Safety Publications Tool
2017-0048 : [Correction] Fuselage – Aft Cargo Door Sill Beam Area – Inspection / Modification
EASA approval number
EASA Large Transport Aeroplanes Section
/ Type Designation
This AD is re-published to correct the compliance time description in Table 4.
This AD supersedes EASA AD 2015-0150, dated 23 July 2015.
Publication(s) and related information
Airbus AOT A53W005-14 original issue dated 22 April 2014, or Revision 01 dated 29 April 2014. Airbus SB A300-53-6179 original issue dated 12 December 2014. Airbus SB A310-53-2139 original issue dated 12 December 2014. Airbus SB A300-53-6181 original issue dated 26 June 2015, or Revision 01 dated 02 July 2015. Airbus SB A310-53-2141 original issue dated 26 June 2015, or Revision 01 dated 02 July 2015. The use of later approved revisions of these 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. This AD was posted on 21 July 2016 as PAD 16-110 for consultation until 18 August 2016. The Comment Response Document can be found at http://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
EASA_AD_2017_0048_C1.pdf (458 kb)
EASA_PAD_16_110.zip (2 mb)
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