Engine Fire Warning Leads to Emergency Diversion of Airbus A330

Casualties unknown • IE

An Airbus A330-202 experienced an engine fire warning shortly after takeoff from Dublin, forcing a diversion and an overweight landing at Shannon Airport.

What happened

On December 28, 2017, an Airbus A330-202, registration EI-LAX, departed Dublin Airport for a scheduled passenger service to Los Angeles. Approximately 15 seconds after takeoff, the flight crew received a fire warning for the No. 2 engine, accompanied by a high-temperature advisory for the engine compartment. Following standard emergency procedures, the crew shut down the right-hand engine.

As the aircraft climbed, the crew declared a MAYDAY and decided to divert to Shannon Airport, which offered a longer runway suitable for the situation. During the flight, the crew proactively discharged an engine fire extinguisher into the No. 2 engine compartment as a precaution. To manage the aircraft's weight for landing, the crew entered a holding pattern near Shannon to burn off fuel, eventually performing an overweight landing on Runway 06. Despite the emergency, all 267 passengers and 11 crew members disembarked without injury.

The investigation

The AAIU examined the engine components and the maintenance history of the aircraft. Investigators focused on the bleed air system, specifically a component known as a "spacer" located at the 14th stage bleed air outlet. The investigation also looked into the maintenance performed at an engine overhaul facility earlier that year, noting that the task card used for the installation of the spacer was incorrectly identified by the facility.

Findings

  • The engine fire warning was triggered by the fatigue failure of a bleed air spacer.
  • This failure allowed hot, high-pressure air to escape into the engine compartment.
  • The escaping air caused the 14th stage bleed air manifold to buckle, which subsequently struck and damaged the No. 2 engine's main fuel feed line.
  • Metallurgical analysis determined the fracture was caused by reversed bending fatigue due to abnormal loading conditions.
  • While the fuel line was impacted, it was not punctured, and no fuel leak occurred.
  • The investigation noted that a Fluorescent Penetrant Inspection (FPI) is now a requirement for these spacers during engine shop visits to prevent similar occurrences.

Probable cause

The primary cause of the incident was the fatigue failure of the No. 2 engine's 14th stage bleed air spacer, which released high-pressure, high-temperature air into the engine compartment, triggering the fire warning and subsequent engine shutdown.

Frequently asked questions

What happened in the null aircraft accident near IE?

An Airbus A330-202 experienced an engine fire warning shortly after takeoff from Dublin, forcing a diversion and an overweight landing at Shannon Airport.

What aircraft was involved and where did it happen?

The accident on null involved a aircraft, registration EI-LAX, at IE.

What was the probable cause of the accident?

The primary cause of the incident was the fatigue failure of the No. 2 engine's 14th stage bleed air spacer, which released high-pressure, high-temperature air into the engine compartment, triggering the fire warning and subsequent engine shutdown.

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