51456 Federal Register / Vol. 80, No. 164 / Tuesday, August 25, 2015 / Rules and Regulations (e) Required Actions (j) Material Incorporated by Reference another country to identify and correct (1) Within 165 hours time-in-service (TIS), (1) The Director of the Federal Register an unsafe condition on an aviation visually inspect the swashplate assembly to approved the incorporation by reference of product. The MCAI describes the unsafe determine whether a ferrule is installed on the service information listed in this condition as cracks found on the main the rotating star. If the ferrule is not visible, paragraph under 5 U.S.C. 552(a) and 1 CFR landing gear cylinders. We are issuing use a magnetic retriever positioned in Area part 51. this AD to require actions to address the (X) as shown in the pictures under paragraph (2) You must use this service information unsafe condition on these products. 3.B.2.b., Accomplishment Instructions, of as applicable to do the actions required by Airbus Helicopters Alert Service Bulletin this AD, unless the AD specifies otherwise. DATES: This AD is effective September (ASB) No. EC130 62A010, ASB No. AS350 (i) Airbus Helicopters Alert Service 29, 2015. 62.00.34, or ASB No. AS355 62.00.33, all Bulletin (ASB) No. EC130 62A010, Revision The Director of the Federal Register Revision 0, and all dated April 28, 2014, 0, dated April 28, 2014. approved the incorporation by reference whichever is applicable to your helicopter, to (ii) Airbus Helicopters ASB No. AS350 of a certain publication listed in this AD determine whether the ferrule is installed. 62.00.34, Revision 0, dated April 28, 2014. as of September 29, 2015. The magnetic retriever will be magnetized if (iii) Airbus Helicopters ASB No. AS355 The Director of the Federal Register a ferrule is installed. 62.00.33, Revision 0, dated April 28, 2014. approved the incorporation by reference (3) For Airbus Helicopters service (2) If a ferrule is not installed, no further of a certain other publication listed in action is needed. information identified in this AD, contact (3) If a ferrule is installed on the rotating Airbus Helicopters, Inc., 2701 N. Forum this AD as of March 23, 2007 (72 FR star, before further flight, dye-penetrant Drive, Grand Prairie, TX 75052; telephone 7576, February 16, 2007). inspect the rotating star for a crack in areas (972) 641–0000 or (800) 232–0323; fax (972) ADDRESSES: You may examine the AD ‘‘Z’’ depicted in Figure 1 of Airbus 641–3775; or at http:// docket on the Internet at http:// Helicopters ASB No. EC130 62A010, ASB www.airbushelicopters.com/techpub. www.regulations.gov by searching for No. AS350 62.00.34, or ASB No. AS355 (4) You may view this service information and locating Docket No. FAA–2015– 62.00.33, all Revision 0, and all dated April at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., 2047; or in person at the Docket 28, 2014, as applicable to your model Management Facility, U.S. Department helicopter. Room 6N–321, Fort Worth, Texas 76177. For (i) If the rotating star has a crack, before information on the availability of this of Transportation, Docket Operations, further flight, remove from service the material at the FAA, call (817) 222–5110. M–30, West Building Ground Floor, rotating star; ferrule; and the screws, washers (5) You may view this service information Room W12–140, 1200 New Jersey and nuts used to attach the pitch change that is incorporated by reference at the Avenue SE., Washington, DC 20590. rods, compass, and the rotating star deflector. National Archives and Records For service information identified in (ii) If the rotating star does not have a Administration (NARA). For information on this AD, contact SOCATA, Direction des crack, within 160 hours TIS, remove from the availability of this material at NARA, call Services, 65921 Tarbes Cedex 9, France; service the rotating star; ferrule; and the (202) 741–6030, or go to: http:// telephone: 33 (0)5 62.41.73.00; fax: 33 screws, washers and nuts used to attach the www.archives.gov/federal-register/cfr/ibr- locations.html. (0)5 62.41.76.54; or SOCATA North pitch change rods, compass, and the rotating America, North Perry Airport, 7501 S star deflector. Issued in Fort Worth, Texas, on August 13, (4) Do not install a rotating star P/N Airport Rd., Pembroke Pines, Florida 2015. 