Safety Publications Tool
2014-0162R2 : Fuselage – 9° Upper Frame – Inspection
EASA approval number
EASA Rotorcraft Section
/ Type Designation
SA 365/366 / AS 365 / EC 155
AS 365 N2
AS 365 N3
SA 365 N
SA 365 N1
This AD revises EASA AD 2014-0162R1 dated 11 July 2014.
Publication(s) and related information
AH ASB AS365 05.00.68 original issue dated 07 April 2014, or Revision 1 dated 19 May 2015, or Revision 2 dated 20 December 2018. AH SB AS365-53.00.57 original issue dated 20 December 2018. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
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. 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.
EASA_AD_2014_0162_R2.pdf (513 kb)
EASA_AD_2014_0162.zip (2 mb)
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