# [Corrected]
**AGENCY:**
Federal Aviation Administration (FAA), Department of Transportation (DOT).
**ACTION:**
Final rule; correction.
**SUMMARY:**
The FAA is correcting airworthiness directive (AD) 2006-24-08. That AD applies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines. We published that AD in the *Federal Register* on December 4, 2006 (71 FR 70284). The fuel manifold part number (P/N) 3025267-01 listed in paragraph (c) is incorrect. This document corrects that P/N. In all other respects, the original document remains the same.
**EFFECTIVE DATE:**
Effective May 22, 2007.
**FOR FURTHER INFORMATION CONTACT:**
Ian Dargin, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA, 01803; telephone (781) 238-7178; fax (781) 238-7199.
**SUPPLEMENTARY INFORMATION:**
On December 4, 2006 (71 FR 70284), we published a final rule AD, FR Doc, E6-20204, in the *Federal Register* . That AD applies to P&WC PW535A turbofan engines. We need to make the following correction:
§ 39.13
On page 70286, in the second column, in paragraph (c), in the fourth line, “3025267-01” is corrected to read “3052627-01”.
Issued in Burlington, Massachusetts, on May 14, 2007.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.