Casualties unknown

Runway Excursion and Wheel Separation During ILS Approach (N921R)

Seattle, WA, US

On July 18, 1998, a Mcdonnell Douglas DC-8-63F (registration N921R) operated by Emery Worldwide Airlines was involved in an aviation accident near Seattle, WA. Investigators recorded the probable cause as: The flight crew's failure to perform a missed approach upon failing to attain and/or maintain proper course/runway alignment and glidepath on final approach, resulting in a high-sink-rate landing and subsequent separation of a main landing gear wheel from the… This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During an ILS approach in low ceiling, the aircraft deviated from the localizer and glide path. After breakout, a high sink rate led to a hard touchdown, causing a wheel to separate and strike ground vehicles.

Approach and Deviation

The flight was cleared for an instrument landing system (ILS) approach. The ceiling was 200 feet overcast, visibility was 1 mile, and runway visual range was greater than 6,000 feet. The first officer was the pilot flying; according to company operating procedures, the minimum ceiling for a first officer flying is normally 500 feet. Air traffic control radar indicated that the aircraft was left of the localizer course and/or below the glide path for the majority of the final approach segment below 1,000 feet above touchdown, deviating from the company's stabilized approach limits.

Breakout and Recovery

The aircraft broke out approximately at minimums (200 feet above touchdown), left of and diverging away from the runway centerline. The captain called out, "push it down, push it down, push it down" and asked, "you got it or you want me to get it?" The first officer replied, "I can get it," and the captain said, "OK." Subsequently, the aircraft pitched down and banked up to approximately 14 degrees while correcting back to the runway. A high sink rate existed in the last few seconds before touchdown; the flight data recorder registered a vertical acceleration of about 1.8 G at touchdown.

Wheel Separation and Damage

The aircraft's number 1 main landing gear wheel separated from the aircraft at or shortly after touchdown. The separated wheel entered the airport ramp area and struck two parked trucks and a baggage cart in front of the main passenger terminal.

Post-Incident Examination

Post-incident examinations of the aircraft's number 1 wheel retaining nut disclosed that the nut threads were worn approximately 0.030 inch beyond engineering drawing specifications.

Regulatory Context

FAA guidance directs FAA principal operations inspectors to ensure their operators' operations manuals contain stabilized approach criteria as well as required actions in the event of deviations ("i.e. missed approach or go/around [sic]"). The company's DC-8 operations manual states only that deviations from the stabilized approach profile "are cause for consideration to abandon the approach."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X10696. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.