# [Corrected]
**AGENCY:**
Federal Aviation Administration, DOT.
**ACTION:**
Final rule; correction.
**SUMMARY:**
This document makes a correction to Airworthiness Directive (AD) 2002-02-12, applicable to Rolls-Royce plc (RR) RB211-524G and -524H series turbofan engines that was published in the *Federal Register* on February 14, 2002 (67 FR 6859). The Amendment number is incorrect and this document corrects that number. In all other respects, the original document remains the same.
**EFFECTIVE DATE:**
March 21, 2002.
**FOR FURTHER INFORMATION CONTACT:**
Keith Mead, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7744 fax (781) 238-7199.
**SUPPLEMENTARY INFORMATION:**
A final rule airworthiness directive applicable to Rolls-Royce plc (RR) RB211-524G and -524H series turbofan engines, was published in the *Federal Register* on February 14, 2002 (67 FR 6859). The following correction is needed:
**14 CFR Part 39**
On page 6859, in the first column, the Amendment No. in the fifth line of the Heading is corrected to read “Amendment 39-12640.”
**PART 39—[CORRECTED]**
§ 39.13
On page 6860, in the third column, in amendatory instruction 2, in the fifth line, and in the heading of the AD, beginning in the first line, correct “Amendment 39-12460” to read “Amendment 39-12640”.
Issued in Burlington, MA, on March 12, 2002.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.