Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes, 11572-11575 [2013-03407]

Download as PDF 11572 Federal Register / Vol. 78, No. 33 / Tuesday, February 19, 2013 / Rules and Regulations the certification basis of the airplane and the approval must specifically refer to this AD. DEPARTMENT OF TRANSPORTATION (m) Related Information Federal Aviation Administration (1) For more information about this AD, contact Nancy Marsh, Aerospace Engineer, Airframe Branch, ANM–120S, Seattle Aircraft Certification Office (ACO), FAA, 1601 Lind Avenue SW., Renton, Washington 98057–3356; phone: 425–917–6440; fax: 425– 917–6590; email: Nancy.Marsh@faa.gov. (2) For Boeing service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H–65, Seattle, Washington 98124–2207; phone: 206–544–5000, extension 1; fax: 206– 766–5680; Internet: https:// www.myboeingfleet.com. (n) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing Special Attention Service Bulletin 757–57–0068, Revision 1, dated July 19, 2011. (ii) Reserved. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H–65, Seattle, Washington 98124–2207; phone: 206–544–5000, extension 1; fax: 206–766– 5680; Internet: https:// www.myboeingfleet.com. (4) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on February 6, 2013. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2013–03268 Filed 2–15–13; 8:45 am] sroberts on DSK5SPTVN1PROD with RULES BILLING CODE 4910–13–P VerDate Mar<15>2010 15:41 Feb 15, 2013 Jkt 229001 14 CFR Part 39 [Docket No. FAA–2012–0732; Directorate Identifier 2012–CE–022–AD; Amendment 39–17311; AD 2012–26–16] RIN 2120–AA64 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: We are superseding an existing airworthiness directive (AD) for all Pilatus Aircraft Ltd. Models PC–12, PC–12/45, PC–12/47, and PC–12/47E airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a need to incorporate new revisions into the Limitations section, Chapter 4, of the FAA-approved maintenance program (e.g., maintenance manual). We are issuing this AD to require actions to address the unsafe condition on these products. SUMMARY: This AD is effective March 26, 2013. The Director of the Federal Register approved the incorporation by reference of certain publications listed in the AD as of March 26, 2013. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of August 19, 2009 (74 FR 34213, July 15, 2009). ADDRESSES: You may examine the AD docket on the Internet at https:// www.regulations.gov or in person at 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 service information identified in this AD, contact Pilatus Aircraft Ltd., Customer Service Manager, CH–6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; Internet: https://www.pilatusaircraft.com or email: SupportPC12@pilatus-aircraft.com. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For DATES: PO 00000 Frm 00022 Fmt 4700 Sfmt 4700 information on the availability of this material at the FAA, call (816) 329– 4148. FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329– 4059; fax: (816) 329–4090; email: doug.rudolph@faa.gov. SUPPLEMENTARY INFORMATION: Discussion We issued a supplemental notice of proposed rulemaking (SNPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That SNPRM was published in the Federal Register on October 22, 2012 (77 FR 64442), which proposed to supersede AD 2009–14–13, Amendment 39–15963 (74 FR 34213, July 15, 2009). Since we issued AD 2009–14–13, Amendment 39–15963 (74 FR 34213, July 15, 2009), Pilatus Aircraft Ltd. has issued revisions to the Limitations section of the airplane maintenance manual to include an inspection of the wing main spar fastener holes at rib 6 for cracks. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued AD No. 2012– 0099, dated June 8, 2012 (referred to after this as ‘‘the MCAI’’), to correct an unsafe condition for the specified products. The MCAI states: The mandatory instructions and airworthiness limitations applicable to the Structure and Components of the PC–12 are specified in the Aircraft Maintenance Manual (AMM) under Chapter 4. Prompted by a crack found on one wing of the aeroplane fleet leader, a more restrictive airworthiness limitation was introduced, in that manual, for the inspection of the main spar rib 6 strap fastener. These documents include the maintenance instructions and/or airworthiness limitations developed by Pilatus Aircraft Ltd. and approved by EASA. Failure to comply with these instructions and limitations could potentially lead to unsafe condition. For the reasons described above, this AD requires the implementation of more restrictive maintenance instructions and/or airworthiness limitations. You may obtain further information by examining the MCAI in the AD docket. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the SNPRM (77 FR 64442, October 22, 2012) or on the determination of the cost to the public. E:\FR\FM\19FER1.SGM 19FER1 Federal Register / Vol. 78, No. 33 / Tuesday, February 19, 2013 / Rules and Regulations Conclusion We reviewed the relevant data and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial changes. We have determined that these minor changes: • Are consistent with the intent that was proposed in the SNPRM (77 FR 64442, October 22, 2012) for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the SNPRM (77 FR 64442, October 22, 2012). Costs of Compliance We estimate that this AD will affect 678 products of U.S. registry. We also estimate that it will take about 3.5 workhours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $300 per product. Based on these figures, we estimate the cost of this