| Number |
DCA-R2000-23B |
| Issued by |
New Zealand |
| Issue date |
2007-10-25 |
| Effective date |
2007-10-25 |
| EASA approval number |
|
| ATA Chapter |
27 |
Approval Holder / Type Designation |
-
ALPHA AVIATION CONCEPT LTD
-
HR 200
-
HR 200-100
-
HR 200-100 S
-
HR 200-120
-
HR 200-120 B
-
HR 200-160
-
R 2000
-
R 2100
-
R 2100 A
-
R 2112
-
R 2120 U
-
R 2160
-
R 2160 D
-
R 2160i
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes CAA NZ AD DCA/2000/23A, which superseded DGAC France AD 95-217 dated 11 November 1995. This AD also supersedes CAA NZ AD DCA/R2000/16 which superseded DGAC France AD 86-148R1 dated 26 November 1986.
|
| Publication(s) and related information |
Alpha Aviation Service Bulletin AA-SB27-003. |
| Remarks |
This AD is considered embodied if reinforced rudder bars are already installed in accordance with DCA/R2000/23, DCA/R2000/23A or DGAC F-1995-217. The installation of rudder bars P/N 27.40.31.010 and P/N 27.40.31.020 is a terminating action to the requirements of this AD. Enquiries regarding this AD should be referred to Safety Information Section, EASA. E-mail: ADs[at]easa.europa.eu.
|