[Corrected]

---
identifier: "/us/fr/01-25053"
source: "fr"
legal_status: "authoritative_unofficial"
title: "[Corrected]"
title_number: 0
title_name: "Federal Register"
section_number: "01-25053"
section_name: "[Corrected]"
positive_law: false
currency: "2001-10-13"
last_updated: "2001-10-13"
format_version: "1.1.0"
generator: "[email protected]"
agency: "DEPARTMENT OF TRANSPORTATION"
document_number: "01-25053"
document_type: "rule"
publication_date: "2001-10-13"
agencies:
  - "DEPARTMENT OF TRANSPORTATION"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
---


#  [Corrected]

**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.

**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.

**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:

**14 CFR Part 39**

**PART 39—[CORRECTED]**

§ 39.13

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.”

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

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.