AD 2004-21-08 R1

AD Final Rules - 2004-21-08 R1_Correction.pdf
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AD Number:
2004-21-08 R1
Document Type:
AD Final Rules
Docket Number:
FAA-2004-18033
Subject Heading:
Airworthiness Directives; Cessna Aircraft Company Airplanes
Subject:
Aileron Control System
Status:
Current
Citation:
Federal Register Volume 78, Number 82 (Monday, April 29, 2013)
Citation Publish Date:
04/29/2013
Effective Date:
05/09/2013
Make:
Cessna Aircraft Company
Model:
190 | 195 | 195A | 195B
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
2004-21-08
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: Federal Register Volume 78, Number 82 (Monday, April 29, 2013); Page 24985.
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[Federal Register Volume 78, Number 82 (Monday, April 29, 2013)]


[Rules and Regulations]


[Page 24985]


From the Federal Register Online via the Government Printing 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:


gary.park@faa.gov.


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
2


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


§ 39.13 [Corrected]


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.