Federal Register / Vol. 76, No. 25 / Monday, February 7, 2011 / Rules and Regulations 6525 (2) The service information allows flight Kansas City, Missouri 64106. For information ACTION: Final rule. with known cracks provided they do not on the availability of this material at the exceed a certain limit. FAA policy does not FAA, call 816–329–4148. SUMMARY: We are superseding an allow flight with cracks in primary structure. existing airworthiness directive (AD) for Material Incorporated by Reference Since the fuselage is considered primary the products listed above. AD 2009–09– structure, we are mandating repair before (h) You must use RUAG Alert Service 09 currently requires repetitive further flight after any crack is found. Bulletin No. ASB–228–266, dated December inspections of the rudder hinges and the 1, 2006; and Dornier 228 Time Limits/ Other FAA AD Provisions Maintenance Checks Manual, Temporary rudder hinge brackets for damage, i.e., cracking, deformation, and (h) The following provisions also apply to Revision No. 05–27, dated August 4, 2008, to this AD: do the actions required by this AD, unless the discoloration. If damage is found during (1) Alternative Methods of Compliance AD specifies otherwise. any inspection, AD 2009–09–09 also (AMOCs): The Manager, Standards Office, (1) The Director of the Federal Register requires replacing the damaged rudder FAA, has the authority to approve AMOCs approved the incorporation by reference of hinge and/or rudder hinge bracket. This for this AD, if requested using the procedures Dornier 228 Time Limits/Maintenance new AD retains the inspection found in 14 CFR 39.19. Send information to Checks Manual, Temporary Revision No. 05– requirements of AD 2009–09–09, adds Attn: Greg Davison, Aerospace Engineer, 27, dated August 4, 2008, under 5 U.S.C. airplanes to the Applicability section, FAA, Small Airplane Directorate, 901 Locust, 552(a) and 1 CFR part 51. (2) On June 26, 2007 (72 FR 28591, May and adds a terminating action for the Room 301, Kansas City, Missouri 64106; repetitive inspection requirements. This telephone: (816) 329–4130; fax: (816) 329– 22, 2007), the Director of the Federal Register 4090. Before using any approved AMOC on previously approved the incorporation by AD resulted from the manufacturer any airplane to which the AMOC applies, reference of RUAG Alert Service Bulletin No. developing a modification that notify your appropriate principal inspector ASB–228–266, dated December 1, 2006. terminates the repetitive inspections (PI) in the FAA Flight Standards District (3) For service information identified in and from the manufacture adding Office (FSDO), or lacking a PI, your local this AD, contact RUAG Aerospace Services airplane serial numbers into the FSDO. GmbH, Dornier 228 Customer Support, P.O. Applicability section. We are issuing Box 1253, 82231 Wessling, Germany; (2) Airworthy Product: For any requirement this AD to detect and correct damage in in this AD to obtain corrective actions from telephone: + 49 (0) 8153–302280; fax: + 49 (0) 8153–303030. the rudder hinges and the rudder hinge a manufacturer or other source, use these brackets, which could result in failure of actions if they are FAA-approved. Corrective (4) You may review copies of the actions are considered FAA-approved if they referenced service information at the FAA, the rudder. This failure could lead to are approved by the State of Design Authority Small Airplane Directorate, 901 Locust, loss of control. (or their delegated agent). You are required Kansas City, Missouri 64106. For information DATES: This AD is effective March 14, to assure the product is airworthy before it on the availability of this material at the 2011. is returned to service. FAA, call 816–329–4148. The Director of the Federal Register (3) Reporting Requirements: For any (5) You may also review copies of the approved the incorporation by reference service information incorporated by reference reporting requirement in this AD, a federal of certain publications listed in the AD agency may not conduct or sponsor, and a for this AD at the National Archives and Records Administration (NARA). For as of March 14, 2011. person is not required to respond to, nor The Director of the Federal Register shall a person be subject to a penalty for information on the availability of this material at NARA, call (202) 741–6030, or go approved the incorporation by reference failure to comply with a collection of to: http://www.archives.gov/federal_register/ information subject to the requirements of of a certain publication listed in this AD code_of_federal_regulations/ the Paperwork Reduction Act unless that as of May 11, 2009 (74 FR 19873, April ibr_locations.html. collection of information displays a current 30, 2009). valid OMB Control Number. The OMB Issued in Kansas City, Missouri, on January ADDRESSES: For service information Control Number for this information 25, 2011. identified in this AD, contact Cessna collection is 2120–0056. Public