Back to publication catalog

Published 2003-09-18 · Federal Register document 03-23816

Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2003-16-03 applicable to Turbomeca Arriel 1 Series turboshaft engines that was published in the Federal Register on August 8, 2003 (68 FR 47208). Turbomeca Arriel turboshaft engine 1 C1 was omitted from the Applicability. This document corrects that omission. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:10.496508+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2003-b6c0b146601d56c4
Source row
results[339]
Raw source SHA-256
b6c0b146601d56c4829685d26300140986ff1ab0185264ed2f7f002dc27cf9e7

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2003-16-03
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Find all recorded historical references to AD 2003-16-03 · 0 printed reference observations in this pinned collection.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: 4867f23cb1265954fb724b2c1c43b1eac1804cbaf101412742a8fc3baa7d5f68. Source manifest: f1679524d881b935907c0ededf3a58e69bb355e70536f6838ff2c4bbadccbfdc.

Official source · 2003-09-18

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 68, Number 181 (Thursday, September 18, 2003)]
[Rules and Regulations]
[Page 54653]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-23816]



[[Page 54653]]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94-ANE-08-AD; Amendment 39-13256; AD 2003-16-03]
RIN 2120-AA64


Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft 
Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2003-16-03 applicable to Turbomeca Arriel 1 Series turboshaft 
engines that was published in the Federal Register on August 8, 2003 
(68 FR 47208). Turbomeca Arriel turboshaft engine 1 C1 was omitted from 
the Applicability. This document corrects that omission. In all other 
respects, the original document remains the same.

EFFECTIVE DATE: Effective September 18, 2003.

FOR FURTHER INFORMATION CONTACT: Antonio Cancelliere, Aerospace 
Engineer, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; 
telephone (781) 238-7751; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 03-19836, 
applicable to Turbomeca Arriel 1 Series turboshaft engines, was 
published in the Federal Register on August 8, 2003 (68 FR 47208). The 
following correction is needed:

PART 39--AIRWORTHINESS DIRECTIVES


Sec.  39.13  [Corrected]

0
On page 47209, in the third column, in the Applicability Section, the 
first sentence ``This airworthiness directive (AD) applies to Turbomeca 
turboshaft engine models Arriel 1 A, 1 A1, 1 A2, 1 B, 1 C, 1 C2, 1 D, 1 
D1, 1 E2, 1 K, 1 K1, 1 S, and 1 S1 that have not incorporated 
modification TU 202'' is corrected to read, ``This airworthiness 
directive (AD) applies to Turbomeca turboshaft engine models Arriel 1 
A, 1 A1, 1 A2, 1 B, 1 C, 1 C1, 1 C2, 1 D, 1 D1, 1 E2, 1 K, 1 K1, 1 S, 
and 1 S1 that have not incorporated modification TU 202''.

    Issued in Burlington, MA, on September 11, 2003.
Francis A. Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 03-23816 Filed 9-17-03; 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 2026-10-09T04:10:42.704493+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
c9a01ce94c2d36a88a76a07e01170ca15b524a9a4a45cfa0414aca3feb5afb7f
Text SHA-256
4867f23cb1265954fb724b2c1c43b1eac1804cbaf101412742a8fc3baa7d5f68

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.