Published 2013-04-29 · Federal Register document 2013-09496
Airworthiness Directives; Cessna Aircraft Company Airplanes
Publication summary
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Cessna Aircraft Company (Cessna) Models 190, 195 (L-126A,B,C), 195A, and 195B airplanes that are equipped with certain inboard aileron hinge brackets. The AD docket number in the preamble section and the rule portion of the AD is incorrect. Also, the statement that no comments on the notice of proposed rulemaking (NPRM) were received is incorrect. This document corrects these errors. In all other respects, the original document remains the same.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
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- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2004-21-08 R1
- Effective date printed in this edition
- Unknown
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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Find all recorded historical references to AD 2004-21-08 R1 · 0 printed reference observations in this pinned collection.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: 6c256244ecdde5b3f0a01fcde6b8ce85820ac18be43e41513dcdb608b978963f. Source manifest: 54b92422ac638384314ffc8da610144ec293f36503e5e8e3ba9026713b14723e.
Official source · 2013-04-29
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 78, Number 82 (Monday, April 29, 2013)]
[Rules and Regulations]
[Page 24985]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-09496]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2004-18033; Directorate Identifier 2004-CE-16-AD;
Amendment 39-17400; AD 2004-21-08 R1]
RIN 2120-AA64
Airworthiness Directives; Cessna Aircraft Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to all Cessna
Aircraft Company (Cessna) Models 190, 195 (L-126A,B,C), 195A, and 195B
airplanes that are equipped with certain inboard aileron hinge
brackets. The AD docket number in the preamble section and the rule
portion of the AD is incorrect. Also, the statement that no comments on
the notice of proposed rulemaking (NPRM) were received is incorrect.
This document corrects these errors. In all other respects, the
original document remains the same.
DATES: This correction is effective April 29, 2013. The effective date
for AD 2004-21-08 R1 remains May 9, 2013.
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: Gary Park, Aerospace Engineer, Wichita
ACO, FAA, 1801 Airport Road, Wichita, KS 67209; phone: (316) 946-4123;
fax: (316) 946-4107; email: [email protected].
SUPPLEMENTARY INFORMATION: AD 2004-21-08 R1, amendment 39-17400 (78 FR
20227, April 4, 2013), currently requires you to repetitively inspect
the affected inboard aileron hinge brackets for cracks or corrosion and
replace them if cracks or corrosion is found for all Cessna Models 190,
195 (L-126A,B,C), 195A, and 195B airplanes that are equipped with
certain inboard aileron hinge brackets. Replacement with aluminum
brackets would terminate the need for the repetitive inspections.
Future compliance requires following a revised service bulletin that
clarifies the casting numbers and part numbers to be inspected.
As published, the AD docket number in the final rule headings and
in the headings of the AD is incorrect.
It was incorrectly stated in the comments section that we received
no comments on the NPRM (78 FR 1155, January 8, 2013). We received one
supportive comment on the NPRM.
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 May 9, 2013.
Correction of Non-Regulatory Text
In the Federal Register of April 4, 2013, AD 2004-21-08 R1;
Amendment 39-17400 is corrected as follows:
On page 20227, in the first column, on line 4 in the headings of
the final rule, change ``Docket No. FAA-2012-18033 * * *.'' to ``Docket
No. FAA-2004-18033 * * *.''
On page 20227, in the third column, beginning on the second line
under the ``Comments'' section, change the second sentence from ``We
received no comments on the NPRM (78 FR 1155, January 8, 2013) or on
the determination of the cost to the public.'' to ``We received one
supportive comment on the NPRM (78 FR 1155, January 8, 2013) and no
comments on the determination of the cost to the public.''
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of April 4, 2013, on page 20228, in the second
column, the AD headings immediately following the second amendatory
instruction are corrected to read as follows:
2004-21-08 R1 Cessna Aircraft Company: Amendment 39-17400; Docket
No. FAA-2004-18033; Directorate Identifier 2004-CE-16-AD.
Issued in Kansas City, Missouri, on April 17, 2013.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-09496 Filed 4-26-13; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
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- 035c542239e2803fb0173ecdf20813eeaacf4f6012e7f49d9ca1a7b85aefcd7a
- Text SHA-256
- 6c256244ecdde5b3f0a01fcde6b8ce85820ac18be43e41513dcdb608b978963f
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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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