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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.

Why this record is shown

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
Source row
results[139]
Raw source SHA-256
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

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Find all recorded historical references to AD 2004-21-08 R1 · 0 printed reference observations in this pinned collection.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.

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: 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]


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

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.

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

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

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:55:30.812183+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
035c542239e2803fb0173ecdf20813eeaacf4f6012e7f49d9ca1a7b85aefcd7a
Text SHA-256
6c256244ecdde5b3f0a01fcde6b8ce85820ac18be43e41513dcdb608b978963f

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Coverage and limits

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.