Safety Publications Tool

2021-0221 : Air Conditioning – Belly Fairing Air Cooling Pack Discharge Duct Adjustable Rods – Replacement / Electrical Power – Generator and Ground Power Control Unit – Replacement / Software Update / Equipment / Furnishings – Modified Door Lining Panels – Installation / Fuel – Refuel Diffusers / Engine Feed Fuel Pipe End Fittings – Replacement / Fuselage – Nose Landing Gear Bay Bulkhead Panel – Inspection / Powerplant – Redesigned Fan Cowl Latch Access Panels – Installation

Number 2021-0221
Issued by Europe  Europe
Issue date 2021-10-01
Effective date 2021-10-15
EASA approval number
ATA Chapter 21, 24, 25, 28, 53, 71
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A380
      • A380-841
      • A380-842
      • A380-861
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus SB A380-21-8092 original issue dated 08 March 2018, or Revision 01 dated 19 December 2018. Airbus SB A380-21-8093 original issue dated 08 March 2018, or Revision 01 dated 19 December 2018. Airbus SB A380-24-8130 original issue dated 02 October 2017. Airbus SB A380-25-8195 original issue dated 04 April 2017. Airbus SB A380-25-8196 original issue dated 04 April 2017. Airbus SB A380-25-8197 original issue dated 04 April 2017. Airbus SB A380-25-8198 original issue dated 04 April 2017. Airbus SB A380-25-8199 original issue dated 04 April 2017. Airbus SB A380-25-8200 original issue dated 04 April 2017. Airbus SB A380-25-8201 original issue dated 04 April 2017. Airbus SB A380-25-8202 original issue dated 04 April 2017. Airbus SB A380-28-8047 original issue dated 02 September 2015. Airbus SB A380-28-8050 original issue dated 10 September 2015, or Revision 01 dated 09 January 2017, or Revision 02 dated 20 December 2017. Airbus SB A380-53-8122 original issue dated 23 August 2018. Airbus SB A380-71-8006 original issue dated 23 April 2013. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 21-092R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 25 June 2021 as PAD 21-092 for consultation until 23 July 2021 and thereafter re-published on 16 September 2021 as PAD 21-092R1 for additional consultation until 30 September 2021. No comments were received during the additional consultation period. The Comment Response Document for PAD 21-092 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.