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.
Show Low, AZ
The pilot said while in level cruise on an IFR flight the engine began to loose power due to carburetor ice and attempts to remedy the situation were unsuccessful with the engine eventually loosing all power. The pilot declared an emergency with Albuquerque Center and was radar vectored toward the Show Low Airport. The flight was intermittently in clouds during the emergency descent and broke out at a low altitude. The aircraft had insufficient altitude to make the airport and landed in the only available location, a field about 23 miles from the airport. During roll out, the aircraft collided with a ditch and nosed over. Post accident examination of the aircraft by FAA inspectors revealed that the carburetor heat box had separated from the heat muff of the exhaust system and was hanging loose in the cowling attached only by the fabric hose. A metal band which attaches the carb heat box to the muff had separated. Chaffing on the cowling in the area of where the heat box was hanging indicated it had been separated for some time. The last 100 hour inspection was accomplished 80 operating hours prior to the accident.
THE FAILURE OF THE CARBURETOR HEAT BOX ATTACH STRAPS WHICH ALLOWED THE CARBURETOR HEAT BOX TO SEPARATE FROM THE EXHAUST SYSTEM HEAT MUFF AND RENDERED THE CARBURETOR HEAT SYSTEM INOPERATIVE. THE ENGINE THEN LOST POWER DUE TO CARBURETOR ICE.
THE PILOT SAID WHILE IN LEVEL CRUISE ON AN IFR FLIGHT THE ENGINE BEGAN TO LOOSE POWER DUE TO CARBURETOR ICE AND ATTEMPTS TO REMEDY THE SITUATION WERE UNSUCCESSFUL WITH THE ENGINE EVENTUALLY LOOSING ALL POWER. THE PILOT DECLARED AN EMERGENCY WITH ALBUQUERQUE CENTER AND WAS RADAR VECTORED TOWARD THE SHOW LOW AIRPORT. THE FLIGHT WAS INTERMITTENTLY IN CLOUDS DURING THE EMERGENCY DESCENT AND BROKE OUT AT A LOW ALTITUDE. THE AIRCRAFT HAD INSUFFICIENT ALTITUDE TO MAKE THE AIRPORT AND LANDED IN THE ONLY AVAILABLE LOCATION, A FIELD ABOUT 23 MILES FROM THE AIRPORT. DURING ROLL OUT, THE AIRCRAFT COLLIDED WITH A DITCH AND NOSED OVER. POST ACCIDENT EXAMINATION OF THE AIRCRAFT BY FAA INSPECTORS REVEALED THAT THE CARBURETOR HEAT BOX HAD SEPARATED FROM THE HEAT MUFF OF THE EXHAUST SYSTEM AND WAS HANGING LOOSE IN THE COWLING ATTACHED ONLY BY THE FABRIC HOSE. A METAL BAND WHICH ATTACHES THE CARB HEAT BOX TO THE MUFF HAD SEPARATED. CHAFFING ON THE COWLING IN THE AREA OF WHERE THE HEAT BOX WAS HANGING INDICATED IT HAD BEEN SEPARATED FOR SOME TIME. THE LAST 100 HOUR INSPECTION WAS ACCOMPLISHED 80 OPERATING HOURS PRIOR TO THE ACCIDENT.