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Published 2004-09-30 · Federal Register document 04-21912

Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, and RB211-535 Series Turbofan Engines

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2004-19-04. That AD applies to Rolls-Royce plc (RR) RB211-22B, RB211-524, and RB211-535 series turbofan engines. That AD was published in the Federal Register on September 22, 2004 (69 FR 56683). In the amendatory language, under Sec. 39.13 [Amended], the amendment number for the AD was inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:13.905821+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2004-cb1e1f18d61cac01
Source row
results[422]
Raw source SHA-256
cb1e1f18d61cac01616802134d899b0c8ce1a9f79716b5ee037f78e4cb53a00a

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2004-19-04
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2004-19-04 · 0 printed reference observations in this pinned collection.

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 2a10a5ad4b5749fe5a90cfd4abb6ada64d5d3337443dedc74bdc95ac088e299f. Source manifest: eada70c44ffcfc4a64f4ad110c8ea98ba4099887c20e1d1c1fb3f0771a641403.

Official source · 2004-09-30

Publication text

This is the complete recorded text of this dated publication.

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Read the complete official publication text
[Federal Register Volume 69, Number 189 (Thursday, September 30, 2004)]
[Rules and Regulations]
[Pages 58257-58258]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-21912]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-57-AD; Amendment 39-13798; AD 2004-19-04]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, 
and RB211-535 Series Turbofan Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

[[Page 58258]]

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2004-19-04. That AD applies to Rolls-Royce plc (RR) RB211-22B, 
RB211-524, and RB211-535 series turbofan engines. That AD was published 
in the Federal Register on September 22, 2004 (69 FR 56683). In the 
amendatory language, under Sec.  39.13 [Amended], the amendment number 
for the AD was inadvertently omitted. This document corrects that 
omission. In all other respects, the original document remains the 
same.

EFFECTIVE DATE: Effective September 30, 2004.

FOR FURTHER INFORMATION CONTACT: Christopher Spinney, Aerospace 
Engineer, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; 
telephone (781) 238-7175, fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-21173 that 
applies to RR RB211-22B, RB211-524, and RB211-535 series turbofan 
engines, was published in the Federal Register on September 22, 2004 
(69 FR 56683). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 56684, in the second column, under Sec.  39.13 [Amended], in 
the fifth line, ``2004-19-04 Rolls-Royce plc: Docket No.'' is corrected 
to read ``2004-19-04 Rolls-Royce plc: Amendment 39-13798. Docket No.''.

    Issued in Burlington, MA, on September 23, 2004.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 04-21912 Filed 9-29-04; 8:45 am]
BILLING CODE 4910-13-P
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Source SHA-256
7ac22a6529e6091bdec4a070de5466a3f245ea028e391251971f0f4ee949e0d3
Text SHA-256
2a10a5ad4b5749fe5a90cfd4abb6ada64d5d3337443dedc74bdc95ac088e299f

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