Safety Publications Tool
2016-0106R2 : Fuselage – Frame 35.2A - Inspection
EASA approval number
EASA Large Transport Aeroplanes Section
/ Type Designation
This AD revises EASA AD 2016-0106R1 dated 20 December 2018.
Publication(s) and related information
Airbus SB A320-53-1315 original issue dated 13 January 2016, or Revision 01 dated 08 January 2019. Airbus SB A320-53-1316 original issue dated 13 January 2016, or Revision 01 dated 08 January 2019. Airbus SB A320-53-1355 original issue dated 20 December 2017, or Revision 01 dated 18 June 2019. Airbus SB A320-53-1356 original issue dated 20 December 2017, or Revision 01 dated 09 April 2019. Airbus SB A320-53-1437 original issue dated 06 December 2018. Airbus SB A320-53-1438 original issue dated 06 December 2018.
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 16-049 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_0106R2.pdf (206 kb)
EASA_PAD_16_049.zip (2 mb)
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