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Airworthiness Directives; Rolls-Royce plc. RB211 535 Turbofan Engines, Correction

Document Details

Information about this document as published in the Federal Register.

Published Document

This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.

Start Preamble

AGENCY:

Federal Aviation Administration, DOT.

ACTION:

Final rule; request for comments, correction.

SUMMARY:

This document makes a correction to Airworthiness Directive (AD) 2001-19-05 applicable to Rolls-Royce plc (RR) models RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines, with radial drive steady bearing, part number (P/N) LK76084, that was published in the Federal Register on September 26, 2001 (66 FR 49099). A part number referenced in items (3) and (4) of Table 1 in the regulatory information is incorrect. This document corrects that part number. In all other respects, the original document remains the same.

EFFECTIVE DATE:

October 11, 2001.

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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

SUPPLEMENTARY INFORMATION:

A final rule; request for comments airworthiness directive applicable to (RR) models RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines, with radial drive steady bearing, part number (P/N) LK76084, was published in the Federal Register on September 26, 2001 (66 FR 49099). The following correction is needed:

Start Part

PART 39—[CORRECTED]

[Corrected]

On page 49100, in the third column in the Regulatory Information, Table 1, “(3) One engine has a radial drive steady bearing P/N FK76084 with fewer than 600 HSN, and the other engine has a bearing P/N FK76084 with more than 1,500 HSN,” is corrected to read “(3) One engine has a radial drive steady bearing P/N LK76084 with fewer than 600 HSN, and the other engine has a bearing P/N LK76084 with more than 1,500 HSN.” Also, Table 1 “(4) Both engines have a radial drive steady bearing P/N FK76084 with 600 or more HSN,” is corrected to read “(4) Both engines have a radial drive steady bearing P/N LK76084 with 600 or more HSN.”

End Part Start Signature

Issued in Burlington, MA, on October 1, 2001.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.

End Signature End Supplemental Information

[FR Doc. 01-25053 Filed 10-12-01; 8:45 am]

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