# [Corrected]
**AGENCY:**
Federal Aviation Administration, DOT.
**ACTION:**
Final rule; correction.
**SUMMARY:**
This document makes a correction to Airworthiness Directive (AD) 2001-08-14 applicable to Turbomeca S.A. Arrius models 2B, 2B1, and 2F turboshaft engines, that was published in the *Federal Register* on April 26, 2001 (66 FR 20910). The amendment number of 39-12191 used in this AD is incorrect. This document corrects that amendment number. In all other respects, the original document remains the same.
**EFFECTIVE DATE:**
May 31, 2001.
**FOR FURTHER INFORMATION CONTACT:**
James Rosa, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone (781) 238-7152, fax (781) 238-7199.
**SUPPLEMENTARY INFORMATION:**
A final rule airworthiness directive (FR Doc. 01-10021) applicable to Turbomeca S.A. Arrius models 2B, 2B1, and 2F turboshaft engines was published in the *Federal Register* on April 26, 2001 (66 FR 20912). The following correction is needed:
**14 CFR Part 39**
1. On page 20910, in the first column, in the Heading of the document, the docket line is corrected to read “[Docket No. 2000-NE-12-AD; Amendment 39-12218; AD 2001-08-14]”.
**PART 39—[CORRECTED]**
§ 39.13
**14 CFR Part 39**
2. On page 20911, in the first column, under amendatory instruction 2, the heading of AD 2001-08-14 is corrected to read as follows:
*2001-08-14 Turbomeca S.A. Arrius Models 2B, 2B1, and 2F Turboshaft Engines:* Amendment 39-12218. Docket No. 2000-NE-12-AD.
Issued in Burlington, MA, on April 30, 2001.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.