On October 25, 1994, Hultgreen died when her F-14A-95-GR,
BuNo 160390, Finding herself overshooting the landing area centerline, Hultgreen attempted to correct her approach by applying left rudder pedal, which caused the nose to disrupt the airflow over the left (inside) wing, as well as the airflow to the port engine intake. The port engine suffered a
compressor stall and lost power—a well-known deficiency characteristic of the F-14A's
TF30-P-414A engine when inlet air is no longer flowing straight into it. For this reason, the F-14
NATOPS flight manual warned against excess yaw. Loss of an F-14 engine results in asymmetric thrust, which can exceed rudder authority (the degree of control exerted over the aircraft), especially at low speeds. After aborting the approach, Hultgreen selected full afterburner on the remaining engine, causing an even greater asymmetry. This, combined with a high
angle of attack, caused an unrecoverable approach turn
stall and rapid wing drop to the left. The
radar intercept officer in the rear seat, Lt. Matthew Klemish, initiated ejection for himself and Hultgreen as soon as it was apparent the aircraft was becoming uncontrollable. First in the automated ejection sequence, Klemish survived. However, by the time Hultgreen's seat fired 0.4 seconds later, the plane had exceeded 90 degrees of roll, and she was ejected downward into the water, killing her instantly. On November 12, 19 days after the crash, the Navy salvaged the plane and recovered Hultgreen's body, still strapped into the ejection seat, from a depth of . As with most approaches to a carrier landing, Hultgreen's incident was videotaped by two cameras. The tape shows an overshooting turn onto final, then apparent engine failure, followed by an audible wave-off and gear-up command from the
landing signal officer. Segments shown on broadcast television concluded with the rapid sequence of aircraft stall, roll, crew ejections, and impact with the water. ==Accusations of unqualification==