Dual Engine Bleed Air Fault Triggers Emergency Descent of China Airlines Airbus A330

Casualties unknown • 150NM NE from VVTS/in the air, TW

An Airbus A330-300 operating from Taoyuan to Ho Chi Minh City performed an emergency descent after a dual engine bleed air failure caused cabin altitude warnings.

What happened

On June 3, 2013, China Airlines flight CI781, an Airbus A330-300 with registration B-18317, was operating a scheduled passenger service from Taiwan Taoyuan International Airport to Ho Chi Minh City’s Tan Son Nhat International Airport. The aircraft was carrying 185 passengers and 15 crew members.

Shortly after takeoff, the Electronic Centralized Aircraft Monitoring (ECAM) indicated a bleed air fault in the number 2 engine. The crew followed established procedures and continued the climb to a cruise altitude of 40,000 feet. During cruise, the crew attempted to reset the number 2 engine bleed system, but the fault recurred.

As the aircraft was approximately 110 nautical miles northeast of Ho Chi Minh City, a second fault occurred in the number 1 engine bleed system. This triggered a cabin altitude warning as the cabin altitude rose to 9,536 feet. The crew initiated an emergency descent, utilizing speed brakes to increase the descent rate to approximately 7,696 feet per minute. The crew declared a "MAYDAY" to air traffic control and continued descending until the aircraft reached 10,000 feet, eventually leveling off at 8,000 feet to ensure passenger comfort. The flight landed safely at Tan Son Nhat International Airport without injuries or damage to the aircraft.

The investigation

The Taiwan Transportation Safety Board (TTSB) examined the aircraft's flight data from the Digital Flight Data Recorder (DFDR) and cockpit voice recordings. The investigation focused on the mechanical failure of the engine bleed air systems and the subsequent loss of cockpit voice recorder (CVR) data.

Investigators found that during the post-flight maintenance, technicians failed to pull the correct circuit breaker to stop the CVR from recording, which caused the continuous power supply to overwrite the two hours of critical audio from the incident. The investigation also involved collaboration with the French BEA, Airbus, and the Singaporean AAIB to test faulty components at a facility in Singapore.

Probable cause

The dual engine bleed air failure was caused by **degraded O-rings and contamination within the fan air valve thermostats**, which led to insufficient cooling and subsequent overheating, forcing the pressure regulating valves to close.

Frequently asked questions

What happened in the 2013-06-03 Airbus Industrie/A330-300 accident near 150NM NE from VVTS/in the air, TW?

An Airbus A330-300 operating from Taoyuan to Ho Chi Minh City performed an emergency descent after a dual engine bleed air failure caused cabin altitude warnings.

What aircraft was involved and where did it happen?

The accident on 2013-06-03 involved a Airbus Industrie/A330-300, registration B-18317, at 150NM NE from VVTS/in the air, TW.

What was the probable cause of the accident?

The dual engine bleed air failure was caused by **degraded O-rings and contamination within the fan air valve thermostats**, which led to insufficient cooling and subsequent overheating, forcing the pressure regulating valves to close.

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