Casualties unknown

MD-11 Left Elevator Damaged During Escape Maneuver in Response to False GPWS Warning (N588FE)

Subic Bay, RP

On June 3, 2002, a Mcdonnell Douglas MD-11 (registration N588FE) operated by Federal Express Corp was involved in an aviation accident near Subic Bay, RP. Investigators recorded the probable cause as: The elevator damage occurred as a result of an exceedance of the airplane's design aerodynamic stall buffet boundary, which led to a severe vibration of the elevator; the stall buffet boundary was exceeded as a result of the captain's initiation of the escape… 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
Aircraft registered N588FE
Aircraft registered N588FE. Photo: Maarten Visser from Capelle aan den IJssel, Nederland / CC BY-SA 2.0, via Wikimedia Commons

An MD-11 sustained structural damage to its left elevator after the flight crew initiated an aggressive escape maneuver in response to a false GPWS alert during heavy precipitation. The aircraft landed safely; no injuries were reported.

Incident Summary

On a flight operating an MD-11 aircraft, the flight crew initiated an abrupt maneuver while descending to land. The maneuver was triggered by a false ground proximity warning system (GPWS) alert that activated as the airplane encountered heavy precipitation at an altitude of approximately 9,800 feet above mean sea level. The GPWS warning subsided during the maneuver. The airplane subsequently landed without further incident. Both flight crewmembers, who were the sole occupants, were not injured.

Investigation Findings

The investigation determined that the escape maneuver was aggressive and consistent with procedures published in Federal Express' airplane flight manual for "GPWS Pull Up Warning." Post-flight inspection revealed that the outboard portion of the left elevator, including its balance weight, was partially separated. The flight crew reported no handling difficulties after the escape maneuver.

Further examination indicated that the elevator damage resulted from an exceedance of the airplane's design aerodynamic stall buffet boundary, which caused a severe vibration of the elevator. The stall buffet boundary was exceeded due to the captain's initiation of the escape maneuver. The false GPWS warning was prompted by false readings from the no. 1 and no. 2 radio altimeters, most likely caused by signal return off heavy precipitation. No mechanical deficiencies were found in the flight controls, avionics, or elevator structure after the event.

Probable cause

The elevator damage occurred as a result of an exceedance of the airplane's design aerodynamic stall buffet boundary, which led to a severe vibration of the elevator; the stall buffet boundary was exceeded as a result of the captain's initiation of the escape maneuver.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020604X00806. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.