| Number |
2011-0109 |
| Issued by |
 Europe |
| Issue date |
2011-06-15 |
| Effective date |
2011-06-17 |
| EASA approval number |
|
| ATA Chapter |
63 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
This AD has been republished to remove the P/N 92351-15100-045 Main
Module from the Applicability. This can only be installed in combination with a
P/N 92351-15310-041 MGB upper housing assembly, which is a ‘Phase III’
component that is not known to be affected by this unsafe condition. This AD
has also been corrected to clarify that the aft MGB mounting foot rib does not
need to be inspected.
|
| Supersedure |
This AD deviates from and thereby replaces (State of Design) FAA AD 2011-12-03
for affected helicopters registered in an EU Member State or associated country.
|
| Publication(s) and related information |
Sikorsky ASB 92-63-025 dated 11 May 2011, or ASB 92-63-025A dated 12
May 2011, or ASB 92-63-025B dated 20 May 2011.
Sikorsky S-92A MM SA S92A-AWL-000, TR No.5-87 dated 12 May 2011.
Sikorsky S-92A MM SA S92A-AMM-000, TR No.63-32 dated 11 May 2011. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The required actions and the risk allowance have granted the issuance of a
Final AD with Request for Comments, postponing the public consultation
process after publication.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail: ADs[@]easa.europa[dot]eu.
|
