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2020-0274 : Electrical Power – Nickel-Cadmium Rechargeable Batteries – Replacement

Number 2020-0274
Issued by Europe  Europe
Issue date 2020-12-10
Effective date 2020-12-24
EASA approval number
Contributor EASA Large Aeroplanes Department
ATA Chapter 24
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
    • A330
      • A330-201
      • A330-202
      • A330-203
      • A330-223
      • A330-223F
      • A330-243
      • A330-243F
      • A330-301
      • A330-302
      • A330-303
      • A330-321
      • A330-322
      • A330-323
      • A330-341
      • A330-342
      • A330-343
      • A330-743L (BelugaXL)
      • A330-841
      • A330-941
    • A340
      • A340-211
      • A340-212
      • A340-213
      • A340-311
      • A340-312
      • A340-313
      • A340-541
      • A340-542
      • A340-642
      • A340-643
    • A380
      • A380-841
      • A380-842
      • A380-861
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus AOT A24N006-20 original issue dated 09 September 2020, or Revision 1 dated 12 October 2020. Airbus AOT A24L007-20 original issue dated 23 September 2020. Airbus AOT A24R009-20 original issue dated 23 September 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-164
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 12 October 2020 as PAD 20-164 for consultation until 26 October 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 Programming and Continued Airworthiness 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.