| Number |
2016-0075R1 |
| Issued by |
 Europe |
| Issue date |
2022-03-24 |
| Effective date |
2022-04-07 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
-
AIRBUS DEFENCE & SPACE S.A.
-
CN-235
-
CN-235
-
CN-235-100
-
CN-235-200
-
CN-235-300
|
| Revision |
This AD revises EASA AD 2016-0075 dated 10 April 2016.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus D&S AOT-CN235-55-0001 original issue dated 16 December 2014, or Revision 1 dated 06 March 2015, or Revision 2 dated 10 March 2015.
Airbus D&S AOT-CN235-55-0003 original issue dated 22 December 2015.
Airbus D&S SB SB-235-55-0014C original issue dated 23 January 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-023 |
| 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 10 February 2016 as PAD 16-023 for consultation until 09 March 2016. No comments were received during the consultation period.
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.
|
