Casualties unknown

Cargo Flight Endures Severe Clear Air Turbulence, Loses Engine and Wing Section (N810CK)

Denver, CO, US

On December 9, 1992, a Douglas DC-8-52 (registration N810CK) operated by Connie Kalitta Services was involved in an aviation accident near Denver, CO. Investigators recorded the probable cause as: AN ENCOUNTER WITH SEVERE CLEAR AIR TURBULENCE. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 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
Aircraft registered N810CK
Aircraft registered N810CK. Photo: Ken Fielding / CC BY-SA 3.0, via Wikimedia Commons

A cargo flight encountered severe clear air turbulence at FL310, causing separation of the number one engine and 19 feet of left wing leading edge, and structural damage to the number four engine pylon. The aircraft landed safely at Denver's Stapleton Airport.

Incident Overview

A cargo flight operating under 14 CFR Part 121 experienced a severe clear air turbulence event while in cruise at Flight Level 310, approximately 20 miles west of Denver, Colorado. The turbulence induced major fluctuations in airspeed and caused significant oscillations in both pitch and roll axes.

Sequence of Events

During the departures from controlled flight resulting from the turbulence, the number one engine and a 19-foot section of the left wing leading edge separated from the aircraft. Additionally, the number four engine pylon sustained a crack and extensive structural damage. The flight crew executed a precautionary descent and subsequently landed without further incident at Stapleton International Airport in Denver, Colorado.

Preceding Conditions

Prior to the occurrence, the flight had been experiencing light to occasionally moderate chop. The forecast for the area included moderate to severe turbulence, which aligned with the conditions encountered.

Damage Assessment

The damage was confined to the left wing leading edge and the number one engine, which completely detached, and the number four engine pylon, which was cracked but remained attached. The extent of the damage required a careful approach and landing, which the crew managed successfully.

Conclusion

The aircraft sustained substantial damage but was able to land safely. No further information regarding the aircraft type, registration, or occupants was provided in the official report.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X16147. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.