Casualties unknown

2017 Boeing 737-600 cabin depressurization near Munich

nahe München, DE

On May 14, 2017, a Boeing B737-600 was involved in an aviation accident near nahe München, DE. Investigators recorded the probable cause as: A leaking valve in the transition area from the APU to the cabin (bulk seal on the keel beam of the APU bleed duct) caused the cabin pressure loss. This summary draws on records from the German Federal Bureau of Aircraft Accident Investigation (BFU).

Sourcesthe German Federal Bureau of Aircraft Accident Investigation (BFU)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Boeing 737-600 suffered a cabin pressure loss near Munich on 14 May 2017. The crew made an emergency descent and landed safely at Munich Airport with no injuries or damage.

Incident Overview and Flight Details On 14 May 2017, a Boeing 737-600 departed Prague Airport at 09:25 UTC on runway 24, bound for Djerba-Zarzis Airport in Tunisia. During climb in German airspace, the aircraft experienced a cabin pressure loss around 09:39 UTC while passing flight level 320. The passenger oxygen masks deployed automatically. ## Crew Actions and Emergency Descent Both pilots donned their oxygen masks and initiated an emergency descent to flight level 100. At 09:40:14 UTC, the crew informed Munich Radar of the emergency descent and received clearance at 09:40:17 UTC. The crew decided to divert to Munich Airport and prepared for an approach to runway 26L. After declaring ready at 09:55:37 UTC, the aircraft was cleared for the ILS approach to runway 26L at 09:55:41 UTC. ## Landing and Post-Incident Findings The aircraft landed safely on runway 26L at approximately 10:05 UTC and taxied to parking stand 196 under its own power. Medical services at Munich Airport reported no health complaints from passengers or crew. ## Technical Investigation The German Federal Bureau of Aircraft Accident Investigation (BFU) determined that the pressure loss was caused by a leaking valve in the transition area from the APU to the cabin, specifically a bulk seal on the keel beam of the APU bleed duct. A loose clamp was found in position 2, where it should have been over the bulk seal in position 1. An additional leak was identified in the L/H-Pack area. Both cabin pressure controllers stored the error 'High Cabin Air Leak Rate,' which requires a cabin pressure rate exceeding 2,000 SLFPM. After repairs, a final pressure test revealed another leak at the L/H-Pack. After shutting down the L/H-Pack, the cabin was found to be airtight, and the aircraft was released for a no-passenger flight to flight level 250 under the Minimum Equipment List (MEL).

Probable cause

A leaking valve in the transition area from the APU to the cabin (bulk seal on the keel beam of the APU bleed duct) caused the cabin pressure loss.