Airworthiness Directive · Amendment 39-19268 · Fuselage
Airbus Airplanes
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, on which Airbus modification 44360 has not been embodied in production.
(1) Airbus Model A330-301, -321, -322, -341, and -342 airplanes, all manufacturer serial numbers on which Airbus Service Bulletin A330-53-3093 has been embodied in service, except those on which Airbus Service Bulletin A330-53-3145 has been embodied in service.
(2) Airbus Model A340-211, -212, -213 airplanes, all manufacturer serial numbers on which Airbus Service Bulletin A340-53-4104 has been embodied in service.
(3) Airbus Model A340-311, -312, and -313 airplanes, all manufacturer serial numbers on which Airbus Service Bulletin A340-53-4104 has been embodied in service.
We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-301, -321, -322, -341, and -342 airplanes; Model A340-200 series airplanes; and Model A340-300 series airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by reports of cracks on both left-hand (LH) and right-hand (RH) sides on certain frame (FR) locations. We are issuing this AD to address the unsafe condition on these products.
Within 30 days after the effective date of this AD, request instructions from the Manager, International Section, Transport Standards Branch, FAA, to address the unsafe condition specified in paragraph (e) of this AD; and accomplish the actions at the times specified in, and in accordance with, those instructions. Guidance can be found in Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) AD 2011-0171R1, dated January 11, 2013.