AD on U.S. operators to be $405,105, or $597.50 per product. In addition, we estimate that any necessary corrective actions that must be taken based on incorporating the new revisions into the limitation section of the maintenance manual will take about 6 work-hours and require parts costing approximately $4,000, for a cost of $4,510 per product. We have no way of determining the number of products that may need these necessary corrective actions. We estimate that it will take about 12 work-hours per product to comply with the new addition of the wing main spar fastener holes inspection requirement of this AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of the wing main spar fastener holes on U.S. operators to be $691,560, or $1,020 per product. In addition, we estimate that any necessary repairs to the wing main spar will take about 7 work-hours and require parts costing approximately $5,000, for a cost of $5,595 per product. We have no way of determining the number of products that may need these corrective actions. sroberts on DSK5SPTVN1PROD with RULES Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. ‘‘Subtitle VII: Aviation Programs,’’ describes in more detail the scope of the Agency’s authority. We are issuing this rulemaking under the authority described in ‘‘Subtitle VII, VerDate Mar<15>2010 15:41 Feb 15, 2013 Jkt 229001 Part A, Subpart III, Section 44701: General requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Is not a ‘‘significant rule’’ under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. Examining the AD Docket You may examine the AD docket on the Internet at https:// 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 the SNPRM (77 FR 64442, October 22, 2012), the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone (800) 647– 5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PO 00000 Frm 00023 Fmt 4700 Sfmt 4700 11573 PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by removing Amendment 39–15963 (74 FR 34213, July 15, 2009), and adding the following new AD: ■ 2012–26–16 Pilatus Aircraft Ltd.: Amendment 39–17311; Docket No. FAA–2012–1052; Directorate Identifier 2012–CE–014–AD. (a) Effective Date This airworthiness directive (AD) becomes effective March 26, 2013. (b) Affected ADs This AD supersedes AD 2009–14–13, Amendment 39–15963 (74 FR 34213, July 15, 2009). (c) Applicability This AD applies to Pilatus Aircraft Ltd. Models PC–12, PC–12/45, PC–12/47, and PC– 12/47E airplanes, all manufacturer serial numbers (MSNs), certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 05: Time Limits. (e) Reason This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a need to incorporate new revisions into the Limitations section, Chapter 4, of the FAAapproved maintenance program (e.g., maintenance manual). The limitations were revised to include an inspection of the wing main spar fastener holes at rib 6 for cracks. These actions are required to ensure the continued operational safety of the affected airplanes. (f) Actions and Compliance Unless already done, do the following actions: (1) For Models PC–12 and PC–12/45 airplanes, MSNs 101 through 299: Within the next 100 hours time-in-service (TIS) after August 19, 2009 (the effective date retained from AD 2009–14–13, Amendment 39–15963 (74 FR 34213, July 15, 2009)) or 1 year after August 19, 2009 (the effective date retained from AD 2009–14–13), whichever occurs first, replace the torque tube part number (P/ N) 532.50.12.047 with torque tube P/N 532.50.12.064 following PILATUS AIRCRAFT LTD. Service Bulletin No: 32– 021, dated November 21, 2008. (2) For all airplanes: As of March 26, 2013 (the effective date of this AD), do not install torque tube P/N 532.50.12.047. (3) For all airplanes: Before further flight after March 26, 2013 (the effective date of E:\FR\FM\19FER1.SGM 19FER1 11574 Federal Register / Vol. 78, No. 33 / Tuesday, February 19, 2013 / Rules and Regulations sroberts on DSK5SPTVN1PROD with RULES this AD), insert Data module code 12–A–04– 00–00–00A–000A–A, ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, PC 12/47 AMM Document No. 02049, 12–A–AM–00–00–00– I, revision 26, dated December 15, 2012, for Models PC–12, PC–12/45, PC–12/47, and Data module code 12–B–04–00–00–00A– 000A–A, ‘‘STRUCTURAL AND COMPONENT LIMITATIONS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC 12/47E AMM Document No. 02300, 12–B–AM–00–00–00–I, revision 9, dated December 15, 2012, for Model PC–12/ 47E, into the Limitations section of the FAAapproved maintenance program (e.g., maintenance manual). These limitations section revisions do the following: (i) Establish an inspection of the wing main spar fastener holes at rib 6, (ii) Specify replacement of components before or upon reaching the applicable life limit, and (iii) Specify accomplishment of all applicable maintenance tasks within certain thresholds and intervals. (4) For all airplanes: If no compliance time is specified in the documents listed in paragraph (f)(3) of this AD when doing any corrective actions where discrepancies are found as required in paragraph (f)(3)(iii) of this AD, do these corrective actions before further flight after doing the applicable maintenance task. (5) For all airplanes: During the accomplishment of the actions required in paragraphs (f)(3)(i), (f)(3)(ii), and (f)(3)(iii) of this AD, if a discrepancy is found that is not identified in the documents listed in paragraph (f)(3) of this AD, before further flight after finding the discrepancy, contact Pilatus Aircraft Ltd. at the address specified in paragraph (i)(5) of this AD for a repair scheme