Safety Publications Tool
2016-0105R2 : Fuselage – Cabin Floor Beam Junction - Inspection
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD revises EASA AD 2016-0105R1 dated 21 September 2018.
Publication(s) and related information
Airbus SB A320-53-1317 original issue dated 15 December 2015, or Revision 01 dated 19 June 2018. Airbus SB A320-53-1318 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018. Airbus SB A320-53-1319 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018. Airbus SB A320-53-1320 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018. Airbus SB A320-53-1351 original issue dated 20 December 2017. Airbus SB A320-53-1352 original issue dated 20 December 2017. Airbus SB A320-53-1353 original issue dated 20 December 2017. Airbus SB A320-53-1354 original issue dated 20 December 2017. Airbus SB A320-53-1433 original issue dated 28 June 2019. Airbus SB A320-53-1434 original issue dated 28 June 2019. Airbus SB A320-53-1435 original issue dated 28 June 2019. Airbus SB A320-53-1436 original issue dated 28 June 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 05 April 2016 as PAD 16-048 for consultation until 19 April 2016. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, 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 AD 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_AD_2016_0105_R2.pdf (210 kb)
EASA_PAD_16_048.zip (2 mb)
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