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Published 2003-07-02 · Federal Register document 03-16690

Airworthiness Directives; International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 Turbofan Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2003-11-23 applicable to IAE V2522-A5, V2524-A5, V2527-A5, V2527E- A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines that was published in the Federal Register on June 5, 2003 (68 FR 33621). The lists of engine models in the Airworthiness Directives title, the Summary, the Supplementary Information, and the Applicability section are incorrect. This document corrects those listings. Also, paragraph (c) of the regulatory text was incorrectly printed as run-in with the heading Applicability. In all other respects, the original document remains the same.

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

Source revision
federal_register_ad_metadata_2003-b6c0b146601d56c4
Source row
results[237]
Raw source SHA-256
b6c0b146601d56c4829685d26300140986ff1ab0185264ed2f7f002dc27cf9e7

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2003-11-23
Effective date printed in this edition
Unknown

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: f7aff84a4aa576f3822337ff94e7a74c4da9aa218db1689528bf1bf6d031e6c8. Source manifest: 731982022b0a045636563e571347d6f9e60844f91cba9b0a2ad02cb14608ced7.

Official source · 2003-07-02

Publication text

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Read the complete official publication text
[Federal Register Volume 68, Number 127 (Wednesday, July 2, 2003)]
[Rules and Regulations]
[Page 39449]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-16690]


=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-21-AD; Amendment 39-13183; AD 2003-11-23]
RIN 2120-AA64


Airworthiness Directives; International Aero Engines AG (IAE) 
V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and 
V2533-A5 Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2003-11-23 applicable to IAE V2522-A5, V2524-A5, V2527-A5, V2527E-
A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines that was 
published in the Federal Register on June 5, 2003 (68 FR 33621). The 
lists of engine models in the Airworthiness Directives title, the 
Summary, the Supplementary Information, and the Applicability section 
are incorrect. This document corrects those listings. Also, paragraph 
(c) of the regulatory text was incorrectly printed as run-in with the 
heading Applicability. In all other respects, the original document 
remains the same.

EFFECTIVE DATE: Effective June 20, 2003.

FOR FURTHER INFORMATION CONTACT: Glorianne Niebuhr, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; telephone (781) 238-
7132; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc, 03-14133 applicable 
to IAE V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, 
and V2533-A5 turbofan engines, was published in the Federal Register on 
June 5, 2003 (68 FR 33621). The following correction is needed:


Sec.  39.13  [Corrected]

    On page 33621, in the third column, in the Heading Section, in the 
Airworthiness Directives title, ``International Aero Engines AG (IAE) 
V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, and V2530-A5 
Turbofan Engines ``is corrected to read'' International Aero Engines AG 
(IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and 
V2533-A5 Turbofan Engines''. In the same column, in the Summary 
section, in the fourth and fifth lines, ``V2527E-A5, V2527M-A5, and 
V2530-A5 turbofan engines'' is corrected to read ``V2527E-A5, V2527M-
A5, V2530-A5, and V2533-A5 turbofan engines''.
    On page 33622, in the first column, in the Supplementary 
Information section, in third and fourth lines, change ``V2527-A5, 
V2527E-A5, V2527M-A5, and V2530-A5'' to ``V2527-A5, V2527E-A5, V2527M-
A5, V2530-A5, and V2533-A5''. In the same column, third paragraph, 
fourth and fifth lines, change ``V2527-A5, V2527E-A5, V2527M-A5, and 
V2530-A5'' to ``V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-
A5''.

    Issued in Burlington, MA, on June 26, 2003.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 03-16690 Filed 7-1-03; 8:45 am]
BILLING CODE 4910-13-P


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eabc416be1008c51bbdef1e9ae80dcf8672ea75178c55ed9128b4b0e8aedc455
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f7aff84a4aa576f3822337ff94e7a74c4da9aa218db1689528bf1bf6d031e6c8

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