Number |
2017-0111 |
Issued by |
Europe |
Issue date |
2017-06-23 |
Effective date |
2017-06-30 |
EASA approval number |
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Contributor |
EASA Rotorcraft Section |
ATA Chapter |
05, 63 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
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Supersedure |
This AD supersedes EASA AD 2017-0050-E dated 17 March 2017.
|
Publication(s) and related information |
AH AS332 ASB 63.00.83 and EC225 ASB 63A030 (single document) Revision 1, dated 07 October 2016 and Revision 2 dated 23 June 2017.
AH AS332 ASB 05.01.07 Revision 2 dated 07 October 2016, Revision 3 dated 25 February 2017, and Revision 4 dated 17 March 2017 and Revision 5 dated 23 June 2017.
AH EC225 ASB 05A049 Revision 2 dated 07 October 2016, Revision 3 dated 25 February 2017, Revision 4 dated 17 March 2017 and Revision 5 dated 23 June 2017.
AH SB EC225-63-032 original issue dated 23 June 2017.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
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