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.
Brackettville, TX
The aircraft was departing from an airstrip on a ferry permit for an inoperable landing gear mechanism. The pilot reported that the aircraft's right engine failed at approximately 75 to 100 feet AGL during initial climb. The propeller was not of a type that could be feathered. He stated that he was unable to land on the remaining runway and elected to circle to land. During the circling maneuver, the pilot felt that he would be unable to return to the airstrip and attempted to align the aircraft for landing on a road ahead of the aircraft. During a steep right bank for this purpose the aircraft's right wing struck a power line, cartwheeled, and collided with the terrain. The on site inspection revealed that both engines were having some carburetor heat applied even though the control positions were off. The right carburetor inlet screen was very dirty and the accelerator pump was stuck at the one quarter throttle open position. This was not impact related.
AN ENGINE FAILURE CAUSED BY A MALFUNCTIONING CARBURETOR AND THE PILOT'S MISJUDGING HIS OBSTACLE CLEARANCE WHICH RESULTED IN A WIRE STRIKE WHILE MANEUVERING TO LAND. FACTORS IN THE ACCIDENT WERE THE UNCOMMANDED DEPLOYMENT OF CARBURETOR HEAT ON BOTH ENGINES, AN INOPERATIVE GEAR RETRACTION SYSTEM, AND A PROPELLER SYSTEM WHICH COULD NOT BE FEATHERED.
THE AIRCRAFT WAS DEPARTING FROM AN AIRSTRIP ON A FERRY PERMIT FOR AN INOPERABLE LANDING GEAR MECHANISM. THE PILOT REPORTED THAT THE AIRCRAFT'S RIGHT ENGINE FAILED AT APPROXIMATELY 75 TO 100 FEET AGL DURING INITIAL CLIMB. THE PROPELLER WAS NOT OF A TYPE THAT COULD BE FEATHERED. HE STATED THAT HE WAS UNABLE TO LAND ON THE REMAINING RUNWAY AND ELECTED TO CIRCLE TO LAND. DURING THE CIRCLING MANEUVER, THE PILOT FELT THAT HE WOULD BE UNABLE TO RETURN TO THE AIRSTRIP AND ATTEMPTED TO ALIGN THE AIRCRAFT FOR LANDING ON A ROAD AHEAD OF THE AIRCRAFT. DURING A STEEP RIGHT BANK FOR THIS PURPOSE THE AIRCRAFT'S RIGHT WING STRUCK A POWER LINE, CARTWHEELED, AND COLLIDED WITH THE TERRAIN. THE ON SITE INSPECTION REVEALED THAT BOTH ENGINES WERE HAVING SOME CARBURETOR HEAT APPLIED EVEN THOUGH THE CONTROL POSITIONS WERE OFF. THE RIGHT CARBURETOR INLET SCREEN WAS VERY DIRTY AND THE ACCELERATOR PUMP WAS STUCK AT THE ONE QUARTER THROTTLE OPEN POSITION. THIS WAS NOT IMPACT RELATED.