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

---
identifier: "/us/fr/2010-11642"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines; Correction"
title_number: 0
title_name: "Federal Register"
section_number: "2010-11642"
section_name: "Airworthiness Directives; General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines; Correction"
positive_law: false
currency: "2010-05-20"
last_updated: "2010-05-20"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "2010-11642"
document_type: "rule"
publication_date: "2010-05-20"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "75 FR 28188"
fr_volume: 75
docket_ids:
  - "Docket No. FAA-2007-27687"
  - "Directorate Identifier 2000-NE-42-AD"
  - "Amendment 39-16144"
  - "AD 2009-26-09"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration (FAA), DOT.

**ACTION:**

Final rule; correction.

**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:

§ 39.13

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.