Federal Aviation Administration, DOT.
Final rule; correction.
This document makes a correction to Airworthiness Directive (AD) 2000-13-05 applicable to Rolls-Royce plc. (RR) RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 turbofan engines that was published in the Federal Register on July 3, 2000 (65 FR 40983). The statement regarding the reports of fan blade failures in the Summary section and the Internet address for AD comments in the Addresses section are incorrect. This document corrects that statement and that address. In all other respects, the original document remains the same.
August 23, 2000.Start Further Info
FOR FURTHER INFORMATION CONTACT:
James Lawrence, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone 781-238-7176; fax 781-238-7199.End Further Info End Preamble Start Supplemental Information
A final rule airworthiness directive applicable to Rolls-Royce plc. (RR) RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 turbofan engines, was published in the Federal Register on July 3, 2000 (65 FR 40983).
The following corrections are needed:Start Amendment Part
1. On page 40983, in the second column, in the SUMMARY section, in the eleventh and twelfth lines, “fan blade failures due to dovetail root cracks.” is corrected to read “fan blade root cracks in a factory engine.”.End Amendment Part Start Amendment PartEnd Amendment Part Start Signature
Issued in Burlington, MA, on August 16, 2000.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.
[FR Doc. 00-21314 Filed 8-22-00; 8:45 am]
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