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.
Waco, TX
The pilot stated that while returning to the airport, the helicopter’s engine rpm dropped to zero with no warning. He initiated an autorotation and aligned the helicopter to touch down in an open field but noticed powerlines as he got closer. The pilot maneuvered away from the field and aimed for a clearing in a residential backyard. The main rotor blades impacted a tree, and the helicopter fell about 15 ft to the ground before it came to rest on its right side. The helicopter sustained substantial damage to the fuselage and main rotor blades. According to maintenance records, the engine was removed and replaced about a month before the accident. Additionally, a condition inspection was completed by the owner four days before the accident during which he changed the spark plugs and adjusted the fuel mixture. A post-accident examination revealed corrosion at the radiator fill tube connection and a loose band clamp. Additionally, the engine exhibited signatures consistent with being operated at a temperature above the normal operating temperatures and evidence of piston seizure due to thermal expansion.
The total loss of engine power and subsequent impact with terrain during an autorotation. Contributing to the accident was the improper sealing of the liquid cooling system.
The pilot stated that while returning to the airport, the helicopter’s engine rpm dropped to zero with no warning. He initiated an autorotation and aligned the helicopter to touch down in an open field but noticed powerlines as he got closer. The pilot maneuvered away from the field and aimed for a clearing in a residential backyard. The main rotor blades impacted a tree, and the helicopter fell about 15 ft to the ground before it came to rest on its right side. The helicopter sustained substantial damage to the fuselage and main rotor blades. According to maintenance records, the engine was removed and replaced about a month before the accident. Additionally, a condition inspection was completed by the owner four days before the accident during which he changed the spark plugs and adjusted the fuel mixture. A post-accident examination revealed corrosion at the radiator fill tube connection and a loose band clamp. Additionally, the engine exhibited signatures consistent with being operated at a temperature above the normal operating temperatures and evidence of piston seizure due to thermal expansion.