No fatalities

Atlas Air Cargo Boeing 747-400F Loses Fore-Flap Section on Approach to Miami (N498MC)

Miami, FL, United States

On May 17, 2010, a BOEING 747 400F (registration N498MC) operated by ATLAS AIR INC was involved in an aviation accident near Miami, FL. No fatalities were reported. Investigators recorded the probable cause as: Extensive corrosion byproducts covered the lubrication passage in the fore flap attachment fitting, preventing passage of grease to the bearing, causing extensive corrosion in the bore and propagated by fatigue before final ductile separation. This summary draws on records from NTSB; 16 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards
BOEING 747 400F
Photo: Tosaka / CC BY 3.0, via Wikimedia Commons

On May 17, 2010, an Atlas Air Cargo Boeing 747-400F (N498MC) lost a section of its fore-flap while approaching Miami International Airport. The flap portion impacted the fuselage, causing substantial damage, but no crew injuries were reported. The aircraft landed safely.

Incident Summary

On May 17, 2010, an Atlas Air Cargo Boeing 747-400F, registration N498MC, was on approach to Miami International Airport (KMIA), Miami, Florida. The cargo flight had originated from Rio de Janeiro-Galeão-Antonio Carlos Jobim International Airport (BGL) in Rio de Janeiro, Brazil. During the approach, after selecting 30 degrees of flaps, the flight crew heard and felt a large impact. A section of the left fore-flap separated from the aircraft. The flap portion struck the fuselage, resulting in substantial damage. The flight crew was not injured, and the aircraft landed without further incident.

Inspection Findings

A postflight inspection revealed that approximately twelve feet of the right wing inboard fore flap was missing. The missing section had caused substantial damage to the aft fuselage. The separated fore flap section was subsequently recovered for examination.

Examination Results

Examination of the recovered fore flap section showed that a large portion of the enamel was missing from the fore flap attachment fitting of the carriage assembly. There was a large amount of contamination and grease buildup around the lubrication fitting. Extensive corrosion byproducts covered the lubrication passage in the attachment, which prevented the passage of grease to the bearing. This resulted in extensive corrosion in the bore, which propagated by fatigue before the final ductile separation of the flap section.

Probable cause

Extensive corrosion byproducts covered the lubrication passage in the fore flap attachment fitting, preventing passage of grease to the bearing, causing extensive corrosion in the bore and propagated by fatigue before final ductile separation.

Contributing factors

Causes

Fatigue/wear/corrosionTrailing edge flaps — Failure

Other contributing factors

Damaged/degraded