Published 2002-03-20 · Federal Register document 02-6531

Airworthiness Directives; Rolls-Royce plc RB211-524G and -524H Series Turbofan Engines; Correction

Publication 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.

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Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2002-02-12
Effective date printed in this edition: Unknown

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Official source · 2002-03-20

Publication text

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Read the complete official publication text

[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]
BILLING CODE 4910-13-U

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