AD 2004-05-22

final rule

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

AD Number
2004-05-22
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2004-NE-11-AD
FR Citation
69 FR 15238
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Rolls-Royce 611-8 620-15 650-15 651-54 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

Unsafe Condition

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.

Affected Aircraft

RRD (formerly Rolls-Royce, plc) 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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

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.

Document Text

Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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