LAX85IA206

Factual narrative

WHILE CRUISING AT FLT LEVEL 350 IN CLEAR SMOOTH AIR, A LOUD NOISE WAS HEARD, ACCOMPANIED BY A SEVERE JOLT ON THE RIGHT SIDE OF THE CABIN, AS THE NUMBER 3 END SEPARATED FROM ITS MOUNTS. SUBSEQUENT INVESTIGATION DISCLOSED THAT THE FORWARD LAVATORY WAS LEAKING DEODORANT FLUID AND WATER. DEODORANT STAINS EXISTED ALONG THE RIGHT SIDE OF THE FUSELAGE, & WERE SUBSEQUENTLY IDENTIFIED ON THE NUMBER 3 ENGINE NOSE COWL & INLET NOSE CONE. ALL BUT 6 OF THE FIRST STAGE FAN BLADES WERE RECOVERED AT THE ENG IMPACT SITE, & THESE 6 BLADES WERE LOCATED WITHIN A 180 DEGREE SEGMENT OF THE FAN. LEAKAGE OF THE LAVATORY WASTE DRAIN VALVE WAS THE RESULT OF A DAMAGED 'O' RING SEAL. LEAKAGE OF THE DUMP VALVE WAS THE RESULT OF DISBONDING OF A RUBBER BOOT ON ITS SHAFT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12