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.
Greeley, CO
N3554P WAS ON A MAINTENANCE TEST FLIGHT AFTER THE RIGHT WING WAS REPAIRED. THE PILOT LOST CONTROL OF THE AIRPLANE SHORTLY AFTER LIFTOFF AND WAS UNABLE TO REGAIN CONTROL PRIOR TO THE GROUND IMPACT. THE A&P MECHANIC WHO PERFORMED THE REPAIRS, RE ASSEMBLED THE RIGHT WING AILERON CONTROL CABLES PER THE PIPER SERVICE MANUAL. POST ACCIDENT EXAMINATION OF THE AILERON CONTROL SYSTEM REVEALED THE RIGHT WING CONTROL CABLES WERE REVERSED ON THE AILERON BELLCRANK, RESULTING IN BOTH AILERONS MOVING THE SAME DIRECTION (EITHER UP OR DOWN) WHEN THE CONTROL WHEEL WAS TURNED LEFT OR RIGHT.
THE IMPROPER IDENTIFICATION OF PARTS IN THE PIPER PA-31-350 SERVICE MANUAL PERTAINING TO THE AILERON CABLES. THIS DISCREPANCY RESULTED IN THE IMPROPER INSTALLATION OF THE AILERON CABLES ON THE RIGHT AILERON BELLCRANK BY A MECHANIC DURING THE RECONSTRUCTION OF THE RIGHT WING. THE IMPROPER CONNECTION RESULTED IN A LOSS OF AIRCRAFT CONTROL BY THE PILOT IMMEDIATELY AFTER TAKEOFF. ALSO CAUSAL TO THE ACCIDENT WERE THE INADEQUATE INSPECTION OF THE FLIGHT CONTROL SYSTEM BY A SECOND MECHANIC WITH INSPECTION AUTHORIZATION, AND THE INADEQUATE PREFLIGHT INSPECTION OF THE FLIGHT CONTROL SYSTEM BY THE PILOT PRIOR TO TAKEOFF.
N3554P WAS ON A MAINTENANCE TEST FLIGHT AFTER THE RIGHT WING WAS REPAIRED. THE PILOT LOST CONTROL OF THE AIRPLANE SHORTLY AFTER LIFTOFF AND WAS UNABLE TO REGAIN CONTROL PRIOR TO THE GROUND IMPACT. THE A&P MECHANIC WHO PERFORMED THE REPAIRS, RE ASSEMBLED THE RIGHT WING AILERON CONTROL CABLES PER THE PIPER SERVICE MANUAL. POST ACCIDENT EXAMINATION OF THE AILERON CONTROL SYSTEM REVEALED THE RIGHT WING CONTROL CABLES WERE REVERSED ON THE AILERON BELLCRANK, RESULTING IN BOTH AILERONS MOVING THE SAME DIRECTION (EITHER UP OR DOWN) WHEN THE CONTROL WHEEL WAS TURNED LEFT OR RIGHT.