Published 1998-10-02 · Federal Register document 98-26355
Airworthiness Directives; Rolls-Royce, plc RB211 Trent 800 Series Turbofan Engines; Correction
Publication summary
This document makes a correction to Airworthiness Directive (AD) 98-ANE-33-AD; Amendment 39-10762 that is applicable to Rolls- Royce, plc RB211 Trent 800 series turbofan engines that was published in the Federal Register on September 22, 1998 (63 FR 50484-50485). The AD number ``AD 98-18-21'' is incorrect. The correct AD number is ``AD 98-19-21''. In all other respects, the original document remains the same.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:53.985165+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_1998-f5c1cf5c93c99179
- Source row
- results[563]
- Raw source SHA-256
- f5c1cf5c93c99179023030016db80652e7593139090148c64a6fd533918aa991
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 98-19-21
- 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Find all recorded historical references to AD 98-19-21 · 0 printed reference observations in this pinned collection.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: 9b95f77be399e5d4f19be8333f89174a46e834479414ab8c68367142180aa8e0. Source manifest: 88735e6c431c7fdc7ee16eb9eb2544e2ae97c2b7e4b70c6e9b1aa67b195bf68a.
Official source · 1998-10-02
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 63, Number 191 (Friday, October 2, 1998)]
[Rules and Regulations]
[Page 52961]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-26355]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-ANE-33-AD; Amendment 39-10762; AD 98-19-21]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce, plc RB211 Trent 800 Series
Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 98-ANE-33-AD; Amendment 39-10762 that is applicable to Rolls-
Royce, plc RB211 Trent 800 series turbofan engines that was published
in the Federal Register on September 22, 1998 (63 FR 50484-50485). The
AD number ``AD 98-18-21'' is incorrect. The correct AD number is ``AD
98-19-21''. In all other respects, the original document remains the
same.
DATES: Effective October 7, 1998.
SUPPLEMENTARY INFORMATION: A final rule airworthiness directive
applicable to Rolls-Royce, plc RB211 Trent 800 series turbofan engines
was published in the Federal Register on September 22, 1998 (63 FR
50484). The published AD number is incorrect and the following
corrections are needed:
On page 50484, in the first column, in the fifth line of the
heading, ``AD 98-18-21'' is corrected to read ``AD 98-19-21''.
On page 50485, in the second column, sixth line from the top of the
column, ``98-18-21'' is corrected to read ``98-19-21''.
Issued in Burlington, Massachusetts, on September 24, 1998.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 98-26355 Filed 10-1-98; 8:45 am]
BILLING CODE 4910-13-U
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:57:47.483087+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- fe511a06e71e144c23cb5f2a1ef12ca0a8ead805ed9d58fcecf246773331d282
- Text SHA-256
- 9b95f77be399e5d4f19be8333f89174a46e834479414ab8c68367142180aa8e0
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.