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Published 2002-12-13 · Federal Register document 02-31395

Airworthiness Directives; Rolls-Royce plc. RB211-535 Turbofan Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2002-23-08, applicable to Rolls-Royce plc. (RR) models RB211- 535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines. AD 2002-23-08 was published in the Federal Register on November 29, 2002 (67 FR 71094). In the DATES section of the preamble, two dates are incorrect. This document corrects those dates. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:07.262592+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2002-c8c2ee537a56d16c
Source row
results[431]
Raw source SHA-256
c8c2ee537a56d16c3d3246bbaa55e183792a136494260623f45827707b4e2a64

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2002-23-08
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

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Find all recorded historical references to AD 2002-23-08 · 0 printed reference observations in this pinned collection.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: 16e3077e7afb42e0f88115fab310c800ceea1205c5cc5dbc3a0e5c471072c199. Source manifest: 61c455ab5cbda08574252e08f3ccaed1a3167a5a050edec05eb7d5b89c733233.

Official source · 2002-12-13

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 67, Number 240 (Friday, December 13, 2002)]
[Rules and Regulations]
[Page 76673]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-31395]



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Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
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Federal Register / Vol. 67, No. 240 / Friday, December 13, 2002 / 
Rules and Regulations

[[Page 76673]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2002-NE-16-AD; Amendment 39-12952; AD 2002-23-08]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce plc. RB211-535 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) 2002-23-08, applicable to Rolls-Royce plc. (RR) models RB211-
535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines. AD 
2002-23-08 was published in the Federal Register on November 29, 2002 
(67 FR 71094). In the DATES section of the preamble, two dates are 
incorrect. This document corrects those dates. In all other respects, 
the original document remains the same.

EFFECTIVE DATE: December 16, 2002.

FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7178; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule; request for comments 
airworthiness directive FR Doc. 02-29001, applicable to models RB211-
535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines, was 
published in the Federal Register on November 29, 2002 (67 FR 71094). 
The following correction is needed:
    On page 71094, in the second column, second paragraph, in the DATES 
section, first line, remove the phrase ``Effective December 30, 2002.'' 
and add in its place ``Effective December 16, 2002.'' Also, in the 
fifth line, remove the phrase ``as of December 30, 2002.'' and add in 
its place ``as of December 16, 2002.''

    Issued in Burlington, MA, on December 5, 2002.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-31395 Filed 12-12-02; 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 2026-10-09T04:16:34.432097+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
c27048f2710cffcbb69f92a912b9b0fdb2c2bab02f82c1a5b944be3801f66912
Text SHA-256
16e3077e7afb42e0f88115fab310c800ceea1205c5cc5dbc3a0e5c471072c199

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