Dual System Failures Lead to Two Cabin Depressurisation Events in Boeing 737

Casualties unknown • Overhead Brussels, GB

A Boeing 737-3Y0 experienced two separate cabin altitude climbs over Europe due to a combination of electrical and pneumatic malfunctions.

What happened

On 25 May 2000, a Boeing 737-3Y0, registration G-IGOG, was performing a scheduled passenger flight from Venice to London Stansted. While cruising at FL 350 near Brussels, the crew noticed a rapid increase in cabin altitude, which was climbing at approximately 2,000 feet per minute. Although the crew attempted to use the standby pressurisation system and manually close the outflow valve, the cabin altitude continued to rise.

In response, the flight crew donned oxygen masks and initiated an emergency descent to FL 100. During the descent, the passenger oxygen masks deployed automatically. The cabin crew promptly secured the cabin and passengers, managing the situation through regular announcements despite some passenger confusion regarding the oxygen flow. The aircraft continued to its destination, Stansted, without further incident.

Two days later, during a return flight from Alicante to Stansted, a second event occurred. As the aircraft began its descent, engine power was reduced, causing the cabin altitude to climb at 4,000 feet per minute. The crew declared a PAN-PAN call and descended to FL 100. In this instance, the pressurisation system reverted to standby mode effectively, preventing the deployment of passenger oxygen masks.

The investigation

The investigation focused on identifying why the pressurisation system failed to maintain altitude during both incidents. Following the first event, the operator and manufacturer identified a fault in the feedback loop between the pressure controller and the outflow valve, leading to the replacement of the valve.

However, the second event prompted a deeper technical analysis. Investigators examined the electrical and pneumatic systems to determine why the cabin altitude climbed specifically when engine thrust was reduced. The investigation scrutinized the electrical relay components and the pneumatic air supply from the engines.

Probable cause

The depressurisation was caused by the simultaneous occurrence of two independent failures: an intermittent fault in the Number One Transfer Relay, which caused the outflow valve to freeze in the cruise position, and a sluggish High Pressure Shut-off Valve on the Number 1 engine, which reduced the air supply to the cabin during thrust reduction.

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Frequently asked questions

What happened in the 2000-05-25 BOEING 737-3Y0 accident near Overhead Brussels, GB?

A Boeing 737-3Y0 experienced two separate cabin altitude climbs over Europe due to a combination of electrical and pneumatic malfunctions.

What aircraft was involved and where did it happen?

The accident on 2000-05-25 involved a BOEING 737-3Y0, registration G-IGOG, at Overhead Brussels, GB.

What was the probable cause of the accident?

The depressurisation was caused by the simultaneous occurrence of two independent failures: an intermittent fault in the Number One Transfer Relay, which caused the outflow valve to freeze in the cruise position, and a sluggish High Pressure Shut-off Valve on the Number 1 engine, which reduced the air supply to the…

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