Back to publication catalog

Published 1998-09-28 · Federal Register document 98-25782

Airworthiness Directives; Rolls-Royce Limited, Aero Division Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines

Publication summary

The FAA is withdrawing the final rule; request for comments, which was published on September 16, 1998 (63 FR 49418). The reason for the withdrawal is because it is a duplicate of a final rule; request for comments, published on September 15, 1998 (63 FR 49278). The September 15, 1998, final rule, remains effective September 30, 1998. The September 15, 1998 amendment adopted a new airworthiness directive (AD) that is applicable to Rolls-Royce Limited, Aero Division--Bristol/ S.N.E.C.M.A. Olympus 593 series turbojet engines.

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[554]
Raw source SHA-256
f5c1cf5c93c99179023030016db80652e7593139090148c64a6fd533918aa991

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
98-19-11
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 98-19-11 · 0 printed reference observations in this pinned collection.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: 4cac1c79a0ef58a91a4e43d953d6973ed6b9297b73a9ee853446c9e5bb666c79. Source manifest: 1c8d0474e1aeb069e5af38ef62b3809843322a9b6f15bff0f8077b5ce0dcfa5f.

Official source · 1998-09-28

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 187 (Monday, September 28, 1998)]
[Rules and Regulations]
[Page 51525]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-25782]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-ANE-07-AD; Amendment 39-10753; AD 98-19-11]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Limited, Aero Division--
Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments, withdrawal.

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

SUMMARY: The FAA is withdrawing the final rule; request for comments, 
which was published on September 16, 1998 (63 FR 49418). The reason for 
the withdrawal is because it is a duplicate of a final rule; request 
for comments, published on September 15, 1998 (63 FR 49278). The 
September 15, 1998, final rule, remains effective September 30, 1998. 
The September 15, 1998 amendment adopted a new airworthiness directive 
(AD) that is applicable to Rolls-Royce Limited, Aero Division--Bristol/
S.N.E.C.M.A. Olympus 593 series turbojet engines.

DATES: The final rule; request for comments, published Wednesday, 
September 16, 1998, at 63 FR 49418, is withdrawn on September 17, 1998.

FOR FURTHER INFORMATION CONTACT: Mary Culver, Technical Publications 
Specialist, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; 
telephone (781) 238-7125, fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: The FAA is withdrawing Docket No. 98-ANE-07-
AD; Amendment 39-10753; AD 98-19-11 which was published on September 
16, 1998 (63 FR 49418). The reason for the withdrawal is because it is 
a duplicate of a final rule; request for comments, published on 
September 15, 1998 (63 FR 49278). The September 15, 1998, final rule 
that is applicable to Rolls-Royce Limited, Aero Division--Bristol/
S.N.E.C.M.A. Olympus 593 series turbojet engines, remains effective 
September 30, 1998.

    Issued in Burlington, Massachusetts, on September 17, 1998.
Kirk Gustafson,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 98-25782 Filed 9-25-98; 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 2026-10-09T04:57:56.468698+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
d554153962007eb033255b3ebdbaffa11c398cde195767ece5e4d08f971af515
Text SHA-256
4cac1c79a0ef58a91a4e43d953d6973ed6b9297b73a9ee853446c9e5bb666c79

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.