Safety Publications Tool

2022-0060 : Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 / Certification Maintenance Requirements – Amendment

Number 2022-0060
Issued by Europe  Europe
Issue date 2022-04-01
Effective date 2022-04-15
EASA approval number
ATA Chapter 05
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
      • A300F4-622R
    • A300-600ST (Beluga)
      • A300F4-608ST
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus A300-600 (including A300-600ST) ALS Part 3 Revision 1, Variation 1.2, dated 16 December 2021. Airbus A310 ALS Part 3 Revision 1, Variation 1.2, dated 16 December 2021. The use of later approved revisions or variations of the above-mentioned documents, or of an ALS revision which includes the technical content of the Variation(s), is acceptable for compliance with the requirements of this AD.
PAD number 22-009
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 31 January 2022 as PAD 22-009 for consultation until 28 February 2022. 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.