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Published 2012-02-24 · Federal Register document 2012-4285

Airworthiness Directives; CFM International S.A. Model CFM56 Turbofan Engines

Publication summary

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to CFM International S.A. CFM56-2, CFM56-3, CFM56-5A, CFM56-5B, CFM56-5C, and CFM56-7B series turbofan engines with certain part number (P/N) and serial number (SN) high-pressure compressor (HPC) 4-9 spools installed. In Table 1 of the AD, the HPC 4-9 spool SN GWN05AMO in the 2nd column of the Table is incorrect. This document corrects that error. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[49]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2009-11-02
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Find all recorded historical references to AD 2009-11-02 · 0 printed reference observations in this pinned collection.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.

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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: d262ce3f2ffb84565038b95109e8a47e54210c2ff88e7464713005a713ff853d. Source manifest: f73be127d8c64ec21271c14a7362beaf978098f090d679c1b9136f1564d5264c.

Official source · 2012-02-24

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 77, Number 37 (Friday, February 24, 2012)]
[Rules and Regulations]
[Pages 10952-10953]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-4285]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-1245; Directorate Identifier 2008-NE-27-AD; 
Amendment 39-15912; AD 2009-11-02]
RIN 2120-AA64


Airworthiness Directives; CFM International S.A. Model CFM56 
Turbofan Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to CFM International 
S.A. CFM56-2, CFM56-3, CFM56-5A, CFM56-5B, CFM56-5C, and CFM56-7B 
series turbofan engines with certain part number (P/N) and serial 
number (SN) high-pressure compressor (HPC) 4-9 spools installed. In 
Table 1 of the AD, the HPC 4-9 spool SN GWN05AMO in the 2nd column of 
the Table is incorrect. This document corrects that error. In all other 
respects, the original document remains the same.

DATES: This final rule is effective February 24, 2012. The effective 
date for AD 2009-11-02 (74 FR 23305, May 19, 2009) remains June 23, 
2009.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The address for the 
Docket Office (phone: 800-647-5527) is Document Management Facility, 
U.S. Department of Transportation, Docket Operations, M-30, West 
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Martin Adler, Aerospace Engineer, 
Engine Certification Office, FAA, Engine & Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; phone: 781-238-7157; 
fax: 781-238-7199; email: [email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2009-11-02, 
Amendment 39-15912 (74 FR 23305, May 19, 2009), currently requires 
removing certain HPC 4-9 spools listed by P/N and SN in the AD.
    As published, in Table 1 of the AD, the HPC 4-9 spool SN GWN05AMO 
in the 2nd column of the Table is incorrect.
    No other part of the preamble or regulatory information has been 
changed; therefore, only the changed portion of the final rule is being 
published in the Federal Register.
    The effective date of this AD remains June 23, 2009.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

0
In the Federal Register of May 19, 2009, on page 23306, in the 3rd 
column, in Table 1, under the HPC 4-9 Spool SN heading, in the 
twentieth line of AD

[[Page 10953]]

2009-11-02; Amendment 39-15912 is corrected as follows:
* * * * *
    GWN05AM0
* * * * *

    Issued in Burlington, Massachusetts, on February 13, 2012.
Peter A. White,
Manager, Engine & Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-4285 Filed 2-23-12; 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 2026-10-09T03:04:30.461260+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
3c088aedc685f1fc230eac599ff718e427b768e16c2d849e977241923de55f07
Text SHA-256
d262ce3f2ffb84565038b95109e8a47e54210c2ff88e7464713005a713ff853d

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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.

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