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2021-0234R1 : Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification

Number 2021-0234R1
Issued by Europe  Europe
Issue date 2023-05-11
Effective date 2023-05-18
EASA approval number
ATA Chapter 46
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A318
      • A318-111
      • A318-112
    • A319
      • A319-111
      • A319-112
      • A319-114
      • A319-115
      • A319-132
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-231
      • A320-232
      • A320-251N
    • A321
      • A321-211
      • A321-231
      • A321-232
      • A321-251N
      • A321-253N
    • A330
      • A330-202
      • A330-223
      • A330-243
      • A330-322
      • A330-343
    • A340
      • A340-312
      • A340-313
      • A340-542
  • ATR
    • ATR42
      • 500
    • ATR72
      • 212
      • 212A
  • BOEING
    • 737
      • 737-300
      • 737-400
      • 737-500
      • 737-700
      • 737-800
      • 737-900ER
    • 757
      • 757-200
    • 767
      • 767-200
      • 767-300
    • 777
      • 777-200LR
  • BOMBARDIER
    • CL-600 (Challenger)
      • CL-600-2B16 (601-3A Variant)
      • CL-600-2B16 (601-3R Variant)
      • CL-600-2B16 (604 Variant)
  • DE HAVILLAND AIRCRAFT OF CANADA LTD.
    • DHC-8
      • DHC-8-202
      • DHC-8-311
      • DHC-8-314
      • DHC-8-315
      • DHC-8-402
  • FOKKER SERVICES
    • CRR-0146
    • CRR-0185
    • CRR-0186
    • CRR-0190
    • CRR-0206
    • CRR-0210
    • CRR-0241
    • CRR-0265
    • CRR-0290
    • CRR-0300
    • CRR-0309
    • EASA STC 10046185
    • EASA STC 10061825
    • ECR016073
    • F27
      • MARK050
    • F28
      • MARK0070
      • MARK0100
      • MARK3000
  • MHI RJ Aviation ULC
    • CL-600 (Regional Jet)
      • CL-600-2C10 (RJ 700)
      • CL-600-2C10 (RJ 701)
      • CL-600-2C10 (RJ 702)
Revision This AD revises EASA AD 2021-0234 dated 28 October 2021.
Correction Not applicable
Supersedure The original issue of this AD supersedes EASA AD 2018-0259R1 dated 07 February 2019.
Publication(s) and related information Fokker Services SBF50-46-006 dated 27 July 2018. Fokker Services SBF28-46-002 dated 27 July 2018. Fokker Services SBF100-46-008 dated 27 July 2018. Fokker Services EBA320-0167 Revision 4 dated 30 July 2021. Fokker Services EBA330-0011 dated 27 July 2018. Fokker Services EBA340-0005 dated 27 July 2018. Fokker Services EBAT72-0013 dated 27 July 2018. Fokker Services EBB737-0156 Revision 3 dated 25 February 2019. Fokker Services EBB757-0020 dated 27 July 2018. Fokker Services EBB767-0023 dated 27 July 2018. Fokker Services EBB777-0009 dated 27 July 2018. Fokker Services EBCL60-0010 Revision 1 dated 30 August 2018. Fokker Services EBDHC8-0035 dated 27 July 2018. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 21-137
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 22 September 2021 as PAD 21-137 for consultation until 20 October 2021. No comments were received during the consultation period. 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.