Inflight Decompression and Engine Cowling Separation During Cruise

Casualties unknown • Denver, CO, US

A crew experienced an inflight decompression and engine instrument failure while cruising at 37,000 feet, leading to an emergency diversion to Denver.

What happened

The aircraft was in cruise flight at 37,000 feet MSL when the crew heard a loud bang accompanied by significant airframe vibration. Following this event, the aircraft began to lose cabin pressurization. The engine instruments for the number two engine ceased functioning, prompting the crew to pull the number two emergency 'T' handle.

The crew donned oxygen masks and initiated a descent, diverting the flight to Denver. There were no injuries reported during the event.

The investigation

Post-landing inspections of the number two engine nacelle revealed that both the inboard and outboard main engine cowlings had separated from the aircraft. Investigators discovered an 18x6 inch hole in the fuselage at the pressure bulkhead, located just aft of the left wing. The left horizontal stabilator also sustained damage.

Detailed examination of the engine identified that a 4-inch-diameter high-pressure bleed air duct had separated from the high-pressure relief valve. The clamp intended to connect these components was missing and was not recovered during the investigation. Additionally, the wire bundle responsible for transmitting monitoring data from the number two engine to the cockpit was found to be cut. There was no evidence of an engine fire or a fire within the nacelle cavity.

Probable cause

The failure of a clamp connecting the high-pressure bleed air duct to the high-pressure relief valve caused high-pressure bleed air to discharge into the nacelle, leading to over-pressurization and the subsequent separation of the engine cowlings.

Frequently asked questions

What happened in the 2000-04-28 Douglas DC-8-62F accident near Denver, CO?

A crew experienced an inflight decompression and engine instrument failure while cruising at 37,000 feet, leading to an emergency diversion to Denver.

What aircraft was involved and where did it happen?

The accident on 2000-04-28 involved a Douglas DC-8-62F, registration N990CF, operated by Emery Worldwide Airlines, at Denver, CO.

What was the probable cause of the accident?

The failure of a clamp connecting the high-pressure bleed air duct to the high-pressure relief valve caused high-pressure bleed air to discharge into the nacelle, leading to over-pressurization and the subsequent separation of the engine cowlings.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20794. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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