Rules and Regulations. Final rule; correction

Agency: Federal Aviation Administration, DOT
Action: Final rule; correction
Citation: FR Doc. 02-6531 · RIN 2120-AA64 · Docket No. 2000-NE-02; Amendment 39-12640; AD 2002-02-12 · 14 CFR 39

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.

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: 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 [Corrected] 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. [FR Doc. 02-6531 Filed 3-19-02; 8:45 am]