| Number |
2021-0039R2 |
| Issued by |
 Europe |
| Issue date |
2021-02-17 |
| Effective date |
2021-02-17 |
| EASA approval number |
|
| ATA Chapter |
22, 27, 31, 34 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2021-0039R1 dated 03 February 2021.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2019-0051R1 dated 25 March 2019.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, or Revision 1 dated 23 December 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 dated 25 September 2020, EASA approved on 23 December 2020.
Boeing 737 document D626A014 (Operational Suitability Data - Flight Crew) Revision NEW dated 24 November 2020, EASA approved on 22 December 2020.
Boeing 737 document D626A014-1 (Operator Difference Requirement Tables) Revision NEW dated 24 November 2020, EASA approved on 22 December 2020.
Boeing 737 MAX B-737-8/-9 AFM, Boeing document D631A002 (operator-customised AFM applies), EASA approved on 22 December 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-184 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 24 November 2020 as PAD 20-184 for consultation until 22 December 2020. 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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