and incorporate that repair scheme. (g) Credit for Actions Accomplished in Accordance With Previous Service Information This paragraph provides credit for the actions required in paragraph (f)(3) of this AD if already done before March 6, 2013 (the effective date of this AD) following Pilatus PC12 Aircraft Maintenance Manual Temporary Revision No. 04–03, dated October 15, 2012, which transmits Unclassified 12–A/AMP–04 ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS— AIRWORTHINESS LIMITATIONS,’’ document 12–A–04–00–00–00A–000A–A, dated October 15, 2012; and Pilatus PC12/ 47E Aircraft Maintenance Manual Temporary Revision No. 04–01, dated October 15, 2012, which transmits Unclassified 12–B/AMP–04 ‘‘STRUCTURAL AND COMPONENT LIMITATIONS—AIRWORTHINESS LIMITATIONS,’’ document 12–B–04–00–00– 00A–000A–A, dated October 15, 2012. (h) Other FAA AD Provisions The following provisions also apply to this AD: VerDate Mar<15>2010 15:41 Feb 15, 2013 Jkt 229001 (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4059; fax: (816) 329– 4090; email: doug.rudolph@faa.gov. (i) Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (ii) AMOCs approved for AD 2009–14–13, Amendment 39–15963 (74 FR 34213, July 15, 2009) are not approved as AMOCs for this AD. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, a federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120–0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES–200. (i) Related Information Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2012–0099, dated June 8, 2012; Pilatus Aircraft Ltd. Service Bulletin No: 32–021, dated November 21, 2008; Data module code 12–A–04–00–00– 00A–000A–A, ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, PC 12/47 AMM Document No. 02049, 12–A–AM–00–00–00– I, revision 26, dated December 15, 2012; Data module code 12–B–04–00–00–00A–000A–A, ‘‘STRUCTURAL AND COMPONENT LIMITATIONS—AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC 12/47E AMM Document No. 02300, 12–B–AM–00–00–00– I, revision 9, dated December 15, 2012; PO 00000 Frm 00024 Fmt 4700 Sfmt 4700 Pilatus PC12 Aircraft Maintenance Manual Temporary Revision No. 04–03, dated October 15, 2012, which transmits Unclassified 12–A/AMP–04 ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS— AIRWORTHINESS LIMITATIONS,’’ document 12–A–04–00–00–00A–000A–A, dated October 15, 2012; and PC12/47E Aircraft Maintenance Manual Temporary Revision No. 04–01, dated October 15, 2012, which transmits Unclassified 12–B/AMP–04 ‘‘STRUCTURAL AND COMPONENT LIMITATIONS—AIRWORTHINESS LIMITATIONS,’’ document 12–B–04–00–00– 00A–000A–A, dated October 15, 2012, for related information. (i) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (3) The following service information was approved for IBR on March 26, 2013. (i) Data module code 12–A–04–00–00– 00A–000A–A, ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, PC 12/47 AMM Document No. 02049, 12–A–AM–00–00–00– I, revision 26, dated December 15, 2012. (ii) Data module code 12–B–04–00–00– 00A–000A–A, ‘‘STRUCTURAL AND COMPONENT LIMITATIONS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC 12/47E AMM Document No. 02300, 12–B–AM–00–00–00–I, revision 9, dated December 15, 2012. Note to paragraph (i)(3) of this AD: Data module code 12–A–04–00–00–00A–000A–A, ‘‘STRUCTURAL, COMPONENT AND MISCELLANEOUS—AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, PC 12/ 47 AMM Document No. 02049, 12–A–AM– 00–00–00–I, revision 26, dated December 15, 2012; and Data module code 12–B–04–00– 00–00A–000A–A, ‘‘STRUCTURAL AND COMPONENT LIMITATIONS— AIRWORTHINESS LIMITATIONS,’’ dated October 15, 2012, of the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC 12/47E AMM Document No. 02300, 12–B–AM–00–00–00–I, revision 9, dated December 15, 2012, were issued as complete updates to the AMM Airworthiness Limitations sections and incorporate all technical information contained in Pilatus AMM Temporary Revision No. 04–01 and Pilatus AMM Temporary Revision No. 04–03, both dated October 15, 2012. (4) The following service information was approved for IBR on August 19, 2009 (74 FR 34213, July 15, 2009). (i) Pilatus Aircraft Ltd. Service Bulletin No: 32–021, dated November 21, 2008. (ii) Reserved. E:\FR\FM\19FER1.SGM 19FER1 Federal Register / Vol. 78, No. 33 / Tuesday, February 19, 2013 / Rules and Regulations (5) For Pilatus Aircraft Ltd. service information identified in this AD, contact Pilatus Aircraft Ltd., Customer Service Manager, CH–6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; Internet: https://www.pilatusaircraft.com or email: SupportPC12@pilatusaircraft.com. (6) You may view this 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. (7) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ index.html. Issued in Kansas City, Missouri, on February 8, 2013. