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Published 2012-02-03 · Federal Register document 2012-2295

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain Model DC- 10-10, DC-10-10F, and MD-10-10F airplanes. The airplane manufacturer name stated in the subject line, product identification section, and paragraph (c) of that AD, is incorrect. Also, the email address provided in paragraphs (i)(1) and (j) of that AD is incorrect. This document corrects those errors. In all other respects, the original document remains the same.

Why this record is shown

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

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[25]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2011-24-04
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Find all recorded historical references to AD 2011-24-04 · 0 printed reference observations in this pinned collection.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: 355f2c30c48aad9da0f77a140a768c76c8d564c09d76f018d05e531f0e710f25. Source manifest: dad43b07f1659664a212e1b753fbd5ec865f6f76caa3ff856ef3fdcc78673264.

Official source · 2012-02-03

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 23 (Friday, February 3, 2012)]
[Rules and Regulations]
[Pages 5386-5387]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-2295]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1206; Directorate Identifier 2009-NM-216-AD; 
Amendment 39-16868; AD 2011-24-04]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Airplanes

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 certain Model DC-
10-10, DC-10-10F, and MD-10-10F airplanes. The airplane manufacturer 
name stated in the subject line, product identification section, and 
paragraph (c) of that AD, is incorrect. Also, the email address 
provided in paragraphs (i)(1) and (j) of that AD is incorrect. This 
document corrects those errors. In all other respects, the original 
document remains the same.

DATES: This final rule is effective February 3, 2012. The effective 
date for AD 2011-24-04, Amendment 39-16868 (76 FR 73491, November 29, 
2011) remains January 3, 2012.

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: Nenita Odesa, Aerospace Engineer, 
Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification 
Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; 
phone: (562) 627-5234; fax: (562) 627-5210; email: 
[email protected].

[[Page 5387]]


SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-24-04, 
amendment 39-16868 (76 FR 73491, November 29, 2011), currently requires 
repetitive inspections for cracking on the lower cap of the rear spar 
of the left and right wings between stations Xors=417 and the outboard 
edge of the lower cap splice of the wing rear spar at station Xors=400; 
temporary and permanent repairs if necessary; and repetitive 
inspections of repaired areas, and corrective actions if necessary, for 
certain Model DC-10-10, DC-10-10F, and MD-10-10F airplanes.
    As published, the airplane manufacturer name specified in the 
subject line, product identification section, and paragraph (c) of AD 
2011-24-04, Amendment 39-16868 (76 FR 73491, November 29, 2011), is 
incorrect.
    As published, the email address provided in paragraphs (i)(1) and 
(j) of AD 2011-24-04, Amendment 39-16868 (76 FR 73491, November 29, 
2011), is incorrect.
    No other part of the preamble or regulatory information has been 
changed; therefore, only the changed portions of the final rule are 
being published in the Federal Register.
    The effective date of this AD remains January 3, 2012.

Correction of Non-Regulatory Text

    In the Federal Register of November 29, 2011, AD 2011-24-04, 
Amendment 39-16868 (76 FR 73491, November 29, 2011), is corrected as 
follows:
    On page 73491, in the second column, in the subject line, change 
the subject line to read as follows:

``Airworthiness Directives; The Boeing Company Airplanes.''

Correction of Regulatory Text


Sec.  39.13  [Corrected]

0
In the Federal Register of November 29, 2011, on page 73492, in the 
third column, the product identification line of AD 2011-24-04, 
Amendment 39-16868 (76 FR 73491, November 29, 2011), is corrected to 
read as follows:
* * * * *
2011-24-04 The Boeing Company: Amendment 39-16868; Docket No. FAA-
2010-1206; Directorate Identifier 2009-NM-216-AD.
* * * * *
0
In the Federal Register of November 29, 2011, on page 73492, in the 
third column, paragraph (c) of AD 2011-24-04 Amendment 39-16868 (76 FR 
73491, November 29, 2011), is corrected to read as follows:
* * * * *

(c) Applicability

    This AD applies to The Boeing Company Model DC-10-10, DC-10-10F, 
and MD-10-10F airplanes; certificated in any category; as identified 
in Boeing Alert Service Bulletin DC10-57A156, Revision 2, dated 
August 23, 2011.
* * * * *
0
In the Federal Register of November 29, 2011, on page 73493, in the 
third column, paragraph (i)(1) of AD 2011-24-04 Amendment 39-16868 (76 
FR 73491, November 29, 2011), is corrected to read as follows:
* * * * *
    (1) The Manager, Los Angeles Aircraft Certification Office, 
(ACO) FAA, has the authority to approve AMOCs for this AD, if 
requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Nenita Odesa, Aerospace Engineer, Airframe 
Branch, ANM-120L, FAA, Los Angeles ACO, 3960 Paramount Boulevard, 
Lakewood, California 97012-4137; phone: 562-627-5234; fax: 562-627-
5210; email: [email protected].
* * * * *
0
In the Federal Register of November 29, 2011, on page 73494, in the 
first column, paragraph (j) of AD 2011-24-04 Amendment 39-16868 (76 FR 
73491, November 29, 2011), is corrected to read as follows:
* * * * *

(i) Related Information

    For more information about this AD, contact Nenita Odesa, 
Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles ACO, 
3960 Paramount Boulevard, Lakewood, California 97012-4137; phone: 
562-627-5234; fax: 562-627-5210; email: [email protected].
* * * * *

    Issued in Renton, Washington, on January 23, 2012.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-2295 Filed 2-2-12; 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 2026-10-09T03:04:55.954624+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
f7c5c966625a30e4715e6674e446d23dc336d2d30ca7cc462ccb9f5026ba987b
Text SHA-256
355f2c30c48aad9da0f77a140a768c76c8d564c09d76f018d05e531f0e710f25

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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.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.