| Number |
2019-0224 |
| Issued by |
 Europe |
| Issue date |
2019-09-06 |
| Effective date |
2019-09-20 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2011-0159 dated 26 August 2011 and EASA AD 2017-0163 dated 04 September 2017.
|
| Publication(s) and related information |
Fokker Services SBF100-32-158 original issue dated 02 October 2009.
Fokker Services SBF100-32-161 original issue dated 07 April 2011.
Fokker Services SBF100-32-172 original issue dated 25 June 2019.
Goodrich SB 41000-32-036 original issue dated 24 June 2019.
Fokker Services report SE-623 issue 8 dated 20 December 2010.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-150R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 30 July 2019 as PAD 19-150 and re-published on 01 August 2019 as PAD 19-150R1 for consultation until 27 August 2019. 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 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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