AD 2001-19-05

[Federal Register Volume 66, Number 199 (Monday, October 15, 2001)]
[Rules and Regulations]
[Page 52312]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 01-25053]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2001-NE-22; Amendment 39-12445; AD 2001-19-05]
RIN 2120-AA64


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

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:

PART 39--[CORRECTED]


Sec. 39.13  [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.''

    Issued in Burlington, MA, on October 1, 2001.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 01-25053 Filed 10-12-01; 8:45 am]
BILLING CODE 4910-13-P