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2019-0011R2 : Fuselage – Aft Fitting of Frame 40 – Inspection

Number 2019-0011R2
Issued by Europe  Europe
Issue date 2025-08-08
Effective date 2025-08-22
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300
      • A300B4-102
      • A300B4-103
      • A300B4-120
      • A300B4-203
      • A300B4-220
      • A300B4-2C
      • A300C4-203
      • A300F4-203
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
Revision This AD revises EASA AD 2019-0011R1 dated 22 February 2019 original issue of which superseded DGAC France AD F-1998-481-270R2 dated 12 November 2003 and DGAC France AD F-2000-038-032R1 dated 21 January 2004.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A300-53-0296 Revision 01 dated 30 September 1998. Airbus SB A300-53-6048 Revision 01 dated 30 September 1998, Revision 02 dated 12 May 1999, Revision 03 dated 21 February 2000, Revision 04 dated 26 February 2003 and Revision 05 dated 04 October 2018. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 18-170
Remarks 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 11 December 2018 as PAD 18-170 for consultation until 08 January 2019. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa[dot]europa[dot]eu. 4. 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.