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.
Sedona, AZ
The pilot was providing for hire sightseeing tours of a scenic area of Sedona, Arizona, in a vintage biplane. The front cockpit had been modified to accommodate two passengers. No record of an approved seat modification in accordance with factory specifications or a FAA field approval was located. The pilot stated that he departed with 10 gallons of fuel on board for a 30 minute tour. He could not say how the fuel was distributed in the tanks. He also said he did not use a dip stick or other measuring device to quantify the fuel level, but estimated the total fuel based on consumption estimates from prior flights. The airplane has two 25 gallon fuel tanks in the top wings with float sight gauges underwing. The aircraft maintenance manual states that 10 gallons of fuel is the minimum required for takeoff in the tank selected. Regarding the sight gauges, the manual states: 'An accurate reading cannot be obtained from the gasoline gauges on the ground'. Both gauges were contaminated with a tar like substance adhering to the wire indicators, which resembled an unidentified coating found inside the fuel tanks. Examination of the fuel system disclosed that only residual fuel remained in the fuel tanks and lines to the engine. Fuel system continuity was established.
FUEL EXHAUSTION DUE TO THE PILOTS INADEQUATE PREFLIGHT PLANNING AND HIS FAILURE TO REFUEL THE AIRPLANE PRIOR TO DEPARTURE. FACTORS IN THE ACCIDENT WERE: 1) THE UNRELIABLE FUEL SIGHT GAUGES WHICH WERE CONTAMINATED WITH A TAR LIKE RESIDUE WHICH MAY HAVE PROVIDED AN ERRONEOUS INDICATION OF FUEL IN THE SYSTEM, 2) INADEQUATE AIRPLANE MAINTENANCE, AND, 3) THE UNSUITABLE TREE COVERED NATURE OF THE TERRAIN WHERE THE FORCED LANDING WAS ATTEMPTED.
THE PILOT WAS PROVIDING FOR HIRE SIGHTSEEING TOURS OF A SCENIC AREA OF SEDONA, ARIZONA, IN A VINTAGE BIPLANE. THE FRONT COCKPIT HAD BEEN MODIFIED TO ACCOMMODATE TWO PASSENGERS. NO RECORD OF AN APPROVED SEAT MODIFICATION IN ACCORDANCE WITH FACTORY SPECIFICATIONS OR A FAA FIELD APPROVAL WAS LOCATED. THE PILOT STATED THAT HE DEPARTED WITH 10 GALLONS OF FUEL ON BOARD FOR A 30 MINUTE TOUR. HE COULD NOT SAY HOW THE FUEL WAS DISTRIBUTED IN THE TANKS. HE ALSO SAID HE DID NOT USE A DIP STICK OR OTHER MEASURING DEVICE TO QUANTIFY THE FUEL LEVEL, BUT ESTIMATED THE TOTAL FUEL BASED ON CONSUMPTION ESTIMATES FROM PRIOR FLIGHTS. THE AIRPLANE HAS TWO 25 GALLON FUEL TANKS IN THE TOP WINGS WITH FLOAT SIGHT GAUGES UNDERWING. THE AIRCRAFT MAINTENANCE MANUAL STATES THAT 10 GALLONS OF FUEL IS THE MINIMUM REQUIRED FOR TAKEOFF IN THE TANK SELECTED. REGARDING THE SIGHT GAUGES, THE MANUAL STATES: 'AN ACCURATE READING CANNOT BE OBTAINED FROM THE GASOLINE GAUGES ON THE GROUND'. BOTH GAUGES WERE CONTAMINATED WITH A TAR LIKE SUBSTANCE ADHERING TO THE WIRE INDICATORS, WHICH RESEMBLED AN UNIDENTIFIED COATING FOUND INSIDE THE FUEL TANKS. EXAMINATION OF THE FUEL SYSTEM DISCLOSED THAT ONLY RESIDUAL FUEL REMAINED IN THE FUEL TANKS AND LINES TO THE ENGINE. FUEL SYSTEM CONTINUITY WAS ESTABLISHED.