Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes, 52841-52847 [2013-20731]

Download as PDF Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations Requirements (CMRs), D626A001–CMR, Revision August 2012, of the Boeing 737– 600/700/700C/800/900/900ER MPD Document. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H–65, Seattle, WA 98124–2207; telephone 206– 544–5000, extension 1; fax 206–766–5680; Internet https://www.myboeingfleet.com. (4) You may review copies of the referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. 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: http:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on July 21, 2013. Stephen P. Boyd, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2013–20730 Filed 8–26–13; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2012–1078; Directorate Identifier 2011–NM–012–AD; Amendment 39–17534; AD 2013–15–18] RIN 2120–AA64 Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: We are superseding an airworthiness directive (AD) for all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L– 1011 series airplanes. AD 2005–15–01 required repetitive inspections to detect corrosion or fatigue cracking of certain structural elements of the airplane, corrective actions if necessary, and incorporation of certain structural modifications. This new AD reduces certain compliance times for the initial inspection and the repetitive inspection interval for certain airplanes. This AD was prompted by reports of small cracks in additional areas outside those addressed in AD 2005–15–01, prior to the inspection threshold required by the AD 2005–15–01. We are issuing this AD pmangrum on DSK3VPTVN1PROD with RULES SUMMARY: VerDate Mar<15>2010 13:33 Aug 26, 2013 Jkt 229001 52841 to prevent corrosion or fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane. DATES: This AD is effective October 1, 2013. The Director of the Federal Register approved the incorporation by reference of certain publications listed in the AD as of October 1, 2013. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of August 26, 2005 (70 FR 42262, July 22, 2005). ADDRESSES: For service information identified in this AD, contact Lockheed Martin Corporation/Lockheed Martin Aeronautics Company, L–1011 Technical Support Center, Dept. 6A4M, Zone 0579, 86 South Cobb Drive, Marietta, GA 30063–0579; telephone 770–494–5444; fax 770–494–5445; email L1011.support@lmco.com; Internet http://www.lockheedmartin.com/ams/ tools/TechPubs.html. You may review copies of the referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call 425–227–1221. NPRM proposed to continue to require repetitive inspections to detect corrosion or fatigue cracking of certain structural elements of the airplane, corrective actions if necessary, and incorporation of certain structural modifications. The NPRM also proposed to require reducing certain compliance times for the initial inspection and the repetitive inspection interval for certain airplanes. Examining the AD Docket 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: Carl Gray, Aerospace Engineer, Airframe Branch, ACE–117A, FAA, Atlanta Aircraft Certification Office (ACO), 1701 Columbia Avenue, College Park, Georgia 30337; phone: 404–474–5554; fax: 404– 474–5605; email: carl.w.gray@faa.gov. SUPPLEMENTARY INFORMATION: Additional Change Made to This AD Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005). AD 2005–15–01 applied to the specified products. The NPRM published in the Federal Register on October 16, 2012 (77 FR 63275). The PO 00000 Frm 00015 Fmt 4700 Sfmt 4700 Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the proposal (77 FR 63275, October 16, 2012) and the FAA’s response to each comment. Request To Update Certain Address Information Lockheed Martin Corporation/ Lockheed Martin Aeronautics Company requested that we revise the NPRM (77 FR 63275, October 16, 2012) to update its address information. We agree to update the address information in this final rule. We have included this updated information in the ADDRESSES section and paragraph (n)(5) of this AD. We have revised paragraph (g)(10) of this AD (in table 1 to paragraph (g) of this AD) to include paragraph identifiers for paragraphs (g)(10)(i) and (g)(10)(ii) of this AD. This change is for formatting purposes only. Conclusion We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting this AD with the change described previously— and minor editorial changes. We have determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM (77 FR 63275, October 16, 2012) for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM (77 FR 63275, October 16, 2012). We also determined that these changes will not increase the economic burden on any operator or increase the scope of the AD. Costs of Compliance We estimate that this AD affects 26 airplanes of U.S. registry. We estimate the following costs to comply with this AD: E:\FR\FM\27AUR1.SGM 27AUR1 52842 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations ESTIMATED COSTS Action Labor cost Inspections [retained actions from AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)]. Modification [retained action from AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)]. 