Cessna Caravan Reached 350kt in Unrecovered Post-Skydive Dive, NTSB Says

The key change on the Cessna 208B Grand Caravan’s sixth skydiving flight was how quickly its descent departed from the pattern of the five earlier flights. After initially following a similar profile for about 14 seconds, the aircraft entered a near-vertical dive and reached 350kt before impact. The National Transportation Safety Board says the pilot did not recover the aircraft.

The crash occurred near Youngstown, New York, on 20 July 2024, during a skydiving festival at Windsor airport. The pilot was the sole occupant after the skydivers had exited. The pilot did not survive.

A familiar profile changed on the sixth flight

On each of the first five flights that day, the Caravan climbed and levelled at about 10,000–13,000ft before the skydivers jumped. The aircraft then began a steep descent, with its rate reaching 7,500–10,000ft per minute. Before landing, the pilot reduced the descent rate to about 2,500–5,000ft per minute.

The sixth flight began in a similar way, but the descent did not remain within that earlier pattern. After roughly 14 seconds, the aircraft pitched into what the NTSB describes as a “near vertical” dive. Its descent rate rose to 35,000ft per minute, and its speed reached 350kt—far above the aircraft’s maximum operating speed. The airplane struck the ground without recovering.

That comparison with the previous flights gives the accident sequence its central detail: a steep post-jump descent had been part of the day’s flying, but the final descent continued well beyond the earlier profiles. The report says the pilot would have had only six seconds to recover after the descent passed those earlier profiles and before the airplane reached its maximum operating speed.

Trim position and the limits of the findings

Investigators found the elevator trim in the full nose-down position. The airplane’s electric and manual trim controls could not be tested because of damage. The inquiry nevertheless assessed that the trim was likely “intentionally placed into this position” to help initiate and maintain the descent.

The report does not establish what control forces the pilot would have needed to pull out of the dive. It says that amount could not be determined. It also notes that the post-crash examinations indicated pitch trim and engine power conditions that, after the airplane exceeded its operating speed limit, likely left the pilot unable to regain control.

Those findings distinguish what investigators could observe from what they could not reconstruct. The trim’s final position was documented, but the damaged controls could not be operated to establish their function. Nor could the investigation quantify the force needed to recover. The report’s account therefore links the aircraft’s speed, trim position and engine power indications while leaving the precise control inputs and forces unresolved.

Overspeed and aircraft condition

The NTSB says excessive speed can lead to flight-control flutter, damage or structural failure. Flight-control cable continuity could not be confirmed in this case. Investigators identified all primary and secondary flight-control surfaces in the wreckage except for an inboard section of the left flap.

The report describes the risks associated with exceeding the speed limit, but the available findings do not establish that flutter, control damage or structural failure caused the crash. The aircraft had already reached a speed far above its maximum operating limit while descending at an extreme rate. The report’s conclusion is that the pilot likely could not regain control once the limit was exceeded, given the trim and engine power indications found after the accident.

Pilot and aircraft details

The pilot had been flying with the operator for three months. The NTSB records 1,449 total flight hours, including 102 hours in type. The aircraft, registration N1259K, was built in 2002.

For operators reviewing the event, the report’s most specific operational marker is the six-second interval between the descent moving beyond the earlier flight profiles and the aircraft reaching its maximum operating speed. The inquiry also leaves important limits on the record: damaged trim controls could not be tested, the required recovery force could not be calculated, and cable continuity could not be confirmed.

The sequence documented by investigators is clear in its broad outline: after the jump, the Caravan initially descended much like it had on five earlier flights, then entered a near-vertical dive, exceeded its speed limit and hit the ground. The aircraft’s trim position and the rapid loss of recovery time frame the findings, while the report does not resolve every control detail.

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