[Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011)]
[Rules and Regulations]
[Page 69123]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-28861]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27747; Directorate Identifier 2007-CE-030-AD;
Amendment 39-16782; AD 2009-10-09 R2]
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 certain Cessna
Aircraft Company (Cessna) Models 150F, 150G, 150H, 150J, 150K, 150L,
150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L,
F150M, FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and
FA152 airplanes. There is an error in the compliance instructions. This
document corrects that error. In all other respects, the original
document remains the same.
DATES: This final rule; correction, is effective November 8, 2011. The
effective date for AD 2009-10-09 R2 remains September 12, 2011.
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: Ann Johnson, Aerospace Engineer, FAA,
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; phone: (316) 946-4105; fax: (316) 946-4107;
email: [email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2009-10-09 R2,
Amendment 39-16782 (76 FR 53308, August 26, 2011), currently requires
either installing a placard prohibiting spins and other acrobatic
maneuvers in the airplane or replacing the rudder stop, the rudder stop
bumper, and the attachment hardware with a new rudder stop modification
kit for certain Cessna Models 150F, 150G, 150H, 150J, 150K, 150L, 150M,
A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M,
FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and FA152
airplanes.
As published, the text in the Procedures column of Table 2 in
paragraph (g)(1) of this AD incorrectly states ``* * * fabricate the
placard required in paragraph (g)(1)(i) of this AD * * *'', and the
text should refer to paragraph (g)(1)(ii).
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 September 12, 2011.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
In the Federal Register of August 26, 2011, on page 53311, in the
3rd column, Procedures, paragraph (g)(1), Table 2--Actions, Compliance
and Procedures, of AD 2009-10-09 R2 is corrected to read as follows:
* * * * *
A person authorized to perform maintenance as specified in 14
CFR 43.3 of the Federal Aviation Administration Regulations (14 CFR
43.3) is required to make the AFM and POH changes, fabricate the
placard required in paragraph (g)(1)(ii) of this AD, and make an
entry into the aircraft logbook showing compliance with the portion
of the AD per compliance with 14 CFR 43.9.
* * * * *
Issued in Kansas City, Missouri, on November 2, 2011.
John R. Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-28861 Filed 11-7-11; 8:45 am]
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