Incident Overview

Date: Friday 8 May 2009
Aircraft Type: Boeing 747-48EF
Owner/operator: Asiana Airlines
Registration Number: HL7419
Location: near Frankfurt International Airport (FRA) – ÿ Germany
Phase of Flight: Approach
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 3
Component Affected: Left wing flap (Inboard Fore Flap)Left wing flap (Inboard Fore Flap)
Investigating Agency: BFUBFU
Category: Accident
A Boeing 747-48EF cargo plane was experiencing a landing near runway 25L at Frankfurt International Airport when it encountered a sudden impact, resulting in a wing flap detachment. The plane rolled, leveled, and continued its approach without further issues. A significant section of the left wing flap was lost, with a fracture near the attachment point. Damage to the outer fuselage skin was observed, particularly around the fairing outlet and cargo door, and ribs showed heavy damage. The incident occurred on December 12, 2009, and the missing flap was located in a forest.A Boeing 747-48EF cargo plane was experiencing a landing near runway 25L at Frankfurt International Airport when it encountered a sudden impact, resulting in a wing flap detachment. The plane rolled, leveled, and continued its approach without further issues. A significant section of the left wing flap was lost, with a fracture near the attachment point. Damage to the outer fuselage skin was observed, particularly around the fairing outlet and cargo door, and ribs showed heavy damage. The incident occurred on December 12, 2009, and the missing flap was located in a forest.

Description

The Boeing 747-48EF cargo plane was on approach to runway 25L at Frankfurt International Airport, Germany. In the area of the outer marker to runway 25L at a height of 1400 ft AMSL the landing flaps were moved to the 30ø position. The approach speed at this time was 160 kt (IAS). Shortly after actuating the flap lever, the crew heard an impact sound and noticed vibrations. The plane rolled about 1ø to the left. The autopilot levelled out the incline and the aircraft continued its approach. The landing was without further problems on runway 25L. The aircraft then rolled to the parking position. It appeared a part of the left wing flap (Inboard Fore Flap) with dimensions of about 4.5 x 1 m was missing. The fracture was about half a metre to the left of the inner flap attachment. The remaining flap piece was twisted around the inner attachment point and was jammed between the attachment and the fuselage. Two connecting rods between of the front and middle landing flaps were broken or torn out. The outer fuselage skin of the aircraft was penetrated in the area between the fairing outlet and the rear cargo door over a length of 3.5 m. In this area, the ribs showed heavy damage. The missing flap part was located in a forest on December 12, 2009. Conclusions: “The flap fitting was destroyed by a pronounced vibration fracture, which probably originated in a corrosion cavity .”

Primary Cause

Pronounced vibration fracture, likely originating in a corrosion cavity.Pronounced vibration fracture, likely originating in a corrosion cavity.

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