Published 2004-03-25 · Federal Register document 04-6577

Airworthiness Directives; Rolls-Royce Deutschland (RRD) (Formerly Rolls-Royce, plc) TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 Series Turbofan Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2004-05-22. That AD applies to certain RRD TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 series turbofan engines with ice-impact panels installed in the low pressure (LP) compressor case. We published AD 2004-05-22 in the Federal Register on March 10, 2004, (69 FR 11305). The AD number in the Amendatory Language is incorrect. This document corrects that AD 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: 2004-05-22
Effective date printed in this edition: Unknown

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Official source · 2004-03-25

Publication text

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Read the complete official publication text

[Federal Register Volume 69, Number 58 (Thursday, March 25, 2004)]
[Rules and Regulations]
[Page 15238]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-6577]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2004-NE-11-AD; Amendment 39-13517; AD 2004-05-22]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Deutschland (RRD) (Formerly 
Rolls-Royce, plc) TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-54 
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) 2004-05-22. That AD applies to certain RRD TAY 611-8, TAY 620-15, 
TAY 650-15, and TAY 651-54 series turbofan engines with ice-impact 
panels installed in the low pressure (LP) compressor case. We published 
AD 2004-05-22 in the Federal Register on March 10, 2004, (69 FR 11305). 
The AD number in the Amendatory Language is incorrect. This document 
corrects that AD number. In all other respects, the original document 
remains the same.

EFFECTIVE DATE: Effective March 25, 2004.

FOR FURTHER INFORMATION CONTACT: Jason Yang, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7747; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc, 04-5263 that 
applies to certain RRD TAY 611-8, TAY 620-15, TAY 650-15, and TAY 651-
54 series turbofan engines with ice-impact panels installed in the LP 
compressor case, was published in the Federal Register on March 10, 
2004, (69 FR 11305). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 11307, in the second column, in the Amendatory Language, in the 
third paragraph, in the first line, ``200X-05-22'' is corrected to read 
``2004-05-22''.

    Issued in Burlington, MA, on March 18, 2004.
Mark C. Fulmer,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 04-6577 Filed 3-24-04; 8:45 am]
BILLING CODE 4910-13-P

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