| Number |
2020-0254 |
| Issued by |
 Europe |
| Issue date |
2020-11-13 |
| Effective date |
2020-11-27 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
BAE SYSTEMS (OPERATIONS) LTD
-
AVRO146RJ
-
100
-
100A
-
115
-
70
-
70A
-
85
-
85A
-
BAE146
-
100
-
100A
-
200
-
200A
-
300
-
300A
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes UK CAA AD G-002-07-2001 dated 01 July 2001, UK CAA AD G-2004-0004 dated 26 February 2004, UK CAA AD G-2005-0009 dated 09 March 2005, EASA AD 2007-0307 dated 17 December 2007, EASA AD 2008-0168 dated 02 September 2008, EASA AD 2011-0097 dated 25 May 2011, EASA AD 2012-0106 dated 14 June 2012 and EASA AD 2014-0071 dated 19 March 2014.
|
| Publication(s) and related information |
BAE Systems (Operations) Ltd BAe 146/AVRO 146-RJ AMM Revision 127 dated 15 January 2020.
BAE Systems (Operations) Ltd CPCP Doc. No. CPCP-146-01 Revision 6 dated 15 November 2016.
BAE Systems (Operations) Ltd SSID Doc. No. SSID-146-01 Revision 6 dated 15 March 2017.
BAE Systems (Operations) Ltd MRBR Doc. No. MRB 146-01 Issue 2 Revision 26 dated August 2018.
BAE Systems (Operations) Ltd SRM Doc. No. 146RJ-SRM-E12 Revision 70 dated 15 October 2019.
BAE Systems (Operations) Ltd SRM Doc. No. 146RJ-SRM-E3 Revision 48 dated 15 October 2019.
BAE Systems (Operations) Ltd ISB ISB.53-237 Revision 2 dated 10 June 2014.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-162 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 12 October 2020 as PAD 20-162 for consultation until 09 November 2020. No comments were received during the consultation period.
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.
|
