Overall Trends
Total, fatal, and serious accidents in the selected range.
Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.
Fast key and full-text search with live filters, watches, and precise metadata.
Use quotes for exact phrase matches (for example "fuel selector valve").
Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.
Major cases, deep-report coverage, and investigation media across decades of NTSB history.
Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.
NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.
The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.
The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.
Las Cruces, NM
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.
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.