| Number |
CF-2008-11R1 |
| Issued by |
 Canada |
| Issue date |
2008-05-28 |
| Effective date |
2008-05-28 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
-
DHC-8
-
DHC-8-400
-
DHC-8-401
-
DHC-8-402
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes Transport Canada AD CF-2008-11 dated 5 February 2008, to require the removal of the affected barrel nuts and the application of Type 2 Corrosion Inhibiting Compound.
|
| Publication(s) and related information |
Bombardier Inc. ASB A84-57-19 dated 1 February 2008, or ASB A84-57-19 Revision A, dated
06 February 2008, or ASB A84-57-19, Revision B, dated 6 March 2008, or later revisions, approved by the Chief, Continuing Airworthiness.
|
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu. At the moment of adoption of this AD, the model 400 has not been validated in Europe.
|
