| Number |
US-2010-01-04 |
| Issued by |
 United States of America |
| Issue date |
2010-04-30 |
| Effective date |
2010-04-30 |
| EASA approval number |
|
| ATA Chapter |
72, 73 |
Approval Holder
/ Type Designation |
-
GENERAL ELECTRIC
-
CF34
-
CF34-1A
-
CF34-3A
-
CF34-3A1
-
CF34-3A2
-
CF34-3B
-
CF34-3B1
|
| Revision |
Not applicable
|
| Correction |
The FAA is correcting airworthiness directive (AD) 2010-01-04, which published in
the Federal Register. That AD applies to GE CF34-1A, CF34-3A, and CF34-3B series turbofan
engines. The docket number is incorrect in all three of its locations. This document corrects those
references. In all other respects, the original document remains the same.
|
| Supersedure |
This AD supersedes AD 2009-24-11. This AD supersedure requires the same actions but
corrects the effectivity for certain fan blades requiring corrective actions and changes the effective date of the current AD. This AD supersedure results from the FAA discovering that the existing FAA AD has an incorrect effectivity for certain fan blades requiring corrective actions, and from a report of an under-cowl fire and a failed fan blade.
|
| Publication(s) and related information |
See Table 1 - 'Material Incorporated by Reference' of this FAA AD. |
| Remarks |
For service information identified in this AD, contact General Electric Company, GEAviation,
Room 285, 1 Neumann Way, Cincinnati, OH 45215, telephone (513) 552-3272; fax (513)
552-3329; e-mail: geae.aoc@ge.com.
|