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2013–03407 Filed 2–15–13; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF JUSTICE 28 CFR Part 16 [CPCLO Order No. 001–2013] Privacy Act of 1974; Implementation Federal Bureau of Prisons, Department of Justice. ACTION: Final rule. AGENCY: The Department of Justice (DOJ or Department), Federal Bureau of Prisons (BOP), is issuing a final rule for the modified system of records notice entitled ‘‘Inmate Central Records System’’ (ICRS) (JUSTICE/BOP–005). This system is being exempted from certain subsections of the Privacy Act of 1974 listed below for the reasons set forth in the following text. DATES: Effective: February 19, 2013. FOR FURTHER INFORMATION CONTACT: Wanda M. Hunt, FOIA/Privacy Act Chief, Federal Bureau of Prisons, 202– 514–6655. SUPPLEMENTARY INFORMATION: On April 26, 2012, at 77 FR 24982, the Department published an updated Privacy Act system of records notice (SORN) for the ICRS, a BOP SORN originally published on August 27, 1975 (40 FR 38704). The proposed SORN amendments reflected overall modernization and technological changes of BOP’s information system, and included updates to system routine uses. On April 26, 2012, at 77 FR 24878, the Department also published a proposed rule to amend 28 CFR 16.97, sroberts on DSK5SPTVN1PROD with RULES SUMMARY: VerDate Mar<15>2010 15:41 Feb 15, 2013 Jkt 229001 which had previously established exemptions of the ICRS from various Privacy Act provisions, as expressly authorized by Privacy Act subsection (j). The proposed rule did not significantly change the previously established ICRS exemptions from Privacy Act subsections (c)(3) and (4); (d)(1), (2), (3), and (4); (e)(1), (2), (3), (4)(H), (5), and (8); (f); and (g). In addition to such exemptions, the proposed rule sought to exempt ICRS from Privacy Act subsections (e)(4)(G) and (I), add exemptions pursuant to Privacy Act subsection (k)(2), and made general editorial revisions to the reasons for the already existing ICRS exemptions. Public comments were invited. Comments on the proposed SORN changes were to be submitted by May 29, 2012 (77 FR 24982); comments on the proposed rule were to be received by the Department’s designated recipient by May 29, 2012 (77 FR 24878). The Department received comments from one member of the public. Although some of the comments received pertain to the applicability of exemptions to this SORN, the comments reference only the Federal Register citation for the proposed SORN modifications and not the proposed rule. Moreover, the comments were not received timely with regard to the proposed rule. Accordingly, the Department has carefully reviewed and analyzed these comments in the context of the SORN, but declines to adopt them and hereby implements the proposed rule without substantive change. The comments received to the SORN address four main issues: (1) The routine use disclosures to the news media and public; (2) the routine use disclosures to health care agencies/ professionals; (3) the inapplicability of 5 U.S.C. 552a(j); and (4) the inapplicability of 5 U.S.C. 552a(k). Responses to the comments are set forth below. First, the commenter objected to the scope and lack of specificity of two new routine uses, namely routine use (r) for disclosures to the news media and the public, and new routine use (t) for disclosures to health care agencies/ professionals. The Department, however, maintains that these routine uses provide appropriate specificity, as each routine use indicates the purpose for permissible disclosures and incorporates a defined standard that further limits disclosures to data relevant to each routine use’s particular purpose. Second, the commenter objected to disclosure of medical information without an individual’s consent. The Department understands the sensitivity PO 00000 Frm 00025 Fmt 4700 Sfmt 4700 11575 of medical information of former/ current inmates, and thus, has instituted safeguards appropriate for this kind of information. The Department considers the health care disclosures encompassed in routine use (t) to be lawful, appropriate, and necessary to meet BOP’s responsibilities for the safekeeping, care, and custody of incarcerated (and formerly incarcerated) persons and for the continued safety and security of federal prisons and the public. The commenter also objected to the applicability of 5 U.S.C. 552a (j) and (k). Subsection (j)(2) of the Privacy Act covers records created and maintained by the BOP. This subsection includes records maintained by any component that performs as its principal function any activity pertaining to the enforcement of criminal laws, including activities of correctional authorities (e.g. BOP). Further specified in subsection (j)(2) are the types of records that may be exempted, which include, for example: information compiled for the purpose of identifying individual criminal offenders and alleged offenders, including the nature and disposition of criminal charges, sentencing, confinement, release, and parole and probation status; and reports identifiable to an individual compiled at any stage of the process of enforcement of the criminal laws from arrest or indictment through release from supervision. Such records comprise the vast majority of records in the ICRS. Any ICRS records that would not be within the scope of subsection (j)(2) might nonetheless come within the scope of subsection (k)(2), and thus, are appropriately subject to the (k)(2)-based exemptions that have now being established by this final rule. Moreover, the sections of the SORN that reflect the exemptions established by the underlying rule must necessarily conform to the exemption provisions finalized by this final rule. Additionally, as suggested by the commenter, the Department proposed, and hereby includes in paragraph 16.97(k) of the final rule, that the exemptions apply only to the extent that information in this system is subject to exemption under these subsections. Finally, the commenter alleged that the Department failed to provide a statement of reasons for the exemptions as required by the Privacy Act. However, the Department detailed the reasons for each exemption in paragraphs 16.97(k)(1)–(12) of both the proposed rule and final rule below. The SORN incorporates this underlying information via the section for ‘‘Exemptions Claimed for the System,’’ E:\FR\FM\19FER1.SGM 19FER1

