| Number |
US-2002-13-05R1 |
| Issued by |
 United States of America |
| Issue date |
2003-01-21 |
| Effective date |
2003-02-25 |
| EASA approval number |
|
| ATA Chapter |
|
Approval Holder
/ Type Designation |
-
AEROMETALS, INC.
-
FAA STC SH4801NM
-
FAA STC SH5055NM
-
STC EASA.IM.R.S.01065
-
MD HELICOPTERS INC (MDHI)
|
| Revision |
This AD revises FAA AD 2002-13-05 dated June 27, 2002, reducing the Applicability to include only certain tailboom S/N's and parts that are modified in accordance with either STC SH5055NM or SH4801NM.
|
| Correction |
This revised AD also corrects a typographical error and clarifies that a slippage mark needs to be reapplied to each bolt regardless of the outcome of the required torque test.
|
| Supersedure |
None
|
| Publication(s) and related information |
Aerometals SB-001, dated August 3, 2000, pertains to the subject of this AD. For a copy of this service information, contact Aerometals, 3920 Sandstone Drive, El Dorado Hills, California 95762, United States of America. |
| Remarks |
At the time of issuance of this AD, EASA records do not indicate that STC SH4801NM has been validated in Europe. Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu
|
