Back to publication catalog

Published 2007-10-09 · Federal Register document E7-19686

Airworthiness Directives; Turbomeca S.A. Artouste III B, Artouste III B1, and Artouste III D Turboshaft Engines; Correction

Publication summary

The FAA is correcting airworthiness directive (AD) 2007-19-11. That AD applies to Turbomeca S.A. Artouste III B, Artouste III B1, and Artouste III D turboshaft engines. We published that AD in the Federal Register on September 21, 2007 (72 FR 53937). The AD number of the superseded AD, is incorrect in two places in the preamble, and in one place in paragraph (b). This document corrects those AD numbers. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:23.906952+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2007-daaa03e810180273
Source row
results[364]
Raw source SHA-256
daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2007-19-11
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Find all recorded historical references to AD 2007-19-11 · 0 printed reference observations in this pinned collection.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: f72c2a253ccfa9451a4f3bd61407fbee8b7180a43bbdf1a22c51215cffe888cc. Source manifest: aa440a404ceb36d8be78fc75079098938a3caae2b5d6a875ec62a54d1ae66573.

Official source · 2007-10-09

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 72, Number 194 (Tuesday, October 9, 2007)]
[Rules and Regulations]
[Pages 57195-57196]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-19686]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-23954; Directorate Identifier 2005-NE-54-AD; 
Amendment 39-15202; AD 2007-19-11]
RIN 2120-AA64


Airworthiness Directives; Turbomeca S.A. Artouste III B, Artouste 
III B1, and Artouste III D Turboshaft Engines; Correction

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting airworthiness directive (AD) 2007-19-11. 
That AD applies to Turbomeca S.A. Artouste III B, Artouste III B1, and 
Artouste III D turboshaft engines. We published that AD in the Federal 
Register on September 21, 2007 (72 FR 53937). The AD number of the 
superseded AD, is incorrect in two places in the preamble, and in one 
place in paragraph (b). This document corrects those AD numbers. In all 
other respects, the original document remains the same.

DATES: Effective Date: Effective October 9, 2007.

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

SUPPLEMENTARY INFORMATION: On September 21, 2007 (72 FR 53937), we 
published a final rule AD, FR Doc. E7-18484, in the Federal Register. 
That AD applies to Turbomeca S.A. Artouste III B, Artouste III B1, and 
Artouste III D turboshaft engines. We need to make the following 
corrections:
    On page 53937, in the second column, in the Supplementary 
Information

[[Page 57196]]

paragraph, in the third line, ``2005-04-15'' is corrected to read 
``2006-04-15''.
    On page 53938, in the first column, in the second line, ``2005-04-
15'' is corrected to read ``2006-04-15''.


Sec.  39.13  [Corrected]

0
On page 53938, in the third column, in paragraph (b), in the first 
line, ``2005-04-15'' is corrected to read ``2006-04-15''.

    Issued in Burlington, Massachusetts, on October 1, 2007.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
 [FR Doc. E7-19686 Filed 10-5-07; 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 2026-10-09T03:35:42.379417+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
94739f31479b300f7465689191c116f5637f074fe6e930f8bc5c57a00a226eea
Text SHA-256
f72c2a253ccfa9451a4f3bd61407fbee8b7180a43bbdf1a22c51215cffe888cc

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.