Engine failure during takeoff leads to runway excursion

No fatalities • Ieshima, Japan • Takeoff (climb)

An aircraft experienced a loss of power in its first engine during the takeoff roll, resulting in a deviation from the runway centerline and subsequent damage.

What happened

While performing the takeoff roll, the aircraft's number one engine experienced a mechanical failure. In response to the loss of power, the crew initiated an aborted takeoff procedure. However, the resulting asymmetric thrust caused the plane to drift away from the runway centerline. The aircraft veered toward the left side of the runway and exited the paved surface, eventually coming to a stop in a nearby grassy field.

Although the incident resulted in no injuries to those on board, the aircraft sustained significant damage. The structural impact was severe enough that the airframe was declared a total loss and was not repairable.

Findings

  • The primary factor in the excursion was the failure of the number one engine during the initial phase of takeoff.

Probable cause

The failure of the first engine during the takeoff roll created asymmetric thrust that prevented the crew from maintaining the runway centerline.

Frequently asked questions

What happened in the 1964-05-02 Lockheed C-130 Hercules accident near Ieshima, Japan?

An aircraft experienced a loss of power in its first engine during the takeoff roll, resulting in a deviation from the runway centerline and subsequent damage.

Were there any fatalities in the 1964-05-02 Lockheed C-130 Hercules accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1964-05-02 involved a Lockheed C-130 Hercules, registration 56-0492, operated by United States Air Force - USAF (since 1947), at Ieshima, Japan.

What was the probable cause of the accident?

The failure of the first engine during the takeoff roll created asymmetric thrust that prevented the crew from maintaining the runway centerline.

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