Casualties unknown

2018-02-01: Airbus A330-343 (B-HLN) — Airbus A330-343 Commanded Inflight Shutdown during Takeoff from Hong Kong International Airport, HK

Airbus A330-343 Commanded Inflight Shutdown during Takeoff from Hong Kong International Airport, HK

On February 1, 2018, an Airbus A330-343 (registration B-HLN) was involved in an aviation accident near Airbus A330-343 Commanded Inflight Shutdown during Takeoff from Hong Kong International Airport, HK. Investigators recorded the probable cause as: The engine failure was caused by the fracture and subsequent release of a high-pressure turbine blade. This summary draws on records from the Air Accident Investigation Authority of Hong Kong (AAIA); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Air Accident Investigation Authority of Hong Kong (AAIA)Primary reportUpdated 1785027978Data APIEditorial standards
Aircraft registered B-HLN
Aircraft registered B-HLN. Photo: Yamaguchi Yoshiaki from Japan / CC BY-SA 2.0, via Wikimedia Commons

A high-pressure turbine blade failure on a Cathay Pacific Airbus A330 led to an engine shutdown and emergency return to Hong Kong International Airport.

What happened

On 1 February 2018, a Cathay Pacific Airways Limited Airbus A330-343, registration B-HLN, was performing a takeoff from Hong Kong International Airport. During the takeoff roll, the No.1 engine experienced an audible surge and triggered a stall message on the cockpit displays. Simultaneously, the crew observed high vibration levels in the N2 and N3 shafts, along with low oil pressure warnings.

Following standard operating procedures, the crew executed a commanded inflight shutdown of the engine and declared a Mayday. The aircraft successfully returned to the airport and landed without further incident. There were no injuries to the 272 passengers or 13 crew members on board.

The investigation

The AAIA investigation focused on the mechanical failure of the Rolls-Royce Trent 700 engine. Initial ground inspections revealed metallic debris within the engine's jetpipe. Subsequent borescope examinations confirmed that a single high-pressure turbine blade had fractured.

The investigation examined the metallurgical properties of the failure, specifically looking at corrosion fatigue and the effectiveness of existing inspection protocols. The analysis involved coordinating with the engine manufacturer, Rolls-Royce, the European Union Aviation Safety Agency (EASA), and the UK's Air Accidents Investigation Branch.

Probable cause

The engine failure was caused by the fracture and subsequent release of a high-pressure turbine blade.