Airworthiness directives › 2017-25-06
AD 2017-25-06 Airworthiness Directives; Airbus Airplanes
Models named: A318-111, -112, -121, -122, A319-111, -113, -114, -115, -131, -132. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 153724 was embodied in production. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Except as provided by paragraphs (h)(1) and (h)(2) of this AD: Within 72 months after the effective date of this AD, modify the fuselage structure at FR65, in accordance with the Accomplishment Instructions of the applicable service bulletin specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD. (1) For Model A318 and A319 series airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, as identified in Airbus Service Bulletin A320-53-1262, Revision 01, dated July 29, 2016: Airbus Service Bulletin A320-53-1262, excluding Appendix 01 and including Appendix 02, Revision 01, dated July 29, 2016. (2) For Model A320-211, -212, -214, -232, and -233 airplanes, as identified in Airbus Service Bulletin A320-53-1333, dated July 29, 2016: Airbus Service Bulletin A320-53-1333, excluding Appendix 01 and including Appendix 02, dated July 29, 2016. (3) For Model A321-211, -213, and -231 airplanes as identified in Airbus Service Bulletin A320-53-1334, dated July 29, 2016: Airbus Service Bulletin A320-53-1334, excluding Appendix 01 and including Appendixes 02 and 03, dated July 29, 2016.
Unsafe condition
This AD was prompted by reports of a vertical strut penetrating through the cabin floor during an emergency water landing and on airframe ground contact at certain speeds/accelerations. We are issuing this AD to prevent the central vertical strut at frame (FR) 65 from penetrating through the cabin floor in certain conditions, which could lead to injury of occupants and delays during an emergency evacuation.
Affected ADs
None.
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1