| Number |
CF-2004-05R2 |
| Issued by |
 Canada |
| Issue date |
2005-06-01 |
| Effective date |
2005-06-30 |
| EASA approval number |
|
| ATA Chapter |
64 |
Approval Holder
/ Type Designation |
-
BELL TEXTRON CANADA LTD (BTCL)
-
206
-
206A
-
206B
-
206L
-
206L-1
-
206L-3
-
206L-4
|
| Revision |
This AD revises TCCA AD CF-2004-05R1, dated 28 June 2004, to introduce more stringent tail rotor skin damage limits, and re-balance requirements as specified in “Part F”.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes TCCA AD CF-2004-05R1, dated 28 June 2004.
|
| Publication(s) and related information |
BHTC ASB 206-04-100, Revision C, or ASB 206L-04-127, Revision C, as applicable, or later revisions approved by Chief, Continuing Airworthiness, Transport Canada |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