129 work-hours × $85 per hour = $10,965 per inspection cycle. pmangrum on DSK3VPTVN1PROD 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, 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 have 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 that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and 13:33 Aug 26, 2013 Jkt 229001 Cost per product $0 614 work-hours × $85 per hour = $52,190. We have received no definitive data that would enable us to provide cost estimates for the retained on-condition actions specified in this AD. VerDate Mar<15>2010 Parts cost $142,275 Cost on U.S. operators $10,965 per inspection cycle. $285,090 per inspection cycle. $194,465 ................................ $5,056,090. (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. (d) Subject List of Subjects in 14 CFR Part 39 (e) Unsafe Condition Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. This AD was prompted by reports of small cracks in additional areas outside those addressed in AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005), prior to the inspection threshold required by AD 2005–15–01. We are issuing this AD to prevent corrosion or fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: (f) Compliance 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 airworthiness directive (AD) 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005), and adding the following new AD: ■ 2013–15–18 Lockheed Martin Corporation/ Lockheed Martin Aeronautics Company: Amendment 39–17534; Docket No. FAA–2012–1078; Directorate Identifier 2011–NM–012–AD. (a) Effective Date This AD is effective October 1, 2013. (b) Affected ADs This AD supersedes AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005). (c) Applicability This AD applies to all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L–1011–385–1, L–1011– 385–1–14, L–1011–385–1–15, and L–1011– 385–3 airplanes, certificated in any category. PO 00000 Frm 00016 Fmt 4700 Sfmt 4700 Joint Aircraft System Component (JASC)/ Air Transport Association (ATA) of America Code 51, Standard practices/structures; 52, Doors; 53, Fuselage; 57, Wings. Comply with this AD within the compliance times specified, unless already done. (g) Retained Inspections With Revised Service Information and Reduced Compliance Times This paragraph restates the inspections required by paragraph (a) of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005), with revised service information and reduced compliance times for paragraph (g)(16) of this AD. At the time specified in the ‘‘Initial Compliance Time’’ column of table 1 to paragraph (g) of this AD, perform structural inspections to detect corrosion or fatigue cracking of certain structural elements of the airplane, in accordance with the applicable service bulletins listed under ‘‘Service Bulletin Number, Revision, and Date’’ in tables I and II of Lockheed Tristar L–1011 Service Bulletin 093–51–041, Revision 1, dated March 3, 2000; or Revision 2, dated March 30, 2010 (The applicable service bulletins are also identified in Table 1 to paragraph (g) of this AD.) As of the effective date of this AD, only Lockheed Tristar L–1011 Service Bulletin 093–51–041, Revision 2, dated March 30, 2010, may be used for the actions required by this paragraph. Thereafter, repeat the inspections at intervals specified in the ‘‘Repetitive Intervals’’ column of table 1 to paragraph (g) of this AD. E:\FR\FM\27AUR1.SGM 27AUR1 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations 52843 TABLE 1 TO PARAGRAPH (g) OF THIS AD Lockheed TriStar L–1011 Service Bulletin Initial compliance time (whichever occurs later between the times in ‘‘Inspection Threshold’’ and ‘‘Grace Period’’) Inspection threshold Before the accumulation of 8,000 total flight cycles or 15,000 total flight hours, whichever occurs first. (2) 093–53–274, dated May 28, 1997. Within 14 months after August 26, 2005 (the effective date of AD 2005– 15–01, Amendment 39– 14190 (70 FR 42262, July 22, 2005)). Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. At the next Corrosion Prevention and Control Program (CPCP) inspection after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)). Before the accumulation of 26,000 total flight cycles or 48,000 total flight hours, whichever occurs first. Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. (None) ............................... (3) 093–53–275, dated December 10, 1996. (4) 093–53–276, dated June 17, 1996. (5) 093–57–085, Revision 1, dated December 1, 1997. (6) 093–57–208, Revision 1, dated October 28, 1997. pmangrum on DSK3VPTVN1PROD with RULES Terminating action Grace period (1) 093–53–269, Revision 1, dated October 28, 1997. Repetitive intervals Before the accumulation of 18,000 total flight cycles. (7) 093–52–210, dated July 19, 1991, including Lockheed LCC–7622– 248, Corrosion Removal and Refurbishment of C1–A Cargo Door Cam Latches, Latch Bellcranks and Matched Latch Support Assemblies, dated February 27, 1990. (8) 093–53–054, Revision 1, dated August 12, 1975. Within 5,000 flight hours or 18 months after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. VerDate Mar<15>2010 Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. 13:33 Aug 26, 2013 Jkt 229001 PO 00000 At intervals not to exceed 6,450 flight cycles or 5 years, whichever occurs first. (None). At intervals not to exceed 14 months. (None). (None) ............................... (None) ............................... (None). (None) ............................... At intervals not to exceed the next CPCP inspection. (None). Within 1,800 flight cycles or 3,300 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. (None) ............................... At intervals not to exceed 1,800 flight cycles or 3,300 flight hours, whichever occurs first. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–57–085, Basic Issue, dated May 7, 1993; or Revision 1, dated December 1, 1997. (None). (None) ............................... (None). (None) ............................... (None) ............................... (None). Frm 00017 Fmt 4700 Sfmt 4700 At intervals not to exceed 6,450 flight cycles or 5 years, whichever occurs first. E:\FR\FM\27AUR1.SGM 27AUR1 52844 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations TABLE 1 TO PARAGRAPH (g) OF THIS AD—Continued Lockheed TriStar L–1011 Service Bulletin Initial compliance time (whichever occurs later between the times in ‘‘Inspection Threshold’’ and ‘‘Grace Period’’) Repetitive intervals Terminating action Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–070, Basic Issue, dated September 26, 1974; Revision 1, dated January 23, 1975; Revision 2, dated July 7, 1975; or Revision 3, dated September 19, 1989. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–085, Basic Issue, dated September 29, 1975; Revision 1, dated September 3, 1976; or Revision 2, dated February 8, 1988. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–085, Basic Issue, dated September 29, 1975; Revision 1, dated September 3, 1976; or Revision 2, dated February 8, 1988. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–086, Basic Issue, dated September 26, 1975; Revision 1, dated November 12, 1975; Revision 2, dated December 12, 1976; Revision 3, dated July 19, 1977; Revision 4, dated July 8, 1985; or Revision 5, dated April 12, 1990. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–110, Basic Issue, dated August 19, 1991; or Revision 1, dated May 7, 1993. Inspection threshold Grace period (9) 093–53–070, Revision 3, dated September 19, 1989. Before the accumulation of 6,000 total flight hours. Within 1,500 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)). At intervals not to exceed 3,000 flight hours. (10) 093–53–085, Revision 3, dated December 15, 1989. (i) Part I: Before the accumulation of 20,000 flight cycles or 37,000 total flight hours, whichever occurs first. Part I: Within 1,600 flight cycles or 3,000 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Part II: Within 5,000 flight cycles or 9,200 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Within 1,600 flight cycles or 3,000 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Part I: At intervals not to exceed 1,600 flight cycles or 3,000 flight hours, whichever occurs first. (ii) Part II: Before the accumulation of 30,000 flight cycles or 55,000 total flight hours, whichever occurs first. Before the accumulation of 9,000 flight cycles or 10,000 flight hours, whichever occurs first. (12) 093–53–110, Revision 1, dated May 7, 1993. Before the accumulation of 22,000 total flight cycles or 40,000 total flight hours, whichever occurs