Flap component separation on Boeing 747-400F during approach to Frankfurt

Casualties unknown • Frankfurt am Main, DE

A cargo Boeing 747-400F lost a portion of its left inboard fore flap during final approach to Frankfurt am Main due to fatigue and corrosion.

What happened

On October 8, 2014, a Boeing 747-400F cargo aircraft was on final approach to Frankfurt am Main, Germany, arriving from Moscow, Russia. While the crew was transitioning the flaps from 20° to 30° at an altitude of approximately 2,500 ft AMSL, they heard a noise similar to the landing gear extending. Immediately following this sound, the aircraft experienced a 7° left roll. The pilot disconnected the autopilot and manually maintained the ILS approach path. The aircraft landed without further incident, but upon reaching the parking position, the crew discovered that a section of the left inboard fore flap, measuring approximately 4.5 x 1 meters, was missing. There were no fatalities and no injuries to the four persons on board.

The investigation

The BFU examined the aircraft, the flight data recorder, and the cockpit voice recorder. Investigators recovered the detached flap component from a nearby forest. Laboratory analysis of the broken flap bracket, performed at the Technical University of Braunschweig, focused on the fracture surfaces. The investigation also reviewed historical data regarding similar incidents involving the 747-400 series, including a 2009 occurrence in Frankfurt where flap components struck the aircraft fuselage.

Findings

Technical analysis revealed that the failure was caused by corrosion fatigue. The fracture originated from a pit caused by corrosion on the inner surface of the bracket. The investigation found that the bracket, made of an EN AW 7075 aluminum alloy, exhibited clear fatigue striations under electron microscopy. The corrosion was particularly prominent in areas outside the lubrication groove of the bronze bushing. The fatigue crack propagated through the material until the remaining cross-section could no longer withstand the increased loads applied during flap extension, resulting in a final ductile failure. While the loss of the flap caused a loss of lift, the pilot was able to compensate manually during the landing.

Safety action

  • The aircraft operator should inspect the flap brackets on all Boeing 747-400 aircraft in accordance with revised manufacturer Service Bulletins and Service Letters.
  • The manufacturer should improve the corrosion resistance of the flap brackets, specifically in the area of the bearing seat.

Probable cause

The failure of the flap bracket was caused by a fatigue crack that originated from a corrosion pit on the internal surface of the component, leading to the separation of the flap section during flap deployment.

Frequently asked questions

What happened in the 2014-10-08 The Boeing Company B 747-400 F accident near Frankfurt am Main, DE?

A cargo Boeing 747-400F lost a portion of its left inboard fore flap during final approach to Frankfurt am Main due to fatigue and corrosion.

What aircraft was involved and where did it happen?

The accident on 2014-10-08 involved a The Boeing Company B 747-400 F, at Frankfurt am Main, DE.

What was the probable cause of the accident?

The failure of the flap bracket was caused by a fatigue crack that originated from a corrosion pit on the internal surface of the component, leading to the separation of the flap section during flap deployment.

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