Safety Publications Tool
2017-0129R1 : Integrated Modular Avionics – Internal Timer – Power Cycle (Reset)
EASA approval number
EASA Large Transport Aeroplanes Section
/ Type Designation
This AD revises EASA AD 2017-0129 dated 25 July 2017.
Publication(s) and related information
Airbus AOT A42P001-17 original issue dated 30 June 2017. Airbus SB A350-42-P010 original issue dated 14 August 2018. The use of later approved revisions of these 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 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.
EASA_AD_2017_0129_R1.pdf (494 kb)
EASA_AD_2017_0129.zip (1 mb)
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