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.
Temecula, CA
The instructor pilot said that during climb to cruise the engine suddenly quit completely with a loud noise. The instructor landed the aircraft in a field and the aircraft nosed over after colliding with a berm. Examination of the aircraft revealed that the rear dome of the left muffler had blown out. Scorching and exhaust stains were evident on the firewall to the rear of the muffler and wire bundles routed in this area were found burned with melted insulation noted. The 'P' leads for the magnetos were found routed in this wire bundle. Visual examination and electrical continuity checks of the 'P' leads revealed that the internal insulation had melted allowing the conductors to short within the wires. Examination of the muffler revealed severe internal erosion, with holes through the cabin heat shroud. The failed end of the muffler was found to be severely eroded around the failure point on the end piece, with small holes and external discoloration noted.
THE SHUTDOWN OF THE ENGINE DUE TO THE FAILURE OF THE MUFFLER AND THE RESULTING HEAT INDUCED SHORTING OF THE MAGNETO GROUND WIRES, AND THE INADEQUATE MAINTENANCE INSPECTION OF THE MUFFLER AND THE ENGINE EXHAUST SYSTEM.
THE INSTRUCTOR PILOT SAID THAT DURING CLIMB TO CRUISE THE ENGINE SUDDENLY QUIT COMPLETELY WITH A LOUD NOISE. THE INSTRUCTOR LANDED THE AIRCRAFT IN A FIELD AND THE AIRCRAFT NOSED OVER AFTER COLLIDING WITH A BERM. EXAMINATION OF THE AIRCRAFT REVEALED THAT THE REAR DOME OF THE LEFT MUFFLER HAD BLOWN OUT. SCORCHING AND EXHAUST STAINS WERE EVIDENT ON THE FIREWALL TO THE REAR OF THE MUFFLER AND WIRE BUNDLES ROUTED IN THIS AREA WERE FOUND BURNED WITH MELTED INSULATION NOTED. THE 'P' LEADS FOR THE MAGNETOS WERE FOUND ROUTED IN THIS WIRE BUNDLE. VISUAL EXAMINATION AND ELECTRICAL CONTINUITY CHECKS OF THE 'P' LEADS REVEALED THAT THE INTERNAL INSULATION HAD MELTED ALLOWING THE CONDUCTORS TO SHORT WITHIN THE WIRES. EXAMINATION OF THE MUFFLER REVEALED SEVERE INTERNAL EROSION, WITH HOLES THROUGH THE CABIN HEAT SHROUD. THE FAILED END OF THE MUFFLER WAS FOUND TO BE SEVERELY ERODED AROUND THE FAILURE POINT ON THE END PIECE, WITH SMALL HOLES AND EXTERNAL DISCOLORATION NOTED.