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For service information identified in this final rule, contact Airbus SAS, Airworthiness Office—EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone: 33 5 61 93 36 96; fax: 33 5 61 93 44 51; email: You may view this referenced service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA.For information on the availability of this material at the FAA, call 206-231-3195.The related investigative actions include a rotating probe test of the fastener holes for cracks and checking the hole diameter for certain diameters. You may examine the MCAI in the AD docket on the internet at We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting this AD as proposed except for minor editorial changes.We have determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM.We determined that this AD will not have federalism implications under Executive Order 13132.
FAA-2018-0025; or in person at the Docket Management Facility between 9 a.m.
Airbus has issued Service Bulletin A3, Revision 00, dated November 23, 2016.
The service information describes procedures for a modification of the fastener holes at rib 1, stiffeners 1 to 14, on both outer wings between FR 40 and FR 47 by cold-working and includes related investigative actions and corrective actions.
This AD requires modifying the fastener holes at certain locations, which includes related investigative actions and applicable corrective actions.
We are issuing this AD to address the unsafe condition on these products.