The committee investigating the crash were satisfied that the destructive error in 1989 was not relevant to the 1994 crash. Information provided from Boeing to the investigation led to the following conclusion regarding FADEC performance: "Data from the Digital Electronics Unit (DECU) of the second engine showed no evidence of torque or temperature exceedance and the matched power conditions of the engines post-impact indicate that there was no sustained emergency power demand. No other evidence indicated any FADEC or engine faults." It was expected that in a FADEC engine runaway, engine power would become asynchronous and mismatched. The investigation found the engines at the crash to have matched settings, decreasing the likelihood of a FADEC malfunction being involved.