first. (13) Change Notification 093–53–260, CN4, dated May 8, 1998. pmangrum on DSK3VPTVN1PROD with RULES (11) 093–53–086, Revision 5, dated April 12, 1990. Before the accumulation of 8,000 total flight cycles or 20,000 total flight hours, whichever occurs first. (14) Change Notification 093–53–266, CN1, dated July 10, 1992. Within 12 months after August 26, 2005 (the effective date of AD 2005– 15–01, Amendment 39– 14190 (70 FR 42262, July 22, 2005)). VerDate Mar<15>2010 13:33 Aug 26, 2013 Jkt 229001 PO 00000 Within 2,200 flight cycles or 4,000 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Within 800 flight cycles or 1,500 flight hours after August 26, 2005 (the effective date of AD 2005– 15–01, Amendment 39– 14190 (70 FR 42262, July 22, 2005)), whichever occurs first. (None) ............................... Frm 00018 Fmt 4700 Sfmt 4700 Part II: At intervals not to exceed 5,000 flight cycles or 9,200 flight hours, whichever occurs first. At intervals not to exceed 1,600 flight cycles or 3,000 flight hours, whichever occurs first. At intervals not to exceed 2,200 flight cycles or 4,000 flight hours, whichever occurs first. At intervals not to exceed 800 flight cycles or 1,500 flight hours, whichever occurs first. Inspection and modification in accordance with Part 2.A. of Lockheed TriStar L–1011 Service Bulletin 093–53–260, Basic Issue, dated May 15, 1991. At intervals not to exceed 90 days. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–53–266, Basic Issue, dated March 2, 1992. E:\FR\FM\27AUR1.SGM 27AUR1 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations 52845 TABLE 1 TO PARAGRAPH (g) OF THIS AD—Continued Lockheed TriStar L–1011 Service Bulletin Initial compliance time (whichever occurs later between the times in ‘‘Inspection Threshold’’ and ‘‘Grace Period’’) Repetitive intervals Terminating action Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–57–058, Basic Issue, dated September 16, 1975; Revision 1, dated December 1, 1976; Revision 2, dated June 30, 1978; Revision 3, dated October 19, 1978; Revision 4, dated July 6, 1981; or Revision 5, dated June 9, 1983. Modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–57–195, Revision 2, dated July 27, 1990; Revision 3, dated June 30, 1992; or Revision 4, dated March 17, 2010. Repair or modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–57– 213, Basic Issue, dated December 9, 1994. Inspection threshold Grace period (15) Change Notification 093–57–058, R5–CN1, dated May 3, 1993. Before the accumulation of 20,000 total flight cycles or 37,000 total flight hours, whichever occurs first. Within 1,600 flight cycles or 3,000 flight hours after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. At intervals not to exceed 1,600 flight cycles or 3,000 flight hours, whichever occurs first. (16) Change Notification 093–57–195, R3–CN1, dated August 22, 1995; or Lockheed TriStar L– 1011 Service Bulletin 093–57–195, Revision 4, dated March 17, 2010. At the applicable time specified in paragraph (j) of this AD. At the applicable time specified in paragraph (j) of this AD. At the applicable time specified in paragraph (k) of this AD. (17) Change Notification 093–57–213, CN1, dated February 20, 1996. (i) For Model L–1011– 385–1, L–1011–385–1– 14, L–1011–385–1–15: Before the accumulation of 15,000 total flight cycles. Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. Within 6,450 flight cycles or 5 years after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs first. At intervals not to exceed 6,450 flight cycles or 5 years, whichever occurs first. (ii) For Model L–1011– 385–3: Before the accumulation of 10,000 total flight cycles. At intervals not to exceed 6,450 flight cycles or 5 years, whichever occurs first. pmangrum on DSK3VPTVN1PROD with RULES (h) Retained Corrective Action With a Certain Compliance Method Removed and Revised Service Information Certification Office (ACO), FAA. Information on additional methods of compliance can be obtained from the Manager, Atlanta ACO. This paragraph restates the corrective action required by paragraph (b) of AD 2005– 15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005), with a certain compliance method removed and revised service information. If any cracking or corrosion is detected during any inspection required by paragraph (g) of this AD, prior to further flight, accomplish the actions specified in paragraph (h)(1), (h)(2), or (h)(3) of this AD. (1) Repair in accordance with the applicable service bulletin referenced in table I or II of Lockheed Tristar L–1011 Service Bulletin 093–51–041, Revision 1, dated March 3, 