Sikorsky S-61N Safety Record
Complete NTSB accident and incident history. 6 events recorded from 1983 to 2025.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Jan 10, 2025 | Sédjè, OF | N703HG | Minor | substantial | Investigation pending |
| Sep 01, 2022 | Shady Cove, OR | N617CK | Minor | substantial | A total loss of engine power due to the failure of the No. 2 engine’s stage 1 turbine blades as a result of an unreported hot start two days earlier. |
| Feb 22, 2022 | Kekaha, HI | N615CK | Fatal (4) | destroyed |
The improper installation of the fore/aft primary servo by maintenance personnel, which resulted in the attaching hardware backing out and which subse…The improper installation of the fore/aft primary servo by maintenance personnel, which resulted in the attaching hardware backing out and which subsequently rendered the helicopter uncontrollable. Contributing to the accident was the company’s quality control personnel to identify the improper installation before certifying the helicopter for flight. |
| Aug 06, 2008 | Weaverville, CA | N612AZ | Fatal (9) | destroyed |
The following actions by Carson Helicopters: 1) the intentional understatement of the helicopter's empty weight, 2) the alteration of the power availa…The following actions by Carson Helicopters: 1) the intentional understatement of the helicopter's empty weight, 2) the alteration of the power available chart to exaggerate the helicopter's lift capability, and 3) the practice of using unapproved above-minimum specification torque in performance calculations that, collectively, resulted in the pilots relying on performance calculations that significantly overestimated the helicopter's load-carrying capacity and did not provide an adequate performance margin for a successful takeoff; and insufficient oversight by the U.S. Forest Service and the Federal Aviation Administration. Contributing to the accident was the failure of the flight crewmembers to address the fact that the helicopter had approached its maximum performance capability on their two prior departures from the accident site because they were accustomed to operating at the limit of the helicopter’s performance. Contributing to the fatalities were the immediate, intense fire that resulted from the spillage of fuel upon impact from the fuel tanks that were not crash resistant, the separation from the floor of the cabin seats that were not crash resistant, and the use of an inappropriate release mechanism on the cabin seat restraints. |
| Jul 19, 2008 | Cusco, PE | N91158 | Incident | substantial | Investigation pending |
| Oct 07, 1983 | WEST PALM BEACH, FL | YV323 | Serious (1) | destroyed | Investigation pending |