Agencies

[Federal Register Volume 78, Number 33 (Tuesday, February 19, 2013)]
[Rules and Regulations]
[Pages 11572-11575]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-03407]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0732; Directorate Identifier 2012-CE-022-AD; 
Amendment 39-17311; AD 2012-26-16]
RIN 2120-AA64


Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are superseding an existing airworthiness directive (AD) 
for all Pilatus Aircraft Ltd. Models PC-12, PC-12/45, PC-12/47, and PC-
12/47E airplanes. This AD results from mandatory continuing 
airworthiness information (MCAI) issued by an aviation authority of 
another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as a need to 
incorporate new revisions into the Limitations section, Chapter 4, of 
the FAA-approved maintenance program (e.g., maintenance manual). We are 
issuing this AD to require actions to address the unsafe condition on 
these products.

DATES: This AD is effective March 26, 2013.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in the AD as of March 26, 
2013.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of August 
19, 2009 (74 FR 34213, July 15, 2009).

ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov or in person at 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 service information identified in this AD, contact Pilatus 
Aircraft Ltd., Customer Service Manager, CH-6371 STANS, Switzerland; 
telephone: +41 (0) 41 619 62 08; fax: +41 (0) 41 619 73 11; Internet: 
https://www.pilatus-aircraft.com or email: SupportPC12@pilatus-aircraft.com. You may review copies of the referenced 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.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email: 
doug.rudolph@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a supplemental notice of proposed rulemaking (SNPRM) to 
amend 14 CFR part 39 to include an AD that would apply to the specified 
products. That SNPRM was published in the Federal Register on October 
22, 2012 (77 FR 64442), which proposed to supersede AD 2009-14-13, 
Amendment 39-15963 (74 FR 34213, July 15, 2009).
    Since we issued AD 2009-14-13, Amendment 39-15963 (74 FR 34213, 
July 15, 2009), Pilatus Aircraft Ltd. has issued revisions to the 
Limitations section of the airplane maintenance manual to include an 
inspection of the wing main spar fastener holes at rib 6 for cracks.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued AD 
No. 2012-0099, dated June 8, 2012 (referred to after this as ``the 
MCAI''), to correct an unsafe condition for the specified products. The 
MCAI states:

    The mandatory instructions and airworthiness limitations 
applicable to the Structure and Components of the PC-12 are 
specified in the Aircraft Maintenance Manual (AMM) under Chapter 4. 
Prompted by a crack found on one wing of the aeroplane fleet leader, 
a more restrictive airworthiness limitation was introduced, in that 
manual, for the inspection of the main spar rib 6 strap fastener.
    These documents include the maintenance instructions and/or 
airworthiness limitations developed by Pilatus Aircraft Ltd. and 
approved by EASA. Failure to comply with these instructions and 
limitations could potentially lead to unsafe condition.
    For the reasons described above, this AD requires the 
implementation of more restrictive maintenance instructions and/or 
airworthiness limitations.

