Airworthiness Directives; Cessna Aircraft Company Airplanes

AD 2011-28861 Published 2011-11-08 12 models 8,563 US-registered tails affected Federal Register ↗

Abstract

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.

Applicability

Aircraft makes and models this AD applies to, sorted by US-registered fleet size.

CESSNA 152 TCDS 3A19 1,638 tails
CESSNA 150L TCDS 3A19 1,452 tails
CESSNA 150M TCDS 3A19 1,435 tails
CESSNA 150F TCDS 3A19 1,061 tails
CESSNA 150G TCDS 3A19 979 tails
CESSNA 150H TCDS 3A19 757 tails
CESSNA 150J TCDS 3A19 658 tails
CESSNA 150K TCDS 3A19 303 tails
CESSNA A150M TCDS 3A19 80 tails
CESSNA A150L TCDS 3A19 80 tails
CESSNA A150K TCDS 3A19 72 tails
CESSNA A152 TCDS 3A19 48 tails

Federal Register text

Verbatim from the Federal Register publication — required actions, compliance times, parts/serial numbers, and methods of compliance. The Federal Register is the legally binding document; this rendering is for readability. Cite: 76 FR 69123.

[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] BILLING CODE 4910-13-P

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