No fatalities

2017-05-20: Airbus A380-842 (VH-OQG) — Qantas Airways — near Los Angeles International Airport, International

near Los Angeles International Airport, International

On May 20, 2017, an Airbus A380-842 (registration VH-OQG) operated by Qantas Airways was involved in an aviation accident near near Los Angeles International Airport, International. No fatalities were reported. Investigators recorded the probable cause as: Corrosion of low-pressure turbine stage 2 blades due to chemical residue from cleaning operations, leading to fatigue cracking and subsequent release of blade shroud debris, which caused significant downstream engine damage. This summary draws on records from the Australian Transport Safety Bureau (ATSB); 16 related events involving the same aircraft type or operator are linked below.

Sourcesthe Australian Transport Safety Bureau (ATSB)Primary reportUpdated 1779789371Data APIEditorial standards
Aircraft registered VH-OQG
Aircraft registered VH-OQG. Photo: Eluveitie / CC BY-SA 3.0, via Wikimedia Commons

An investigation by Rolls-Royce into a Trent 900 engine failure found internally-corroded low-pressure turbine stage 2 blades. The corrosion, from cleaning residue, led to fatigue cracking and debris release, causing downstream damage. A spurious fire warning was linked to detector wear and vibration.

Engine Failure Investigation

Rolls-Royce, the manufacturer of the Trent 900 engine, conducted an investigation into an engine failure that resulted in a shutdown. The teardown examination revealed internally-corroded low-pressure turbine stage 2 (LPT2) blades. The corrosion was caused by chemical residue left in the hollow blades from cleaning operations during the last service in July 2015. This corrosion led to fatigue cracking, which subsequently caused the release of blade shroud debris. The debris resulted in significant downstream engine damage.

Following the findings, Rolls-Royce performed a thorough audit of its cleaning operations and implemented additional safety actions, as detailed in the safety action section of the report.

Fire Warning Analysis

The fire and overheat detection system was assessed to determine the cause of a fire warning that occurred during the event. No issues were identified in the system itself, and the fire/overheat detector assemblies were removed and returned to the vendor for further evaluation. The detector manufacturer identified wear in the unit that would have increased its sensitivity to vibration, raising the likelihood of spurious warnings. Rolls-Royce assessed that it was very likely that the wear, combined with the vibrations associated with this event, contributed to the spurious fire warning.

Probable cause

Corrosion of low-pressure turbine stage 2 blades due to chemical residue from cleaning operations, leading to fatigue cracking and subsequent release of blade shroud debris, which caused significant downstream engine damage.