No fatalities

Boeing 737-800 Rapid Depressurization Incident Near Lugano

nahe Lugano (Schweiz), DE

On April 4, 2012, a Boeing 737-800 was involved in an aviation accident near nahe Lugano (Schweiz), DE. No fatalities were reported. Investigators recorded the probable cause as: The static pressure sensor port on Cabin Pressure Controller #1 was obstructed by a shipping plug, causing erroneous pressure readings and loss of cabin pressure control during the climb phase. This summary draws on records from the German Federal Bureau of Aircraft Accident Investigation (BFU); 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe German Federal Bureau of Aircraft Accident Investigation (BFU)Primary reportUpdated 2026-10-11Data APIEditorial standards
Boeing 737-800
Photo: San Diego Air & Space Museum Archives / Public domain, via Wikimedia Commons

In April 2012, a Boeing 737-800 experienced rapid depressurization over Swiss airspace during a flight from Bergamo to East Midlands. The crew executed an emergency descent to Frankfurt-Hahn, resulting in minor injuries to 13 passengers.

Incident Overview

On April 4, 2012, a Boeing 737-8AS (manufactured in 2003) operated by an Irish airline encountered a severe pressurization anomaly while climbing over the Alps. The aircraft was on a scheduled passenger flight from Bergamo, Italy, to East Midlands, United Kingdom. Approximately 13 minutes after takeoff, while flying at Flight Level 308 in Swiss airspace near Lugano, the crew detected a sudden change in cabin pressure.

Crew Actions and Emergency Descent

The flight deck instruments indicated a rapid rate of climb for the cabin altitude, exceeding 4,000 feet per minute, with the cabin altitude surpassing 10,000 feet. The pilots donned oxygen masks and initiated the Cabin Altitude Warning/Rapid Depressurization checklist. After determining that the cabin altitude was uncontrollable, they declared a Mayday and commenced an emergency descent.

The aircraft descended at rates exceeding 6,000 feet per minute initially, leveling off at Flight Level 100. During this maneuver, the Boeing 737-800 briefly approached an Airbus A319 flying below it, with a horizontal separation of 4.5 nautical miles and vertical separation of 325 feet. The aircraft subsequently diverted to Frankfurt-Hahn Airport, where it landed safely.

Investigation Findings

The investigation, delegated by the Swiss accident investigation authority (SUST) to the German Federal Aviation Office (BFU), revealed a critical mechanical failure. Data from the Cabin Pressure Controllers (CPC) showed that communication faults caused the active CPC #2 to switch to standby mode, transferring control to CPC #1.

Physical inspection of the aircraft identified the root cause: the static pressure sensor port on CPC #1 was blocked by a black plastic shipping plug. This obstruction prevented CPC #1 from accurately measuring ambient pressure, leading to erroneous control signals and the rapid loss of cabin pressure. The incident resulted in minor injuries to 13 passengers, including one ruptured eardrum, while no structural damage was reported.

Probable cause

The static pressure sensor port on Cabin Pressure Controller #1 was obstructed by a shipping plug, causing erroneous pressure readings and loss of cabin pressure control during the climb phase.

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Frequently asked questions

What happened in the 4 Apr 2012 Boeing 737-800 accident near nahe Lugano (Schweiz), DE?

In April 2012, a Boeing 737-800 experienced rapid depressurization over Swiss airspace during a flight from Bergamo to East Midlands. The crew executed an emergency descent to Frankfurt-Hahn, resulting in minor injuries to 13 passengers.

Were there any fatalities in the 4 Apr 2012 Boeing 737-800 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 4 Apr 2012 involved a Boeing 737-800, at nahe Lugano (Schweiz), DE.

What was the probable cause of the accident?

The static pressure sensor port on Cabin Pressure Controller #1 was obstructed by a shipping plug, causing erroneous pressure readings and loss of cabin pressure control during the climb phase.