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.
Chandalar Shelf, AK
The pilot reported that during the takeoff roll, as the airplane became airborne, he heard an “audible pop” and immediately felt slack in the left rudder pedal. The airplane banked to the right, unable to recover from the right turn, he decreased power and added right rudder. Subsequently, he continued in the forced bank to the right and maneuvered the airplane for an emergency off-airport landing. During the emergency landing the tail was dragged sideways, the main landing gear collapsed, and the airplane sustained substantial damage to the elevator. A postaccident examination revealed that the forward attachment point of the rudder cable that connects to the rudder pedal came unfastened. The pilot reported that the connecting bolt was recovered but that the nut and cotter pin were not located. Based on the available evidence it was undetermined why the nut disconnected from the bolt.
A separation of the rudder cable from the rudder pedal due to the connecting bolt detaching for undetermined reasons, which resulted in a loss of directional control.
The pilot reported that during the takeoff roll, as the airplane became airborne, he heard an “audible pop” and immediately felt slack in the left rudder pedal. The airplane banked to the right, unable to recover from the right turn, he decreased power and added right rudder. Subsequently, he continued in the forced bank to the right and maneuvered the airplane for an emergency off-airport landing. During the emergency landing the tail was dragged sideways, the main landing gear collapsed, and the airplane sustained substantial damage to the elevator. A postaccident examination revealed that the forward attachment point of the rudder cable that connects to the rudder pedal came unfastened. The pilot reported that the connecting bolt was recovered but that the nut and cotter pin were not located. Based on the available evidence it was undetermined why the nut disconnected from the bolt.