No fatalities

2012-10-13: McDonnell Douglas MD-11 (N988AR) — Centurion Air Cargo — Campinas-Viracopos, Brazil

Campinas-Viracopos, BrazilLanding (descent or approach)

On October 13, 2012, a McDonnell Douglas MD-11 (registration N988AR) operated by Centurion Air Cargo was involved in an aviation accident near Campinas-Viracopos, Brazil during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The landing gear failed due to overload in the cylinder structure. The fracture started in the rear section of the cylinder in a connection hole which served as a tension concentration point, and ended in the front part of the cylinder with its breakage into… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781194598Data APIEditorial standards
Aircraft registered N988AR
Aircraft registered N988AR. Photo: Leviescobar / CC BY 3.0, via Wikimedia Commons

A cargo flight from Miami to Viracopos experienced a left main landing gear collapse after touchdown, causing substantial damage. The three crew members were uninjured.

The Flight

An aircraft departed Miami International Airport (KMIA) on a non-regular cargo transport flight destined for Viracopos Airport (SBKP). On board were two pilots and a mechanic. The flight proceeded without incident until the approach to SBKP.

Landing Mishap

The crew conducted an IFR ILS Z approach for runway 15. Weather conditions were visual meteorological conditions (VMC), with wind from 140° at 19 knots. Upon receiving landing clearance, the wind was reported at 20 knots, gusting to 29 knots. The copilot served as pilot flying (PF) and the captain as pilot monitoring (PM). After the flare, the aircraft touched down, and the left main landing gear collapsed. The aircraft skidded approximately 800 meters before stopping, remaining within the runway limits. The left main gear assembly, left wing, and left engine sustained substantial damage. All three crew members were uninjured.

Probable Cause

The official investigation determined that the landing gear failed due to overload in the cylinder structure. The fracture originated in the rear section of the cylinder at a connection hole that acted as a tension concentration point, then propagated to the front, breaking the cylinder into two parts. Metallurgical analysis at Boeing Long Beach MP&P Laboratories identified characteristics similar to a pre-crack point at one origin of failure, likely from a previous overload. Following a prior incident in 2009 (a hard landing in Montevideo), the right main gear was replaced by VARIG Engineering & Maintenance (VEM), but the organization responsible for damage research, service specification, and airworthiness restoration was not identified. The pre-crack traces from the earlier overload may not have been detected during subsequent inspections and repairs, potentially creating a stress concentration.