2000; or Revision 2, dated March 30, 2010. (2) Accomplish the terminating modification in accordance with the applicable service bulletin referenced in table I or II of Lockheed Tristar L–1011 Service Bulletin 093–51–041, Revision 1, dated March 3, 2000; or Revision 2, dated March 30, 2010. (3) Repair in accordance with a method approved by the Manager, Atlanta Aircraft (i) Retained Terminating Action VerDate Mar<15>2010 13:33 Aug 26, 2013 Jkt 229001 This paragraph restates the terminating action required by paragraph (c) of AD 2005– 15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005). Within 5 years or 5,000 flight cycles after August 26, 2005 (the effective date of AD 2005–15–01), whichever occurs first, install the terminating modification referenced in the applicable service bulletin listed in table 1 to paragraph (g) of this AD, in accordance with the applicable service bulletin listed in table 1 to paragraph (g) of this AD. Such installation constitutes terminating action for the applicable structural inspection required by paragraph (g) of this AD. (j) Newly Revised Initial Inspection Compliance Time for Certain Airplanes For airplanes identified in Lockheed TriStar L–1011 Service Bulletin 093–57–195, Revision 4, dated March 17, 2010: Do the initial inspection required by paragraph (g)(16) of this AD at the applicable time PO 00000 Frm 00019 Fmt 4700 Sfmt 4700 Repair or modification in accordance with Lockheed TriStar L–1011 Service Bulletin 093–57– 213, Basic Issue, dated December 9, 1994. specified in paragraph (j)(1) or (j)(2) of this AD. (1) For airplanes having serial numbers (S/ Ns) 1002 through 1109 inclusive: At the earlier of the times specified in paragraphs (j)(1)(i) and (j)(1)(ii) of this AD. (i) Before the accumulation of 20,000 total flight cycles, or within 2,200 flight cycles after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs later. (ii) Before the accumulation of 15,000 total flight cycles, or within 2,200 flight cycles after the effective date of this AD, whichever occurs later. (2) For airplanes having S/Ns 1110 through 1250 inclusive: At the earlier of the times specified in paragraphs (j)(2)(i) and (j)(2)(ii) of this AD. (i) Before the accumulation of 30,000 total flight cycles, or within 2,200 flight cycles after August 26, 2005 (the effective date of AD 2005–15–01, Amendment 39–14190 (70 FR 42262, July 22, 2005)), whichever occurs later. (ii) Before the accumulation of 15,000 total flight cycles, or within 2,200 flight cycles E:\FR\FM\27AUR1.SGM 27AUR1 52846 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations after the effective date of this AD, whichever occurs later. (k) Newly Revised Repetitive Intervals for Certain Airplanes For airplanes identified in paragraph (j) of this AD, repeat the inspection required by paragraph (j) of this AD thereafter at the applicable times specified in paragraph (k)(1) or (k)(2) of this AD. (1) For airplanes having S/Ns 1002 through 1156 inclusive: Repeat the inspection at intervals not to exceed 2,200 flight cycles. (2) For airplanes having S/Ns 1157 through 1250 inclusive: Repeat the inspection one time within 2,200 flight cycles after the most recent inspection, and thereafter at intervals not to exceed 1,750 flight cycles. (l) Alternative Methods of Compliance (AMOCs) (1) The Manager, Atlanta ACO, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in the Related Information section of this AD. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. pmangrum on DSK3VPTVN1PROD with RULES (m) Related Information For more information about this AD, contact Carl Gray, Aerospace Engineer, Airframe Branch, ACE–117A, FAA, Atlanta Aircraft Certification Office (ACO), 1701 Columbia Avenue, College Park, Georgia 30337; phone: 404–474–5554; fax: 404–474– 5605; email: carl.w.gray@faa.gov. (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. (3) The following service information was approved for IBR on October 1, 2013. (i) Lockheed TriStar L–1011 Service Bulletin 093–57–195, Revision 4, dated March 17, 2010. (ii) Lockheed Tristar L–1011 Service Bulletin 093–51–041, Revision 2, dated March 30, 2010. (iii) Lockheed TriStar L–1011 Service Bulletin 093–53–269, Revision 1, dated October 28, 1997. (iv) Lockheed TriStar L–1011 Service Bulletin 093–53–274, dated May 28, 1997. (v) Lockheed TriStar L–1011 Service Bulletin 093–53–275, dated December 10, 1996. (vi) Lockheed TriStar L–1011 Service Bulletin 093–53–276, dated June 17, 1996. (vii) Lockheed TriStar L–1011 Service Bulletin 093–57–208, Revision 1, dated October 28, 1997. VerDate Mar<15>2010 13:33 Aug 26, 2013 Jkt 229001 (viii) Lockheed TriStar L–1011 Service Bulletin 093–52–210, dated July 19, 1991, including Lockheed LCC–7622–248, Corrosion Removal and Refurbishment of C1–A Cargo Door Cam Latches, Latch Bellcranks and Matched Latch Support Assemblies, dated February 27, 1990. Pages 1 and 3–8 of this document are dated February 27, 1990. Page 2 is dated February 19, 1990. Page 9 is dated January 4, 1990. Pages 10 and 11 are dated January 5, 1990. (ix) Lockheed TriStar L–1011 Service Bulletin 093–53–054, Revision 1, dated August 12, 1975. (x) Lockheed TriStar L–1011 Service Bulletin 093–53–085, Revision 3, dated December 15, 1989. Pages 3, 4, 7–14, and 16– 23 are dated February 8, 1988. Pages 1, 2, 5, 6, and 15 are dated December 15, 1989. (xi) Lockheed TriStar L–1011 Service Bulletin Change Notification 093–53–260, CN4, dated May 8, 1998. (xii) Lockheed TriStar L–1011 Service Bulletin Change Notification 093–53–266, CN1, dated July 10, 1992. (xiii) Lockheed TriStar L–1011 Service Bulletin Change Notification 093–57–058, R5–CN1, dated May 3, 1993. (xiv) Lockheed TriStar L–1011 Service Bulletin Change Notification 093–57–195, R3–CN1, dated August 22, 1995. (xv) Lockheed TriStar L–1011 Service Bulletin Change Notification 093–57–213, CN1, dated February 20, 1996. (xvi) Lockheed TriStar L–1011 Service Bulletin 093–57–195, Revision 2, dated July 27, 1990. (xvii) Lockheed TriStar L–1011 Service Bulletin 093–57–195, Revision 3, dated June 30, 1992. Pages 1–6, 23–28, 33, 34, 41, 42, and 45–52 of this document are identified as Revision 3, dated June 30, 1992; Pages 7–22, 29–32, 35–40, 43, and 44 are identified as Revision 2, dated July 27, 1990. (xviii) Lockheed TriStar L–1011 Service Bulletin 093–57–213, dated December 9, 1994. (4) The following service information was approved for IBR on August 26, 2005 (70 FR 42262, July 22, 2005). (i) Lockheed TriStar L–1011 Service Bulletin 093–51–041, Revision 1, dated March 3, 2000. (ii) Lockheed TriStar L–1011 Service Bulletin 093–53–070, Basic Issue, dated September 26, 1974. (iii) Lockheed TriStar L–1011 Service Bulletin 093–53–070, Revision 1, dated January 23, 1975. Pages 1, 4–7, and 13–17 of this document are identified as Revision 1, dated January 23, 1975. Pages 2, 3, and 8–12 of this document are identified as Basic Issue, dated September 26, 1974. (iv) Lockheed TriStar L–1011 Service Bulletin 093–53–070, Revision 2, dated July 7, 1975. Pages 1, 2, 7, and 9–14 of this document are identified as Revision 2, dated July 7, 1975. Pages 3 and 8 of this document are identified as Basic Issue, dated September 26, 1974. Pages 4–6 and 15–17 of this document are identified as Revision 1, dated January 23, 1975. (v) Lockheed TriStar L–1011 Service Bulletin 093–53–070, Revision 3, dated September 19, 1989. Pages 1–6 and 8–10 of this document are identified as Revision 3, PO 00000 Frm 00020 Fmt 4700 Sfmt 4700 dated September 19, 1989. Page 7 of this document is identified as Basic Issue, dated September 26, 1974. (vi) Lockheed TriStar L–1011 Service Bulletin 093–53–085, Basic Issue, dated September 29, 1975. (vii) Lockheed TriStar L–1011 Service Bulletin 093–53–085, Revision 1, dated September 3, 1976. Pages 1–3, 6, 9–11, and 15 of this document are identified as Revision 1, dated September 3, 1976. Pages 4, 5, 7, 8, 12–14, and 16 of this document are identified as Basic Issue, dated September 29, 1975. (viii) Lockheed TriStar L–1011 Service Bulletin 093–53–085, Revision 2, dated February 8, 1988. (ix) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Basic Issue, dated September 26, 1975. (x) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Revision 1, dated November 12, 1975. Pages 1, 2, 11, and 15 of this document are identified as Revision 1, dated November 12, 1975. Pages 3–10, 12– 14, and 16 of this document are identified as Basic Issue, dated September 26, 1975. (xi) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Revision 2, dated December 12, 1976. Pages 1, 2, 7, 15, and 16 of this document are identified as Revision 2, dated December 12, 1976. Pages 3–6, 8–10, and 12–14 of this document are identified as Basic Issue, dated September 26, 1975. Page 11 of this document is identified as Revision 1, dated November 12, 1975. (xii) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Revision 3, dated July 19, 1977. Pages 1, 2, 4, 7, 10, 11, and 15 of this document are identified as Revision 3, dated July 19, 1977. Pages 3, 5, 6, 8, 9, and 12–14 of this document are identified as Basic Issue, dated September 26, 1975. Page 16 of this document is identified as Revision 2, dated December 12, 