Safety Publications Tool
21-137 : Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification
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ADs [at] easa.europa [dot] eu
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
CL-600-2B16 (601-3A Variant)
CL-600-2B16 (601-3R Variant)
CL-600-2B16 (604 Variant)
DE HAVILLAND AIRCRAFT OF CANADA LTD.
EASA STC 10046185
EASA STC 10061825
MHI RJ Aviation ULC
CL-600 (Regional Jet)
CL-600-2C10 (RJ 700)
CL-600-2C10 (RJ 701)
CL-600-2C10 (RJ 702)
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 EBDH8-0035 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.
1. This Proposed AD will be closed for consultation on 20 October 2021. 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.
EASA_PAD_21_137.pdf (232 kb)
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