Casualties unknown

1986-01-09: Boeing 727-232 (N403DA) — Delta Air Lines,inc. — Memphis, TN

Memphis, TN, US

On January 9, 1986, a Boeing 727-232 (registration N403DA) operated by Delta Air Lines,inc. was involved in an aviation accident near Memphis, TN. Investigators recorded the probable cause as: The left main landing gear outer cylinder failed from fatigue, initiated by a stress corrosion crack on the outer diameter of the strut cylinder where a strap had obscured the corrosion. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards
Boeing 727-232
Photo: Pete Macklin / CC BY-SA 2.0, via Wikimedia Commons

After takeoff, left main gear unsafe indication led to return to Memphis. Landing gear outer cylinder failed from fatigue due to stress corrosion crack. Emergency evacuation initiated but left forward door slide failed to deploy.

Incident Summary

Following takeoff, the flight crew encountered a landing gear malfunction. When the gear was retracted, the left main gear indicated an unsafe condition, and an unsafe door indication also appeared. The crew attempted to recycle the gear, but the same indications persisted. The gear handle was then placed in the neutral position, and the left main gear extended to a down and locked position. The captain decided to return to Memphis for a precautionary landing. After the gear extension cycle, all gear indicated down and safe, and tower personnel confirmed that the gear appeared to be down.

Sequence of Events

Upon touchdown, the left wing began settling, but the crew was able to keep the aircraft on the runway. An emergency evacuation was initiated; however, the slide at the left forward door did not inflate. No pressure was found in the inflation bottle for that slide, and no reason could be determined for the loss of pressure.

Investigation Findings

An investigation revealed that the left main landing gear outer cylinder, part number 65-57901-19, had failed from fatigue. A stress corrosion crack had initiated on the outer diameter of the strut cylinder, where a strap had obscured the corrosion. There was no history of a hard landing.

Probable cause

The left main landing gear outer cylinder failed from fatigue, initiated by a stress corrosion crack on the outer diameter of the strut cylinder where a strap had obscured the corrosion.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010110X00111. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.