| Number |
2007-0183R2 |
| Issued by |
 Europe |
| Issue date |
2007-11-07 |
| Effective date |
2007-07-16 |
| EASA approval number |
|
| Contributor |
EASA |
| ATA Chapter |
76 |
Approval Holder
/ Type Designation |
-
DIAMOND AIRCRAFT INDUSTRIES
|
| Revision |
This AD has been revised to extend the compliance time by one month, to 30 November 2007, and to include reference to an approved alternative method of compliance. Aircraft already in compliance with EASA AD 2007-0183 or its revision 1 are not affected by this change.
|
| Correction |
This AD has been republished to correct a typographical error.
|
| Supersedure |
This Airworthiness Directive (AD) revises and replaces EASA AD 2007-0183 R1 dated 28 August 2007.
|
| Publication(s) and related information |
Diamond Aircraft Industries (DAI) Mandatory Service Bulletin MSB-42-042; DAI WI-MSB-42-042; DAI Service Information SI 42-040;
DAI AFM TR-MÄM-42-240 and AMM-TR-MÄM-42-240;
TAE Installation Manual IM-02-01 Issue 4, Revision 1, Chapter 13 (02-IM-13-01); and
TAE Installation Manual IM-02-02 Issue 1, Revision 3, Chapter 13, (02-IM-13-02).
DAI Optional Service Bulletin OSB-42-050/1; DAI WI-OSB-42-050 Revision 2; and DAI AFM TR-OÄM-42-129 and AMM-TR-OÄM-42-129. |
| PAD number |
07-074 |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
