AD 2011-06-02

final rule

Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI

AD Number
2011-06-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-1243
FR Citation
76 FR 27239

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 172F (USAF T-41A) Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172G Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172H (USAF T-41A) Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172I Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172K Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172L Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172M Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172N Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172P Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172R Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company 172S Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172F Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172G Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172H Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172K Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172L Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172M Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172N Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI
aircraft Cessna Aircraft Company F172P Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI

Unsafe Condition

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to the products listed above. The numbering of paragraphs (j)(3), (j)(4), and (j)(5) in the Material Incorporated by Reference section is incorrect. This document corrects that error. In all other respects, the original document remains the same.

Required Actions

Install a full authority digital engine control (FADEC) backup battery. Replace the supplement pilot's operating handbook and FAA approved airplane flight manual. Replace the FADEC backup battery every 12 calendar months.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months of effective date

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Cessna Aircraft Company Model 172 airplanes modified by Supplemental Type Certificate (STC) SA01303WI.

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 the products listed above. The numbering of paragraphs (j)(3), (j)(4), and (j)(5) in the Material Incorporated by Reference section is incorrect. This document corrects that error. In all other respects, the original document remains the same.

Document Text

Show stored source text (verify against official source)
[Federal Register Volume 76, Number 91 (Wednesday, May 11, 2011)]
[Rules and Regulations]
[Page 27239]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2011-11260]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1243; Directorate Identifier 2010-CE-058-AD; 
Amendment 39-16626; AD 2011-06-02]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company (Cessna) Model 
172 Airplanes Modified by Supplemental Type Certificate (STC) SA01303WI

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 the products 
listed above. The numbering of paragraphs (j)(3), (j)(4), and (j)(5) in 
the Material Incorporated by Reference section is incorrect. This 
document corrects that error. In all other respects, the original 
document remains the same.

DATES: This final rule is effective May 26, 2011.

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: Richard Rejniak, Aerospace Engineer, 
Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, 
Room 100; phone: (316) 946-4128; fax: (316) 946-4107; e-mail: 
<a href="/cdn-cgi/l/email-protection#d8aab1bbb0b9aabcf6aabdb2b6b1b9b398beb9b9f6bfb7ae"><span class="__cf_email__" data-cfemail="77051e141f1605135905121d191e161c3711161659101801">[email&#160;protected]</span></a>.

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-06-02, 
amendment 39-16626 (76 FR 22298, April 21, 2011), currently requires 
installing a full authority digital engine control (FADEC) backup 
battery, replacing the supplement pilot's operating handbook and FAA 
approved airplane flight manual, and replacing the FADEC backup battery 
every 12 calendar months for Cessna Aircraft Company (Cessna) Model 172 
Airplanes modified by Supplemental Type Certificate (STC) SA01303WI.
    As published, the numbering of paragraphs (j)(3), (j)(4), and 
(j)(5) in the Material Incorporated by Reference section is incorrect.
    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 26, 2011.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

    In the Federal Register of April 21, 2011, on page 22301, in the 
right column, paragraph (j) of AD 2011-06-02 is corrected to read as 
follows:
* * * * *
    (1) For service information identified in this AD, contact Thielert 
Aircraft Engines Service GmbH, Platanenstra[szlig]e 14, D-09350 
Lichtenstein, Deutschland; telephone: +49 (37204) 696-1474; fax: +49 
(37204) 696-1910; Internet: <a href="http://www.thielert.com/">http://www.thielert.com/</a>.
    (2) You may review copies of the service information at the FAA, 
Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. 
For information on the availability of this material at the FAA, call 
816-329-4148.
    (3) You may also review copies of the service information that is 
incorporated by reference at the National Archives and Records 
Administration (NARA). For information on the availability of this 
material at an NARA facility, call 202-741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
* * * * *

    Issued in Kansas City, Missouri, on May 3, 2011.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2011-11260 Filed 5-10-11; 8:45 am]
BILLING CODE 4910-13-P

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.