| Number |
CF-2002-13R2 |
| Issued by |
 Canada |
| Issue date |
2005-05-19 |
| Effective date |
2005-06-17 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
-
DHC-8
-
DHC-8-400
-
DHC-8-401
-
DHC-8-402
|
| Revision |
This AD revises TCCA AD CF-2002-13R1 issued 20 November 2002, to provide alternate inspection requirements for P/N 46500-5 up-lock assembly, in place of the life limit imposed by Revision 1 of this directive. In addition, a modified up-lock assembly, P/N 46500-7, has been introduced as a substitute for P/N 46500-3 or 46500-5 and is terminating action to this directive.
|
| Correction |
Not applicable
|
| Supersedure |
This revised AD supersedes TCCA AD CF-2002-13R1 issued 20 November 2002.
|
| Publication(s) and related information |
DHC-8 Series 400 AMM, PSM 1-84-2, Chapter 32-31-21; and Bombardier Alert SB A84-32-15, dated 04 February 2002, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada. |
| Remarks |
At the moment of adoption of this AD, the model 400 has not been validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu
|
