# [Corrected]
**AGENCY:**
Federal Aviation Administration, DOT.
**ACTION:**
Final rule; correction.
**SUMMARY:**
This document makes a correction to Airworthiness Directive (AD) 2002-17-02 applicable to Pratt & Whitney JT8D series turbofan engines that was published in the *Federal Register* on August 28, 2002 (67 FR 55108). The first sentence in the amendatory language that states “2. Section 39.13 is amended by removing Amendment 39-11940 (65 FR 65731, November 2, 2000) and by adding a new airworthiness directive to read as follows:” is incorrect. This document corrects that sentence. In all other respects, the original document remains the same.
**EFFECTIVE DATE:**
August 28, 2002.
**FOR FURTHER INFORMATION CONTACT:**
Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park; Burlington, MA 01803-5299; telephone (781) 238-7175; fax (781) 238-7199.
**SUPPLEMENTARY INFORMATION:**
A final rule airworthiness directive FR Doc. 02-21832 applicable to Pratt & Whitney JT8D series turbofan engines, was published in the *Federal Register* on August 28, 2002 (67 FR 55108). The following correction is needed:
**14 CFR Part 39**
§ 39.13
On page 55110, in the second column, the first sentence of the amendatory language is corrected to read:
“2. Section 39.13 is amended by removing Amendment 39-11940 (65 FR 65731, November 2, 2000) and by adding a new airworthiness directive, Amendment 39-12867, to read as follows:''
Issued in Burlington, MA, on August 30, 2002.
Francis Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.