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.
Osage Beach, MO
The pilot reported that within minutes of departure the engine started to lose power but did not quit completely. He reported that the engine was barely above idle. Passengers flying with the pilot also reported that the engine did not sputter but continued to run smoothly at partial power. The pilot reported that he was unable to restore power to the engine and executed a forced landing at a nearby golf course. Due to golfers on the fairways, the pilot was unable to land on the golf course's fairway. The aircraft landed in rough terrain and went through a ravine which produced substantial damage to the aircraft. The examination of the aircraft revealed that fuel was available in all four fuel tanks prior to impact damage. The fuel lines to the engine driven fuel pump were inspected and were intact with no leakage. The electric boost pump was operated and it indicated normal fuel pressure. The engine driven fuel pump was bench tested and operated normally. The engine was test run and operated within specifications.
a partial loss of power for undetermined reasons.
On May 25, 1996, at 1245 central daylight time, a Piper PA-32, N40933, operated by Sparta Aero Services, sustained substantial damage during a forced landing due to a partial loss of engine power after takeoff near Osage Beach, Missouri. The private pilot and three passengers were not injured. The 14 CFR 91 flight departed Grand Glaize Memorial Airport, Osage Beach, Missouri, on a local flight. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that he had departed Sparta, Illinois, and flew to Osage Beach, Missouri. The distance was about 140 nautical miles and took approximately 1.5 hours. The pilot reported that he departed Osage Beach about 15 minutes later. He reported that within minutes of departure the engine started to lose power but did not quit completely. He reported that the engine was barely above idle. Passengers flying with the pilot also reported that the engine did not sputter but continued to run smoothly at partial power. The pilot reported that he was unable to restore power to the engine, so he did a forced landing at a nearby golf course. Due to golfers on the fairways, the pilot was unable to land on the golf course's fairway. The aircraft landed in rough terrain and went through a ravine which produced substantial damage to the aircraft. The pilot and passengers deplaned without injuries. The examination of the aircraft revealed that fuel was available in all four fuel tanks prior to impact damage. The fuel lines to the engine driven fuel pump were inspected and were intact with no leakage. The electric boost pump was operated and it indicated normal fuel pressure. The engine driven fuel pump was bench tested and it operated normally. The engine was run and it operated within specifications.