reporting for John Colomy, Aircraft Company, Product Support, this collection of information is estimated to Acting Manager, Small Airplane Directorate, P.O. Box 7706; Wichita, Kansas 67277; be approximately 5 minutes per response, Aircraft Certification Service. telephone: (316) 517–5800; fax: (316) including the time for reviewing instructions, completing and reviewing the collection of [FR Doc. 2011–2006 Filed 2–4–11; 8:45 am] 942–9006; Internet: http:// information. All responses to this collection BILLING CODE 4910–13–P www.cessna.com. You may review of information are mandatory. Comments copies of the referenced service concerning the accuracy of this burden and information at the FAA, Small Airplane suggestions for reducing the burden should DEPARTMENT OF TRANSPORTATION Directorate, 901 Locust, Kansas City, be directed to the FAA at: 800 Independence Missouri 64106. For information on the Ave. SW., Washington, DC 20591, Attn: Federal Aviation Administration availability of this material at the FAA, Information Collection Clearance Officer, call (816) 329–4148. AES–200. 14 CFR Part 39 Examining the AD Docket Related Information [Docket No. FAA–2009–1186; Directorate (i) Refer to MCAI European Aviation Safety Identifier 2009–CE–065–AD; Amendment You may examine the AD docket on Agency (EASA) AD No.: 2009–0085, dated 39–16588; AD 2011–03–04] the Internet at http:// April 14, 2009; RUAG Alert Service Bulletin www.regulations.gov; or in person at the RIN 2120–AA64 No. ASB–228–266, dated December 1, 2006; Docket Management Facility between and Dornier 228 Time Limits/Maintenance Airworthiness Directives; Cessna 9 a.m. and 5 p.m., Monday through Checks Manual, Temporary Revision No. 05– Aircraft Company (Type Certificate Friday, except Federal holidays. The AD 27, dated August 4, 2008, for related docket contains this AD, the regulatory information. For service information related Previously Held by Columbia Aircraft Manufacturing (Previously the Lancair evaluation, any comments received, and to this AD, contact RUAG Aerospace Services other information. The address for the GmbH, Dornier 228 Customer Support, P.O. Company)) Models LC40–550FG, Docket Office (phone: 800–647–5527) is Box 1253, 82231 Wessling, Germany; LC41–550FG, and LC42–550FG telephone: + 49 (0) 8153–302280; fax: + 49 Airplanes Document Management Facility, U.S. (0) 8153–303030. You may review copies of Department of Transportation, Docket the referenced service information at the AGENCY: Federal Aviation Operations, M–30, West Building FAA, Small Airplane Directorate, 901 Locust, Administration (FAA), DOT. Ground Floor, Room W12–140, 1200 VerDate Mar<15>2010 14:36 Feb 04, 2011 Jkt 223001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\07FER1.SGM 07FER1 wwoods2 on DSK1DXX6B1PROD with RULES_PART 1 6526 Federal Register / Vol. 76, No. 25 / Monday, February 7, 2011 / Rules and Regulations New Jersey Avenue SE., Washington, Register on October 27, 2010 (75 FR public interest require adopting the AD DC 20590. 66009). That SNPRM proposed to retain as proposed except for minor editorial FOR FURTHER INFORMATION CONTACT: Gary the inspection requirements of AD changes. We have determined that these Park, Aerospace Engineer, Wichita 2009–09–09, add airplanes to the minor changes: Aircraft Certification Office, FAA, 1801 Applicability section, and add a • Are consistent with the intent that terminating action for the repetitive Airport Road, Room 100, Wichita, was proposed in the SNPRM for inspection requirements using revised Kansas 67209; telephone: (316) 946– correcting the unsafe condition; and 4123; fax: (316) 946–4107; e-mail: service information. [email protected]. • Do not add any additional burden Comments upon the public than was already SUPPLEMENTARY INFORMATION: We gave the public the opportunity to proposed in the SNPRM. Discussion participate in developing this AD. We Costs of Compliance We issued a supplemental notice of received no comments on the SNPRM or proposed rulemaking (SNPRM) to on the determination of the cost to the We estimate that this proposed AD amend 14 CFR part 39 to supersede AD public. affects 790 airplanes of U.S. registry. 2009–09–09, Amendment 39–15895 (74 Conclusion We estimate the following costs to FR 19873, April 30, 2009). That AD comply with this AD: applies to the specified products. The We reviewed the relevant data and SNPRM published in the Federal determined that air safety and the ESTIMATED COSTS Action Labor cost Parts cost Cost per product Cost on U.S. operators Inspecting the rudder hinges and 1.5 work-hours × $85 per hour = Not applicable .... $127.50 per in- $72,675 per inspection rudder hinge brackets for damage $127.50 per inspection cycle. spection cycle. cycle. with rudder removed (affects 570 airplanes). Inspecting the rudder hinges and .5 work-hour × $85 per hour = Not applicable .... $42.50 per in- $24,225 per inspection rudder hinge brackets for damage $42.50 per inspection cycle. spection cycle. cycle.