Safety Publications Tool

2021-0049 : Fire Protection – Operational Limitation Doors – Cargo Door Seals – Cleaning / Greasing / Replacement

Number 2021-0049
Issued by Europe  Europe
Issue date 2021-02-18
Effective date 2021-03-04
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 26, 52
Approval Holder
/ Type Designation
  • AIRBUS
    • 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
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
      • A320-251N
      • A320-252N
      • A320-253N
      • A320-271N
      • A320-272N
      • A320-273N
    • A321
      • A321-111
      • A321-112
      • A321-131
      • A321-211
      • A321-212
      • A321-213
      • A321-231
      • A321-232
      • A321-251N
      • A321-251NX
      • A321-252N
      • A321-252NX
      • A321-253N
      • A321-253NX
      • A321-271N
      • A321-271NX
      • A321-272N
      • A321-272NX
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2020-0133 dated 10 June 2020.
Publication(s) and related information Airbus TA 80774334/003/2020 issue 01 dated 01 April 2020 and issue 03 dated 23 June 2020. Airbus SB A320-52-1195 original issue dated 12 October 2020. Airbus SB A320-52-1196 original issue dated 12 October 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-177
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 06 November 2020 as PAD 20-177 for consultation until 04 December 2020. 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.