Number |
2021-0084 |
Issued by |
Europe |
Issue date |
2021-03-19 |
Effective date |
2021-04-02 |
EASA approval number |
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Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
52 |
Approval Holder / Type Designation |
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Revision |
Not applicable
|
Correction |
Not applicable
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Supersedure |
For affected aeroplanes operated under EU regulation, this AD replaces FATA State of Design AD 2020-FATA-01020A-03, AD 2020-FATA-01020A-04, AD 2020-FATA-01020A-15 and AD 2021-FATA-01020A-01, which are not adopted by EASA.
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Publication(s) and related information |
Irkut RRJ-95 SB RRJ-52-00485- original issue dated 18 November 2020.
Irkut RRJ-95 AMM task 52-11-25-710-801 "Operational Test of the Snubber of the Emergency Power Assist System of the Forward (Aft) Entry Door" dated 05 March 2020.
Irkut RRJ-95 AMM task 52-12-25-710-801 "Operational Test of the Snubber of the Emergency Power Assist System of the Forward (Aft) Service Door" dated 05 March 2020.
Irkut RRJ-95 AMM task 52-11-15-900-801 "Removal/Installation of the Entry Door Support Arm" dated 31 December 2019.
Irkut RRJ-95 AMM task 52-12-15-900-801 "Removal/Installation of the Service Door Support Arm" dated 28 June 2019. |
PAD number |
21-006 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 29 January 2021 as PAD 21-006 for consultation until 26 February 2021. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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. 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.
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