EASA Mandates Prompt Detailed Visual Inspections Of The Wings Of 20 A380s | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.24.25

AirborneNextGen-
11.18.25

Airborne-Unlimited-11.19.25

Airborne-AffordableFlyers-11.20.25

AirborneUnlimited-11.21.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Sat, Jan 21, 2012

EASA Mandates Prompt Detailed Visual Inspections Of The Wings Of 20 A380s

Airplanes Which Have Completed Over 1300 Flights Are Covered By The AD

EASA published an AD on Friday mandating a prompt detailed visual inspection of the wings of 20 Airbus A380.

This inspection, which applies to aircraft that have already completed more than 1300 flights, will have to be performed within six weeks of 24 January 2012. Aircraft that have completed more than 1800 flights will have to be inspected within four days of this date.

EASA and Airbus are working closely together to ensure the continuing safe operations of the A380 aircraft type. In accordance with EASA, Airbus has established a repair scheme if cracks are found during the inspection.

According to the AD (EASA AD No. 2012-0013):

Following an unscheduled internal inspection of an A380 wing, some rib feet have been found with cracks originating from the rib to skin panel attachment
holes (Type 1 cracks according to Airbus All Operator Telex (AOT) terminology). Further to this finding, inspections were carried out on a number of other
aeroplanes where further cracks have been found. During one of those inspections, a new form of rib foot cracking originating from the forward and aft edges of the vertical web of the rib feet has been identified (Type 2 cracks according to Airbus AOT terminology). The new form of cracking is more significant than the original rib foot hole cracking. It has been determined that the Type 2 cracks may develop on other aeroplanes after a period of time in service.

This condition, if not detected and corrected, could potentially affect the structural integrity of the aeroplane.

For the reasons described above, this AD requires a Detailed Visual Inspection (DVI) of certain wing rib feet. This AD also requires reporting the inspection results to Airbus.

This AD is considered to be an interim action to immediately address this condition.

EASA continues to review the situation closely. As a result of the on-going investigation, further mandatory actions may be considered.

FMI: http://easa.europa.eu

Advertisement

More News

Classic Aero-TV: Pure Aerial Precision - The Snowbirds at AirVenture 2016

From 2016 (YouTube Edition): The Canadian Forces Snowbirds Can Best Be Described As ‘Elegant’… EAA AirVenture 2016 was a great show and, in no small part, it was>[...]

NTSB Final Report: Costruzioni Aeronautiche Tecna P2012 Traveller

Airplane Lunged Forward When It Was Stuck From Behind By A Tug That Was Towing An Unoccupied Airliner Analysis: At the conclusion of the air taxi flight, the flight crew were taxii>[...]

ANN's Daily Aero-Linx (11.23.25)

Aero Linx: International Stinson Club So you want to buy a Stinson. Well the Stinson is a GREAT value aircraft. The goal of the International Stinson Club is to preserve informatio>[...]

ANN's Daily Aero-Term (11.23.25): Request Full Route Clearance

Request Full Route Clearance Used by pilots to request that the entire route of flight be read verbatim in an ATC clearance. Such request should be made to preclude receiving an AT>[...]

Aero-News: Quote of the Day (11.23.25)

"Today's battlefield is adapting rapidly. By teaching our soldiers to understand how drones work and are built, we are giving them the skills to think creatively and apply emerging>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC