[Federal Register Volume 67, Number 54 (Wednesday, March 20, 2002)]
[Rules and Regulations]
[Pages 12859-12860]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-6531]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NE-02; Amendment 39-12640; AD 2002-02-12]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc RB211-524G and -524H
Series Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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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.
FOR FURTHER INFORMATION CONTACT: Keith Mead, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7744 fax (781) 238-7199.
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.''
[[Page 12860]]
PART 39--[CORRECTED]
Sec. 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]
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