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.
Rock Springs, WY
The pilot stated he flew a total of 3 hours to two airports throughout the day. He stated that 5 miles from the third airport, he turned his landing light and carburetor heat on. Subsequently, both electrical and engine power were lost. The pilot stated he announced a "Mayday" call over the radio and performed a forced landing in hilly, rough terrain, resulting in substantial damage to the airplane. The pilot stated that after the impact he could immediately smell fuel in the cabin and was able to hear it dripping from the airplane. During the recovery of the airplane, one quart of fuel was recovered from the left wing. No further evidence of fuel was noted. An examination of the engine revealed no anomalies that would have precluded the engine from producing power prior to impact. The airplane battery was replaced and the electrical system functioned properly. An examination of the remaining systems revealed no anomalies.
the loss of engine power for reasons undetermined. Contributing to the accident was the dark night and lack of suitable terrain for a forced landing.
On November 15, 2005, approximately 1830 mountain standard time, a Cessna 172L, N2870Q, operated by Fremont Motor Company, was substantially damaged when it impacted terrain during a forced landing 4 nautical miles northeast of Sweetwater County Airport (RKS), Rock Springs, Wyoming. Night visual meteorological conditions prevailed at the time of the accident. The business flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The private pilot reported no injuries. The cross-country flight departed Lander, Wyoming, approximately 1745. According to the NTSB Pilot/Operator Aircraft Accident Report Form (6120.1/2) submitted by the pilot, he departed Rawlins, Wyoming (RWL), on the morning of the accident and had flown to Powell, Wyoming, (POY) for a business meeting. The pilot stated that he departed POY approximately 1600, and flew to Lander, Wyoming (LND). He departed LND for RKS approximately 1745. He stated that 5 miles from the airport, he turned his landing light and carburetor heat on. Subsequently, both electrical and engine power were lost. The pilot stated he announced a "Mayday" call over the radio and performed a forced landing in hilly, rough terrain. The airplane nosed over during the forced landing, coming to rest inverted in a ravine. Both wings were bent down and wrinkled and the left main landing gear assembly separated from the fuselage. The nose wheel separated from the strut and the firewall was winkled. The airplane was recovered and relocated to a hangar in Greeley, Colorado. During recovery, one quart of fuel was recovered from the left wing. No further evidence of fuel was noted. An examination of the engine revealed no anomalies that would have precluded the engine from producing power prior to impact. The airplane master switch had been left on and the battery was dead. The airplane battery was replaced and the electrical system functioned properly. An examination of the remaining systems revealed no anomalies. In a telephone interview with the pilot, he stated that after the impact, he egressed through the front windscreen. The pilot stated that he could immediately smell fuel in the cabin and was able to hear it dripping from the airplane. The pilot stated that he visually verified full fuel tanks prior to departure from RWL, and during his preflight in POY, measured 15 to 16 gallons of fuel in each tank. Fuel consumption calculations, based on calm winds, revealed that the flight activity of the day should have consumed 29 gallons of fuel, leaving approximately 9 gallons on board. The pilot stated that he did not obtain a weather briefing, did not obtain winds aloft, and did not calculate the fuel consumption for the flight.