Document ID: FAA-2007-27687-0037
Agency: faa
Document Type: Rule
Title: Airworthiness Directives: General Electric Company CF34 -1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines; Correction
Posted Date: 2010-05-20T04:00Z

[Federal Register: May 20, 2010 (Volume 75, Number 97)]
[Rules and Regulations]               
[Page 28188]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr20my10-2]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27687; Directorate Identifier 2000-NE-42-AD; 
Amendment 39-16144; AD 2009-26-09]
RIN 2120-AA64

 
Airworthiness Directives; General Electric Company CF34-1A, -3A, 
-3A1, -3A2, -3B, and -3B1 Turbofan Engines; Correction

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting airworthiness directive (AD) 2009-26-09, 
which published in the Federal Register. That AD applies to General 
Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan 
engines. The GE alert service bulletin (ASB) numbers CF34-AL S/B 72 
A0212, CF34-AL S/B 72 A0234, and CF34-AL S/B 72 A0235 in the regulatory 
section are incorrect. This document corrects those ASB numbers. In all 
other respects, the original document remains the same.

DATES: This correction is May 20, 2010. The compliance date of AD 2009-
26-09 remains February 11, 2010.

FOR FURTHER INFORMATION CONTACT: John Frost, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; e-mail: 
john.frost@faa.gov; phone: (781) 238-7756; fax: (781) 238-7199.

SUPPLEMENTARY INFORMATION: On January 7, 2010 (75 FR 910), we published 
a final rule AD, FR Doc, E9-30471, in the Federal Register. That AD 
applies to (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan 
engines. We need to make the following corrections:

Sec.  39.13  [Corrected]

    1. On page 914, in the second column, in paragraph (k)(1)(i), in 
the fifth and eighth lines, ``CF34-AL'' is corrected to read ``CF34-
BJ''.
    2. On page 914, in the second column, in paragraph (k)(2)(iii), in 
the fifth line, ``CF34-AL'' is corrected to read ``CF34-BJ''.
    3. On page 914, in the second column, in paragraph (l), in the 
seventh line, ``CF34-AL'' is corrected to read ``CF34-BJ''.
    4. On page 914, in the second column, in paragraph (l)(1), in the 
second line, ``CF34-AL'' is corrected to read ``CF34-BJ''.
    5. On page 914, in the third column, in paragraph (l)(1)(i), in the 
seventh and tenth lines, ``CF34-AL'' is corrected to read ``CF34-BJ''.
    6. On page 914, in the third column, in paragraph (m)(1), in the 
second, ninth, and twelfth lines, ``CF34-AL'' is corrected to read 
``CF34-BJ''.

    Issued in Burlington, Massachusetts, on May 10, 2010.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2010-11642 Filed 5-19-10; 8:45 am]
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