    You may obtain further information by examining the MCAI in the AD 
docket.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the SNPRM (77 FR 64442, October 22, 
2012) or on the determination of the cost to the public.

[[Page 11573]]

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting the AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
SNPRM (77 FR 64442, October 22, 2012) for correcting the unsafe 
condition; and
     Do not add any additional burden upon the public than was 
already proposed in the SNPRM (77 FR 64442, October 22, 2012).

Costs of Compliance

    We estimate that this AD will affect 678 products of U.S. registry. 
We also estimate that it will take about 3.5 work-hours per product to 
comply with the basic requirements of this AD. The average labor rate 
is $85 per work-hour. Required parts will cost about $300 per product. 
Based on these figures, we estimate the cost of this AD on U.S. 
operators to be $405,105, or $597.50 per product.
    In addition, we estimate that any necessary corrective actions that 
must be taken based on incorporating the new revisions into the 
limitation section of the maintenance manual will take about 6 work-
hours and require parts costing approximately $4,000, for a cost of 
$4,510 per product. We have no way of determining the number of 
products that may need these necessary corrective actions.
    We estimate that it will take about 12 work-hours per product to 
comply with the new addition of the wing main spar fastener holes 
inspection requirement of this AD. The average labor rate is $85 per 
work-hour. Based on these figures, we estimate the cost of the wing 
main spar fastener holes on U.S. operators to be $691,560, or $1,020 
per product.
    In addition, we estimate that any necessary repairs to the wing 
main spar will take about 7 work-hours and require parts costing 
approximately $5,000, for a cost of $5,595 per product. We have no way 
of determining the number of products that may need these corrective 
actions.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. ``Subtitle VII: Aviation 
Programs,'' describes in more detail the scope of the Agency's 
authority.
    We are issuing this rulemaking under the authority described in 
``Subtitle VII, Part A, Subpart III, Section 44701: General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We determined that this AD will not have federalism implications 
under Executive Order 13132. This AD will not have a substantial direct 
effect on the States, on the relationship between the national 
government and the States, or on the distribution of power and 
responsibilities among the various levels of government.
    For the reasons discussed above, I certify this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

Examining the AD Docket

    You may examine the AD docket on the Internet at https://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 the SNPRM (77 FR 64442, October 22, 
2012), the regulatory evaluation, any comments received, and other 
information. The street address for the Docket Office (telephone (800) 
647-5527) is in the ADDRESSES section. Comments will be available in 
the AD docket shortly after receipt.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Amendment 39-15963 (74 FR 
34213, July 15, 2009), and adding the following new AD:

2012-26-16 Pilatus Aircraft Ltd.: Amendment 39-17311; Docket No. 
FAA-2012-1052; Directorate Identifier 2012-CE-014-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective March 26, 
2013.

(b) Affected ADs

    This AD supersedes AD 2009-14-13, Amendment 39-15963 (74 FR 
34213, July 15, 2009).

(c) Applicability

    This AD applies to Pilatus Aircraft Ltd. Models PC-12, PC-12/45, 
PC-12/47, and PC-12/47E airplanes, all manufacturer serial numbers 
(MSNs), certificated in any category.

(d) Subject

    Air Transport Association of America (ATA) Code 05: Time Limits.

(e) Reason

    This AD was prompted by mandatory continuing airworthiness 
information (MCAI) originated by an aviation authority of another 
country to identify and correct an unsafe condition on an aviation 
product. The MCAI describes the unsafe condition as a need to 
incorporate new revisions into the Limitations section, Chapter 4, 
of the FAA-approved maintenance program (e.g., maintenance manual). 
The limitations were revised to include an inspection of the wing 
main spar fastener holes at rib 6 for cracks. These actions are 
required to ensure the continued operational safety of the affected 
airplanes.

