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leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2019-24-01
leading to the decision not to take AD action similar to Federal Aviation Administration (FAA) AD 2020-01-15
2020-0090R1 : Indicating / Recording Systems – Integrated Control Panels – Modification; Airplane Flight Manual – Abnormal / Normal Procedures Sections – Amendment
EASA approval number
EASA Large Aeroplanes Department
/ Type Designation
This AD revises EASA AD 2020-0090 issued on 20 April 2020.
The original issue of this AD superseded EASA Emergency AD 2020-0020-E dated 05 February 2020, including its Correction dated 06 February 2020.
Publication(s) and related information
Airbus A350 AFM TR 123 Issue 1 dated 05 February 2020. Airbus A350 AFM TR 124 Issue 1 dated 02 April 2020. Airbus A350-31-P038 original issue dated 17 April 2020. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. Airbus FOT 999.0006/20 revision 02 dated 16 April 2020. Airbus A350 MMEL MER dated 09 April 2020, EASA approval reference D20008466, which is available at AirbusWorld.
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. 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.
EASA_AD_2020_0090_R1.pdf (573 kb)
EASA_AD_2020_0090.zip (2 mb)
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