Safety Publications Tool
21-134 : Fuselage – Rear Cone Frame Feet 102/103 – Modification
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EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD supersedes EASA AD 2019-0220R1 dated 17 December 2019.
Publication(s) and related information
Airbus SB A380-53-8214 original issue dated 10 August 2021. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
1. This Proposed AD will be closed for consultation on 05 October 2021. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this PAD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
EASA_PAD_21_134.pdf (214 kb)
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