| Number |
2019-0244 |
| Issued by |
 Europe |
| Issue date |
2019-09-30 |
| Effective date |
2019-10-14 |
| EASA approval number |
|
| ATA Chapter |
76 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2019-0089 dated 25 April 2019.
|
| Publication(s) and related information |
GE Aviation Czech SB-H80-76-00-00-0036 Revision 02 dated 29 March 2018, and Revision 03 dated 12 April 2019.
GE Aviation Czech ASB-H80-76-00-00-0048, ASB-H85-76-00-00-0015 (single document), original issue dated 29 March 2019, and Revision 01 dated 12 April 2019.
GE Aviation Czech ASB-H80-76-00-00-0047, ASB-H85-76-00-00-0018 (single document), original issue dated 27 June 2019, Revision 01 dated 12 July 2019, Revision 02 dated 07 August 2019 and Revision 03 dated 27 September 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-158 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 16 August 2019 as PAD 19-158 for consultation until 13 September 2019. 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.
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