[Federal Register Volume 75, Number 97 (Thursday, May 20, 2010)]
[Rules and Regulations]
[Page 28188]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-11642]
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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:
[email protected]; 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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