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.
New Milford, PA
During cruise, the engine lost partial power. The pilot stated he applied carburetor heat, and shortly thereafter, the engine lost all power. During an emergency landing on mountainous wooded terrain, the airplane 'clipped' trees and impacted the ground, then it slid about 30 ft and came to rest inverted. An exam of the airplane revealed no airframe anomalies. The engine was inspected and water was found in the gascolator, carburetor float bowl and accelerator pump housing; source of the water contamination was not determined. Mice were found in the carburetor air box and venturi area. One mouse was lodged in the throttle valve. Receipts showed the airplane received about 17 gallons of fuel on the day before the accident. Since then, the airplane had flown about 1 hr. The pilot said that before each flight, he drained each fuel drain. He said water was found in the fuel samples, but he continued to drain the fuel until no more water was detected.
LOSS OF ENGINE ENGINE POWER DUE TO WATER CONTAMINATION OF THE FUEL. FACTORS RELATED TO THE ACCIDENT WERE THE MICE, WHICH PARTIALLY BLOCKED FUEL AND AIR FLOW TO THE CARBURETOR, AND THE LACK OF SUITABLE TERRAIN IN THE EMERGENCY LANDING AREA.
DURING CRUISE, THE ENGINE LOST PARTIAL POWER. THE PILOT STATED HE APPLIED CARBURETOR HEAT, AND SHORTLY THEREAFTER, THE ENGINE LOST ALL POWER. DURING AN EMERGENCY LANDING ON MOUNTAINOUS WOODED TERRAIN, THE AIRPLANE 'CLIPPED' TREES AND IMPACTED THE GROUND, THEN IT SLID ABOUT 30 FT AND CAME TO REST INVERTED. AN EXAM OF THE AIRPLANE REVEALED NO AIRFRAME ANOMALIES. THE ENGINE WAS INSPECTED AND WATER WAS FOUND IN THE GASCOLATOR, CARBURETOR FLOAT BOWL AND ACCELERATOR PUMP HOUSING; SOURCE OF THE WATER CONTAMINATION WAS NOT DETERMINED. MICE WERE FOUND IN THE CARBURETOR AIR BOX AND VENTURI AREA. ONE MOUSE WAS LODGED IN THE THROTTLE VALVE. RECEIPTS SHOWED THE AIRPLANE RECEIVED ABOUT 17 GALLONS OF FUEL ON THE DAY BEFORE THE ACCIDENT. SINCE THEN, THE AIRPLANE HAD FLOWN ABOUT 1 HR. THE PILOT SAID THAT BEFORE EACH FLIGHT, HE DRAINED EACH FUEL DRAIN. HE SAID WATER WAS FOUND IN THE FUEL SAMPLES, BUT HE CONTINUED TO DRAIN THE FUEL UNTIL NO MORE WATER WAS DETECTED.