1976. (xiii) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Revision 4, dated July 8, 1985. Pages 1–4, 15, and 16 of this document are identified as Revision 4, dated July 8, 1985. Pages 5, 6, 8, 9, and 12–14 of this document are identified as Basic Issue, dated September 26, 1975. Pages 7, 10, and 11 of this document are identified as Revision 3, dated July 19, 1977. (xiv) Lockheed TriStar L–1011 Service Bulletin 093–53–086, Revision 5, dated April 12, 1990. Pages 1–9 and 13 of this document are identified as Revision 5, dated April 12, 1990. Pages 10–12 of this document are identified as Basic Issue, dated September 26, 1975. Page 14 of this document is identified as Revision 4, dated July 8, 1985. (xv) Lockheed TriStar L–1011 Service Bulletin 093–53–110, Basic Issue, dated August 19, 1991. (xvi) Lockheed TriStar L–1011 Service Bulletin 093–53–110, Revision 1, dated May 7, 1993. Pages 1–7 and 9–12 of this document are identified as Revision 1, dated May 7, 1993. Page 8 of this document is identified as Basic Issue, dated August 19, 1991. (xvii) Lockheed TriStar L–1011 Service Bulletin 093–53–260, Basic Issue, dated May 15, 1991. (xviii) Lockheed TriStar L–1011 Service Bulletin 093–53–266, Basic Issue, dated March 2, 1992. E:\FR\FM\27AUR1.SGM 27AUR1 pmangrum on DSK3VPTVN1PROD with RULES Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations (xix) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Basic Issue, dated September 16, 1975. (xx) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Revision 1, dated December 1, 1976. Pages 1, 2, 4, 7, 8, 11, and 15–19 of this document are identified as Revision 1, dated December 1, 1976. Pages 3, 5, 6, 9, 10, and 12–14 of this document are identified as Basic Issue, dated September 16, 1975. (xxi) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Revision 2, dated June 30, 1978. Pages 1–4, 7, 8, 11, and 15–19 of this document are identified as Revision 2, dated June 30, 1978. Pages 5, 6, 9, 10, and 12–14 of this document are identified as Basic issue, dated September 16, 1975. (xxii) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Revision 3, dated October 19, 1978. Pages 1–3, 7, 8, 11, and 15– 19 of this document are identified as Revision 3, dated October 19, 1978. Page 4 of this document is identified as Revision 2, dated June 30, 1978. Pages 5, 6, 9, 10, and 12–14 of this document are identified as Basic Issue, dated September 16, 1975. (xxiii) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Revision 4, dated July 6, 1981. Pages 1–3 and 19 of this document are identified as Revision 4, dated July 6, 1981. Pages 4 and 15 of this document are identified as Revision 2, dated June 30, 1978. Pages 5, 6, 9, 10, and 12–14 of this document are identified as Basic Issue, dated September 16, 1975. Pages 7, 8, 11, and 16–18 of this document are identified as Revision 3, dated October 19, 1978. (xxiv) Lockheed TriStar L–1011 Service Bulletin 093–57–058, Revision 5, dated June 9, 1983. Pages 1, 3, 4, and 7 of this document are identified as Revision 5, dated June 9, 1983. Page 2 of this document is identified as Revision 4, dated July 6, 1981. Pages 5, 6, 9, 10, and 12–14 of this document are identified as Basic Issue, dated September 16, 1975. Pages 8, 11, and 16–19 of this document are identified as Revision 3, dated October 19, 1978. Page 15 of this document is identified as Revision 2, dated June 30, 1978. (xxv) Lockheed TriStar L–1011 Service Bulletin 093–57–085, Basic Issue, dated May 7, 1993. This document was incorrectly identified as ‘‘Revision 1’’ in the ‘‘Service bulletin’’ column of Table 2—Material Incorporated by Reference in AD 2005–15– 01, Amendment 39–14190 (70 FR 42262, July 22, 2005). (xxvi) Lockheed TriStar L–1011 Service Bulletin 093–57–085, Revision 1, dated December 1, 1997. Pages 1–7, 9, and 10 of this document are identified as Revision 1, dated December 1, 1997. Pages 8 and 11–17 are identified as Basic issue, dated May 7, 1993. (5) For Lockheed service information identified in this AD, contact Lockheed Martin Corporation/Lockheed Martin Aeronautics Company, L1011 Technical Support Center, Dept. 6A4M, Zone 0579, 86 South Cobb Drive, Marietta, GA 30063–0579; telephone 770–494–5444; fax 770–494–5445; email L1011.support@lmco.com; Internet http://www.lockheedmartin.com/ams/tools/ TechPubs.html. VerDate Mar<15>2010 13:33 Aug 26, 2013 Jkt 229001 (6) You may view this service information at FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call 425–227–1221. (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: http:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on July 21, 2013. Stephen