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ADs [at] easa.europa [dot] eu
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| Number |
20-184 |
| Issued by |
 Europe |
| Issue date |
2020-11-24 |
| EASA approval number |
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| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
22, 27, 31, 34 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This PAD proposes to supersede EASA AD 2019-0051R1 dated 25 March 2019.
|
| Publication(s) and related information |
Boeing Special Attention SB 737-00-1028 original issue dated 20 July 2020.
Boeing Alert Requirements Bulletin 737-22A1342 RB dated 17 November 2020.
Boeing Special Attention SB 737-27-1318 original issue dated 10 June 2020, or Revision 1 dated 24 June 2020, and Revision 2 dated 10 November 2020.
Boeing SB 737-27-1320 original issue dated 14 October 2020.
Boeing Special Attention SB 737-31-1860 original issue dated 12 June 2020, or Revision 1 dated 02 July 2020.
Boeing SDB-737-001 Revision G dated 09 November 2020.
Boeing SDB-737-006 original issue dated 03 June 2019.
Boeing SDB-737-007 original issue dated 13 June 2019.
EASA-approved Boeing 737 MAX B-737-8/-9 MMEL, Boeing document D639A001-02, Revision 2 [to be published].
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 22 December 2020.
2. Enquiries regarding this PAD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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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