Casualties unknown

2019-09-29: Airbus A330-243 (B-LHA) — Dual Hydraulic Failure of Airbus A330-243 on Departure from Hong Kong International Airport, HK

Dual Hydraulic Failure of Airbus A330-243 on Departure from Hong Kong International Airport, HK

On September 29, 2019, an Airbus A330-243 (registration B-LHA) was involved in an aviation accident near Dual Hydraulic Failure of Airbus A330-243 on Departure from Hong Kong International Airport, HK. 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-LHA
Aircraft registered B-LHA. Photo: Dltl2010 / CC BY-SA 4.0, via Wikimedia Commons

On 29 September 2019, Hong Kong Airlines flight HX707 (Airbus A330-243, B-LHA) suffered low pressure in Green and Blue hydraulic systems shortly after takeoff from Hong Kong. The crew returned for an emergency landing; the aircraft landed safely with a burst No. 5 tyre. No injuries were reported.

History of the Flight

On 29 September 2019 at 1223 hrs, Hong Kong Airlines Limited flight HX707, an Airbus A330-243 aircraft registered B-LHA, departed from Runway 25L at Hong Kong International Airport (HKIA) en route to Denpasar, Indonesia. At 1226 hrs, while climbing through 3,460 ft, the Electronic Centralized Aircraft Monitoring (ECAM) system generated warnings indicating low pressure in the Green and Blue hydraulic systems.

Emergency Response

The flight crew executed the applicable emergency procedures, declared an emergency, and decided to return to HKIA for a full emergency landing. The aircraft landed safely on Runway 25L at 1257 hrs and came to a stop abeam taxiway J3. During the landing, the No. 5 tyre burst. The runway was subsequently closed.

Post-Landing Actions

All passengers were disembarked at the scene. There were no injuries. After the No. 5 tyre was replaced, the aircraft was towed to parking bay D313. The runway was reopened at 1440 hrs.

Inspection Findings

Inspection of the left landing gear wheel well revealed that a manual valve had detached from the Green hydraulic system Ground Service Manifold and a Blue hydraulic system return pipe had been punctured.

Causes and Contributing Factors

The investigation identified causes and a contributing factor for the serious incident, as detailed in the official report. No further details on the stated causes are provided in this summary.