(f) Actions and Compliance

    Unless already done, do the following actions:
    (1) For Models PC-12 and PC-12/45 airplanes, MSNs 101 through 
299: Within the next 100 hours time-in-service (TIS) after August 
19, 2009 (the effective date retained from AD 2009-14-13, Amendment 
39-15963 (74 FR 34213, July 15, 2009)) or 1 year after August 19, 
2009 (the effective date retained from AD 2009-14-13), whichever 
occurs first, replace the torque tube part number (P/N) 
532.50.12.047 with torque tube P/N 532.50.12.064 following PILATUS 
AIRCRAFT LTD. Service Bulletin No: 32-021, dated November 21, 2008.
    (2) For all airplanes: As of March 26, 2013 (the effective date 
of this AD), do not install torque tube P/N 532.50.12.047.
    (3) For all airplanes: Before further flight after March 26, 
2013 (the effective date of

[[Page 11574]]

this AD), insert Data module code 12-A-04-00-00-00A-000A-A, 
``STRUCTURAL, COMPONENT AND MISCELLANEOUS--AIRWORTHINESS 
LIMITATIONS,'' dated October 15, 2012, of the Pilatus Model 
Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, PC 
12/47 AMM Document No. 02049, 12-A-AM-00-00-00-I, revision 26, dated 
December 15, 2012, for Models PC-12, PC-12/45, PC-12/47, and Data 
module code 12-B-04-00-00-00A-000A-A, ``STRUCTURAL AND COMPONENT 
LIMITATIONS--AIRWORTHINESS LIMITATIONS,'' dated October 15, 2012, of 
the Pilatus Model Identification: 12 Aircraft Maintenance Manual, PC 
12/47E AMM Document No. 02300, 12-B-AM-00-00-00-I, revision 9, dated 
December 15, 2012, for Model PC-12/47E, into the Limitations section 
of the FAA-approved maintenance program (e.g., maintenance manual). 
These limitations section revisions do the following:
    (i) Establish an inspection of the wing main spar fastener holes 
at rib 6,
    (ii) Specify replacement of components before or upon reaching 
the applicable life limit, and
    (iii) Specify accomplishment of all applicable maintenance tasks 
within certain thresholds and intervals.
    (4) For all airplanes: If no compliance time is specified in the 
documents listed in paragraph (f)(3) of this AD when doing any 
corrective actions where discrepancies are found as required in 
paragraph (f)(3)(iii) of this AD, do these corrective actions before 
further flight after doing the applicable maintenance task.
    (5) For all airplanes: During the accomplishment of the actions 
required in paragraphs (f)(3)(i), (f)(3)(ii), and (f)(3)(iii) of 
this AD, if a discrepancy is found that is not identified in the 
documents listed in paragraph (f)(3) of this AD, before further 
flight after finding the discrepancy, contact Pilatus Aircraft Ltd. 
at the address specified in paragraph (i)(5) of this AD for a repair 
scheme and incorporate that repair scheme.

(g) Credit for Actions Accomplished in Accordance With Previous Service 
Information

    This paragraph provides credit for the actions required in 
paragraph (f)(3) of this AD if already done before March 6, 2013 
(the effective date of this AD) following Pilatus PC12 Aircraft 
Maintenance Manual Temporary Revision No. 04-03, dated October 15, 
2012, which transmits Unclassified 12-A/AMP-04 ``STRUCTURAL, 
COMPONENT AND MISCELLANEOUS--AIRWORTHINESS LIMITATIONS,'' document 
12-A-04-00-00-00A-000A-A, dated October 15, 2012; and Pilatus PC12/
47E Aircraft Maintenance Manual Temporary Revision No. 04-01, dated 
October 15, 2012, which transmits Unclassified 12-B/AMP-04 
``STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS LIMITATIONS,'' 
document 12-B-04-00-00-00A-000A-A, dated October 15, 2012.

(h) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Doug Rudolph, Aerospace Engineer, FAA, Small 
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email: 
doug.rudolph@faa.gov.
    (i) Before using any approved AMOC on any airplane to which the 
AMOC applies, notify your appropriate principal inspector (PI) in 
the FAA Flight Standards District Office (FSDO), or lacking a PI, 
your local FSDO.
    (ii) AMOCs approved for AD 2009-14-13, Amendment 39-15963 (74 FR 
34213, July 15, 2009) are not approved as AMOCs for this AD.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in 
this AD, a federal agency may not conduct or sponsor, and a person 
is not required to respond to, nor shall a person be subject to a 
penalty for failure to comply with a collection of information 
subject to the requirements of the Paperwork Reduction Act unless 
that collection of information displays a current valid OMB Control 
Number. The OMB Control Number for this information collection is 
2120-0056. Public reporting for this collection of information is 
estimated to be approximately 5 minutes per response, including the 
time for reviewing instructions, completing and reviewing the 
collection of information. All responses to this collection of 
information are mandatory. Comments concerning the accuracy of this 
burden and suggestions for reducing the burden should be directed to 
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: 
Information Collection Clearance Officer, AES-200.

