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Published 2010-11-16 · Federal Register document 2010-28579

Airworthiness Directives; Cessna Aircraft Company (Cessna) 172, 175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 Series Airplanes

Publication summary

The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to the products listed above. In the Information Heading and in the SUMMARY section of the published AD, we incorrectly included Cessna 188 series airplanes. In the Unsafe Condition section, we incorrectly designated that paragraph as (e) instead of (d). Also in the Compliance section, paragraph (f)(2), and in Figure 1, we incorrectly stated the mailing address for the report. We are issuing this document to help eliminate any confusion that this AD may have created in the Information Heading and in the SUMMARY and Unsafe Condition sections. 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 2026-09-03T22:23:33.146842+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2010-a7267cd3a71dbd26
Source row
results[372]
Raw source SHA-256
a7267cd3a71dbd2645583c8a673df65e4a7fa9360a96e3be0de5b81f9d68c9a0

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2008-26-10
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2008-26-10 · 0 printed reference observations in this pinned collection.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: b8254c1983f55d846b4aead96d582fd788865de8534fee876a43ba6ec4a19bfc. Source manifest: ac6a5653c58150f914bdf14fa9f4a2a55ef0de7dd8fcd87706b35752914d9a8f.

Official source · 2010-11-16

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 75, Number 220 (Tuesday, November 16, 2010)]
[Rules and Regulations]
[Pages 69861-69862]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-28579]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-1328; Directorate Identifier 2008-CE-066-AD; 
Amendment 39-15776; AD 2008-26-10]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company (Cessna) 172, 
175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 Series 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an airworthiness directive (AD) that was 
published in the Federal Register. That AD applies to the products 
listed above. In the Information Heading and in the SUMMARY section of 
the published AD, we incorrectly included Cessna 188 series airplanes. 
In the Unsafe Condition section, we incorrectly designated that 
paragraph as (e) instead of (d). Also in the Compliance section, 
paragraph (f)(2), and in Figure 1, we incorrectly stated the mailing 
address for the report. We are issuing this document to help eliminate 
any confusion that this AD may have created in the Information Heading 
and in the SUMMARY and Unsafe Condition sections. This document 
corrects those errors. In all other respects, the original document 
remains the same.

DATES: This final rule is effective November 16, 2010. The effective 
date for AD 2008-26-10 remains January 5, 2009.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the

[[Page 69862]]

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: Ann Johnson, Aerospace Engineer, FAA, 
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, 
Wichita, Kansas 67209; telephone: 316-946-4105; fax: 316-946-4107; e-
mail address: [email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2008-26-10, 
Amendment 39-15776 (73 FR 78939, December 24, 2008), currently requires 
inspecting the alternate static air source selector valve to assure 
that the part number identification placard does not obstruct the 
alternate static air source selector valve port. If the part number 
identification placard obstructs the port, this AD also requires 
removing the placard, assuring that the port is unobstructed, and 
reporting to the FAA if obstruction is found for certain Cessna 172, 
175, 177, 180, 182, 185, 206, 207, 208, 210, 303, 336, and 337 series 
airplanes.
    As published, the Information Heading and the Summary sections of 
the AD incorrectly included Cessna 188 series airplanes. The Unsafe 
Condition section is incorrectly designated as paragraph (e) instead of 
paragraph (d). Also, the mailing address for the report specified in 
the Compliance section, paragraph (f)(2), and in Figure 1 is 
incorrectly stated as 1804 instead of 1801.
    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 AD 2008-26-10 remains January 5, 2009.

Correction of Non-Regulatory Text

    In the Federal Register of December 24, 2008, AD 2008-26-10; 
Amendment 39-15776 is corrected as follows:
    On page 78939, in the second column, on line 10, under the heading 
DEPARTMENT OF TRANSPORTATION, remove 188 from affected series 
airplanes.
    On page 78939, in the second column, on line 19, under the heading 
DEPARTMENT OF TRANSPORTATION, in the SUMMARY section, remove 188 from 
affected series airplanes.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

    In the Federal Register of December 24, 2008, AD 2008-26-10; 
Amendment 39-15776 is corrected as follows:
    On page 78942, in the first column, under the Unsafe Condition 
section, change paragraph (e) to (d).
    On page 78943, in the second column, in paragraph (f)(2), on line 
3, change 1804 to 1801.
    On page 78943, in Figure 1, in the address for the Wichita 
Manufacturing Inspection District Office, change 1804 to 1801.

    Issued in Kansas City, Missouri, on November 4, 2010.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-28579 Filed 11-15-10; 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 2026-10-09T03:12:16.102512+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
355660f05224b35ca605cd5d52791bf010e4c0757c816f6cf6a7ecf2e94af89b
Text SHA-256
b8254c1983f55d846b4aead96d582fd788865de8534fee876a43ba6ec4a19bfc

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