AD 2011-24-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; The Boeing Company Airplanes. |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; The Boeing Company Airplanes. |
| aircraft | The Boeing Company | MD-10-10F | Airworthiness Directives; The Boeing Company Airplanes. |
Unsafe Condition
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections for cracking; perform temporary and permanent repairs if necessary; conduct repetitive inspections of repaired areas; and take corrective actions if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Applicability Source Text
Show captured applicability text from the source AD
(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: <a href="/cdn-cgi/l/email-protection#b8d6ddd6d1ccd996d7dcddcbd9f8ded9d996dfd7ce"><span class="__cf_email__" data-cfemail="96f8f3f8ffe2f7b8f9f2f3e5f7d6f0f7f7b8f1f9e0">[email protected]</span></a>.
* * * * *
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:
* * * * *
Document Text
Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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 <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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:
<a href="/cdn-cgi/l/email-protection#68060d06011c0946070c0d1b09280e0909460f071e"><span class="__cf_email__" data-cfemail="69070c07001d0847060d0c1a08290f0808470e061f">[email protected]</span></a>.
[[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: <a href="/cdn-cgi/l/email-protection#b8d6ddd6d1ccd996d7dcddcbd9f8ded9d996dfd7ce"><span class="__cf_email__" data-cfemail="96f8f3f8ffe2f7b8f9f2f3e5f7d6f0f7f7b8f1f9e0">[email protected]</span></a>.
* * * * *
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: <a href="/cdn-cgi/l/email-protection#8fe1eae1e6fbeea1e0ebeafceecfe9eeeea1e8e0f9"><span class="__cf_email__" data-cfemail="a8c6cdc6c1dcc986c7cccddbc9e8cec9c986cfc7de">[email protected]</span></a>.
* * * * *
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
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