You are not logged in
  Safety Publications Tool

PAD 25-078R1 : Aircraft Flight Manual / Cabin Crew Operating Manual / Cabin Crew Data – Amendment

Please feel free to send us your comments by email at ADs [at] easa.europa [dot] eu

Number 25-078R1
Issued by Europe  Europe
Issue date 2025-06-03
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
      • A318-121
      • A318-122
    • A319
      • A319-111
      • A319-112
      • A319-113
      • A319-114
      • A319-115
      • A319-131
      • A319-132
      • A319-133
      • A319-151N
      • A319-153N
      • A319-171N
      • A319-173N
Revision This PAD is revised to indicate compliance time specified in paragraph (3) for A319 aeroplanes.
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus Certification Package (CP)666 Issue 1.0 AFM, EASA approval dated 06 September 2024. Airbus CIL ref 00A-030-00027548.0001001 dated 24 September 2024. Airbus A320 family CCD: - Cabin Aspects of Special Emphasis (CASE) ref SA01RP1804598, issue 06, dated 13 September 2024. - Difference Requirement Tables and Cabin Aspects of Special Emphasis ref. SA01RP1800465, issue 12, dated 16 September 2024. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Remarks 1. This Proposed AD will be closed for consultation on 10 June 2025. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. 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.