33023, telephone: (954) 893–1400; fax: 350A371003–04, 350A371003–05, Lance T. Gant, 350A371003–06, 350A371003–07, or (954) 964–4141; Internet: http:// 350A371003–08 with a ferrule. Acting Directorate Manager, Rotorcraft www.socata.com. You may view this Directorate, Aircraft Certification Service. referenced service information at the (f) Special Flight Permits [FR Doc. 2015–20587 Filed 8–24–15; 8:45 am] FAA, Small Airplane Directorate, 901 Special flight permits are prohibited. BILLING CODE 4910–13–P Locust, Kansas City, Missouri 64106. (g) Alternative Methods of Compliance For information on the availability of (AMOCs) this material at the FAA, call (816) 329– DEPARTMENT OF TRANSPORTATION (1) The Manager, Safety Management 4148. It is also available on the Internet Group, FAA, may approve AMOCs for this Federal Aviation Administration at http://www.regulations.gov by AD. Send your proposal to: Robert Grant, searching for Docket No. FAA–2015– Aviation Safety Engineer, Safety Management 2047. Group, FAA, 10101 Hillwood Pkwy., Fort 14 CFR Part 39 Worth, Texas 76177; telephone (817) 222– FOR FURTHER INFORMATION CONTACT: [Docket No. FAA–2015–2047; Directorate Albert J. Mercado, Aerospace Engineer, 5110; email [email protected]. Identifier 2015–CE–013–AD; Amendment (2) For operations conducted under a 14 39–18243; AD 2015–17–10] FAA, Small Airplane Directorate, 901 CFR part 119 operating certificate or under Locust, Room 301, Kansas City, 14 CFR part 91, subpart K, we suggest that RIN 2120–AA64 Missouri 64106; telephone: (816) 329– you notify your principal inspector, or 4119; fax: (816) 329–4090; email: lacking a principal inspector, the manager of Airworthiness Directives; SOCATA [email protected]. the local flight standards district office or Airplanes SUPPLEMENTARY INFORMATION: certificate holding district office, before AGENCY: operating any aircraft complying with this Federal Aviation Discussion AD through an AMOC. Administration (FAA), Department of Transportation (DOT). We issued a supplemental notice of (h) Additional Information ACTION: Final rule. proposed rulemaking (SNPRM) to make The subject of this AD is addressed in the changes to an NPRM (80 FR 8821, European Aviation Safety Agency (EASA) AD SUMMARY: We are superseding February 19, 2015), which would amend No. 2014–0132R1, dated June 2, 2014. You Airworthiness Directive (AD) 2007–04– 14 CFR part 39 to add an AD that would may view the EASA AD on the Internet at 13 for certain SOCATA Model TBM 700 apply to certain SOCATA Model TBM http://www.regulations.gov in Docket No. airplaness (type certificate previously 700 airplaness (type certificate FAA–2015–0673. held by EADS SOCATA). This AD previously held by EADS SOCATA). (i) Subject results from mandatory continuing That SNPRM was published in the Joint Aircraft Service Component (JASC) airworthiness information (MCAI) Federal Register on June 11, 2015 (80 Code: 6200, Main Rotor System. issued by an aviation authority of FR 33208), and proposed to supersede VerDate Sep<11>2014 15:04 Aug 24, 2015 Jkt 235001 PO 00000 Frm 00034 Fmt 4700 Sfmt 4700 E:\FR\FM\25AUR1.SGM 25AUR1 Lhorne on DSK5TPTVN1PROD with RULES Federal Register / Vol. 80, No. 164 / Tuesday, August 25, 2015 / Rules and Regulations 51457 AD 2007–04–13, Amendment 39–14945, Comments Authority for This Rulemaking (72 FR 7576, February 16, 2007) (‘‘AD Title 49 of the United States Code 2007–04–13’’). We gave the public the opportunity to Since we issued AD 2007–04–13, it participate in developing this AD. We specifies the FAA’s authority to issue has been determined that the time received one supportive comment to the rules on aviation safety. Subtitle I, between repetitive inspections should NPRM (80 FR 8821, February 19, 2015) section 106, describes the authority of be extended and an optional terminating and no comments on the SNPRM (80 FR the FAA Administrator. ‘‘Subtitle VII: action for the repetitive inspections is 33208, June 11, 2015) or on the Aviation Programs,’’ describes in more now available. determination of the cost to the public. detail the scope of the Agency’s authority. The European Aviation Safety Agency Conclusion (EASA), which is the Technical Agent We are issuing this rulemaking under for the Member States of the European We reviewed the relevant data and the authority described in ‘‘Subtitle VII, Community, has issued AD No. 2006– determined that air safety and the Part A, Subpart III, section 44701: 0085R2, dated January 16, 2015 public interest require adopting the AD General requirements.’’ Under that (referred to after this as ‘‘the MCAI’’), to as proposed except for minor editorial section, Congress charges the FAA with correct an unsafe condition for the changes. We have determined that these promoting safe flight of civil aircraft in specified products. The MCAI states: minor changes: air commerce by prescribing regulations • Are consistent with the intent that for practices, methods, and procedures Cracks on several main landing gear (MLG) the Administrator finds necessary for cylinders have been reported in service. was proposed in the SNPRM (80 FR This condition, if not to detected and 33208, June 11, 2015) for correcting the safety in air commerce. This regulation corrected, could lead to fatigue cracks in the unsafe condition; and is within the scope of that authority shock strut cylinder of the MLG, which could • Do not add any additional burden because it addresses an unsafe condition result in a collapsed MLG during take-off or upon the public than was already that is likely to exist or develop on landing runs, and possibly reduce the proposed in the SNPRM (80 FR 33208, products identified in this rulemaking structural integrity of the aeroplane.