon detecting abnormal engine parameters, the crew declared a MAYDAY emergency and initiated a return to the departure airport. The aircraft completed the approach and landing using only one operational engine. There were no injuries among the 60 passengers and 5 crew members on board, though the left engine sustained significant damage due to the separation of turbine blades.

The investigation

The investigation focused on the mechanical failure of the General Electric CF34-10E5A1G08 engine. Technical analysis of the components revealed that the high-pressure turbine disk possessed a geometric profile that deviated from the intended design. This manufacturing irregularity reduced the clearance between the contact surfaces of the turbine blades and the disk, leading to an uneven distribution of mechanical loads.

Investigators examined the maintenance history and operational parameters of the aircraft. While the operator's engine performance parameters were noted to be higher than some other operators, the investigation confirmed that all values remained within approved operational limits and that the airline adhered to all airworthiness requirements. The engine components, including the blades and disk, had been installed in the engine since new.

Findings

  • The primary cause of the engine failure was a manufacturing defect in the high-pressure turbine disk and blades produced by XAE.
  • A geometric discrepancy in the disk profile caused a concentration of stress due to inadequate clearance between the blade and disk surfaces.
  • This stress concentration led to the failure of the turbine blades under normal operating temperatures and pressures.
  • The defect was a latent condition that could not be detected through standard maintenance or inspection protocols available at the time of the event.

Probable cause

A manufacturing deficiency in the high-pressure turbine disk's geometric profile created uneven load distribution and stress concentration, resulting in the separation of turbine blades during normal engine operation.