Published 2013-11-14 · Federal Register document 2013-27190
Airworthiness Directives; Rolls-Royce plc Turbofan Engines
Publication summary
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Rolls-Royce plc (RR) RB211-535E4-B-37 series turbofan engines. The AD number is incorrect in the Regulatory text. This document corrects that error. In all other respects, the original document remains the same.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
- Source row
- results[372]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2013-19-17
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2013-19-17 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 6ae83f423b10d6024da0ab05d056bc6b41f214898d888dfaa6dad13a640d52a2. Source manifest: 8ec7cac09d1aed225d755ce4e7d5d19ac39cd7783f60f8df7d2feb96f62fa8d6.
Official source · 2013-11-14
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 78, Number 220 (Thursday, November 14, 2013)]
[Rules and Regulations]
[Page 68360]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-27190]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0029; Directorate Identifier 2013-NE-01-AD;
Amendment 39-17599; AD 2013-19-17]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to all Rolls-Royce
plc (RR) RB211-535E4-B-37 series turbofan engines. The AD number is
incorrect in the Regulatory text. This document corrects that error. In
all other respects, the original document remains the same.
DATES: This final rule is effective November 7, 2013.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Robert Green, Aerospace Engineer,
Engine Certification Office, FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; phone: 781-238-7754;
fax: 781-238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2013-19-17,
Amendment 39-17599 (78 FR 61171, October 3, 2013), currently requires
removal of affected parts using a drawdown plan for all RR RB211-535E4-
B-37 series turbofan engines.
As published, the AD number 2013-19-17 under Sec. 39.13 [Amended],
is incorrect.
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains November 7, 2013.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
In the Federal Register of October 3, 2013, on page 61173, in the
first column, lines 4 and 5, under Sec. 39.13 [Amended] of AD 2013-19-
17, are corrected to read as follows:
* * * * *
2013-19-17 Rolls-Royce plc: Amendment 39-17599; Docket No. FAA-2013-
0029;
* * * * *
Issued in Burlington, Massachusetts, on October 25, 2013.
Colleen M. D'Alessandro,
Assistant Directorate Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2013-27190 Filed 11-13-13; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:51:29.835605+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 02b5544ebb5850ae066f802c90183d1a947f7b06221becbdc2457c573c7ced79
- Text SHA-256
- 6ae83f423b10d6024da0ab05d056bc6b41f214898d888dfaa6dad13a640d52a2
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.