# [Corrected]
**AGENCY:**
Federal Aviation Administration, DOT.
**ACTION:**
Final rule; correction.
**SUMMARY:**
This document makes a correction to Airworthiness Directive (AD) 2000-21-07 applicable to Pratt & Whitney JT8D-200 series turbofan engines that was published in the *Federal Register* on October 24, 2000 (65 FR 63540). The statement identifying AD 2000-21-07 as superseding AD 99-12-04, Amendment 39-11188 (64 FR 30382, dated June 8, 1999), was inadvertently omitted from the AD. This document corrects that statement. In all other respects, the original document remains the same.
**EFFECTIVE DATE:**
April 23, 2001.
**FOR FURTHER INFORMATION CONTACT:**
Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone 781-238-7175, fax 781-238-7199.
**SUPPLEMENTARY INFORMATION:**
A final rule airworthiness directive (FR Doc. 00-26970) applicable to Pratt & Whitney JT8D-200 series turbofan engines was published in the *Federal Register* on October 24, 2000 (65 FR 63540). The following correction is needed:
**14 CFR Part 39**
§ 39.13
On page 63541, in the first column, the AD heading is corrected to read “AD 2000-21-07 Pratt & Whitney: Amendment 39-11939. Docket 98-ANE-43-AD. Supersedes AD 99-12-04, Amendment 39-11188.”
Issued in Burlington, MA, on October 26, 2000.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.