(i) Related Information

    Refer to MCAI European Aviation Safety Agency (EASA) AD No. 
2012-0099, dated June 8, 2012; Pilatus Aircraft Ltd. Service 
Bulletin No: 32-021, dated November 21, 2008; Data module code 12-A-
04-00-00-00A-000A-A, ``STRUCTURAL, COMPONENT AND MISCELLANEOUS--
AIRWORTHINESS LIMITATIONS,'' dated October 15, 2012, of the Pilatus 
Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, 
PC 12/47 AMM Document No. 02049, 12-A-AM-00-00-00-I, revision 26, 
dated December 15, 2012; Data module code 12-B-04-00-00-00A-000A-A, 
``STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS LIMITATIONS,'' 
dated October 15, 2012, of the Pilatus Model Identification: 12 
Aircraft Maintenance Manual, PC 12/47E AMM Document No. 02300, 12-B-
AM-00-00-00-I, revision 9, dated December 15, 2012; Pilatus PC12 
Aircraft Maintenance Manual Temporary Revision No. 04-03, dated 
October 15, 2012, which transmits Unclassified 12-A/AMP-04 
``STRUCTURAL, COMPONENT AND MISCELLANEOUS--AIRWORTHINESS 
LIMITATIONS,'' document 12-A-04-00-00-00A-000A-A, dated October 15, 
2012; and PC12/47E Aircraft Maintenance Manual Temporary Revision 
No. 04-01, dated October 15, 2012, which transmits Unclassified 12-
B/AMP-04 ``STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS 
LIMITATIONS,'' document 12-B-04-00-00-00A-000A-A, dated October 15, 
2012, for related information.

(i) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (3) The following service information was approved for IBR on 
March 26, 2013.
    (i) Data module code 12-A-04-00-00-00A-000A-A, ``STRUCTURAL, 
COMPONENT AND MISCELLANEOUS--AIRWORTHINESS LIMITATIONS,'' dated 
October 15, 2012, of the Pilatus Model Identification: 12 Aircraft 
Maintenance Manual, PC12, PC12/45, PC 12/47 AMM Document No. 02049, 
12-A-AM-00-00-00-I, revision 26, dated December 15, 2012.
    (ii) Data module code 12-B-04-00-00-00A-000A-A, ``STRUCTURAL AND 
COMPONENT LIMITATIONS--AIRWORTHINESS LIMITATIONS,'' dated October 
15, 2012, of the Pilatus Model Identification: 12 Aircraft 
Maintenance Manual, PC 12/47E AMM Document No. 02300, 12-B-AM-00-00-
00-I, revision 9, dated December 15, 2012.
    Note to paragraph (i)(3) of this AD: Data module code 12-A-04-
00-00-00A-000A-A, ``STRUCTURAL, COMPONENT AND MISCELLANEOUS--
AIRWORTHINESS LIMITATIONS,'' dated October 15, 2012, of the Pilatus 
Model Identification: 12 Aircraft Maintenance Manual, PC12, PC12/45, 
PC 12/47 AMM Document No. 02049, 12-A-AM-00-00-00-I, revision 26, 
dated December 15, 2012; and Data module code 12-B-04-00-00-00A-
000A-A, ``STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS 
LIMITATIONS,'' dated October 15, 2012, of the Pilatus Model 
Identification: 12 Aircraft Maintenance Manual, PC 12/47E AMM 
Document No. 02300, 12-B-AM-00-00-00-I, revision 9, dated December 
15, 2012, were issued as complete updates to the AMM Airworthiness 
Limitations sections and incorporate all technical information 
contained in Pilatus AMM Temporary Revision No. 04-01 and Pilatus 
AMM Temporary Revision No. 04-03, both dated October 15, 2012.
    (4) The following service information was approved for IBR on 
August 19, 2009 (74 FR 34213, July 15, 2009).
    (i) Pilatus Aircraft Ltd. Service Bulletin No: 32-021, dated 
November 21, 2008.
    (ii) Reserved.

[[Page 11575]]

    (5) For Pilatus Aircraft Ltd. service information identified in 
this AD, contact Pilatus Aircraft Ltd., Customer Service Manager, 
CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 62 08; fax: 
+41 (0) 41 619 73 11; Internet: https://www.pilatus-aircraft.com or 
email: SupportPC12@pilatus-aircraft.com.
    (6) You may view this 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.
    (7) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/.

    Issued in Kansas City, Missouri, on February 8, 2013.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2013-03407 Filed 2-15-13; 8:45 am]
BILLING CODE 4910-13-P
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