AD 2003-11-23
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | International | Various | 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 |
Unsafe Condition
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...
Affected Aircraft
International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Document Text
Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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
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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
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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