P. Boyd, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2013–20731 Filed 8–26–13; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2013–0709; Amendment No. 71–45] RIN 2120–AA66 Airspace Designations; Incorporation by Reference Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: 52847 History FAA Order 7400.9W, Airspace Designations and Reporting Points, effective September 15, 2012, listed Class A, B, C, D and E airspace areas; air traffic service routes; and reporting points. Due to the length of these descriptions, the FAA requested approval from the Office of the Federal Register to incorporate the material by reference in the Federal Aviation Regulations section 71.1, effective September 15, 2012, through September 15, 2013. During the incorporation by reference period, the FAA processed all proposed changes of the airspace listings in FAA Order 7400.9W in full text as proposed rule documents in the Federal Register. Likewise, all amendments of these listings were published in full text as final rules in the Federal Register. This rule reflects the periodic integration of these final rule amendments into a revised edition of Order 7400.9X, Airspace Designations and Reporting Points. The Director of the Federal Register has approved the incorporation by reference of FAA Order 7400.9X in section 71.1, as of September 15, 2013, through September 15, 2014. This rule also explains the procedures the FAA will use to amend the airspace designations incorporated by reference in part 71. Sections 71.5, 71.15, 71.31, 71.33, 71.41, 71.51, 71.61, 71.71, and 71.901 are also updated to reflect the incorporation by reference of FAA Order 7400.9X. SUMMARY: The Rule These regulations are effective September 15, 2013, through September 15, 2014. The incorporation by reference of FAA Order 7400.9X is approved by the Director of the Federal Register as of September 15, 2013, through September 15, 2014. FOR FURTHER INFORMATION CONTACT: Sarah A. Combs, Airspace Policy and ATC Procedures Group, Office of Airspace Services, Federal Aviation Administration, 800 Independence Avenue SW., Washington, DC 20591; telephone: (202) 267–8783. SUPPLEMENTARY INFORMATION: This action amends Title 14 Code of Federal Regulations (14 CFR) part 71 to reflect the approval by the Director of the Federal Register of the incorporation by reference of FAA Order 7400.9X, effective September 15, 2013, through September 15, 2014. During the incorporation by reference period, the FAA will continue to process all proposed changes of the airspace listings in FAA Order 7400.9X in full text as proposed rule documents in the Federal Register. Likewise, all amendments of these listings will be published in full text as final rules in the Federal Register. The FAA will periodically integrate all final rule amendments into a revised edition of the Order, and submit the revised edition to the Director of the Federal Register for approval for incorporation by reference in section 71.1. The FAA has determined that this action: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034; February This action amends Title 14 Code of Federal Regulations (14 CFR) part 71 relating to airspace designations to reflect the approval by the Director of the Federal Register of the incorporation by reference of FAA Order 7400.9X, Airspace Designations and Reporting Points. This action also explains the procedures the FAA will use to amend the listings of Class A, B, C, D, and E airspace areas; air traffic service routes; and reporting points incorporated by reference. DATES: PO 00000 Frm 00021 Fmt 4700 Sfmt 4700 E:\FR\FM\27AUR1.SGM 27AUR1

Agencies

[Federal Register Volume 78, Number 166 (Tuesday, August 27, 2013)]
[Rules and Regulations]
[Pages 52841-52847]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-20731]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-1078; Directorate Identifier 2011-NM-012-AD; 
Amendment 39-17534; AD 2013-15-18]
RIN 2120-AA64


Airworthiness Directives; Lockheed Martin Corporation/Lockheed 
Martin Aeronautics Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are superseding an airworthiness directive (AD) for all 
Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 
L-1011 series airplanes. AD 2005-15-01 required repetitive inspections 
to detect corrosion or fatigue cracking of certain structural elements 
of the airplane, corrective actions if necessary, and incorporation of 
certain structural modifications. This new AD reduces certain 
compliance times for the initial inspection and the repetitive 
inspection interval for certain airplanes. This AD was prompted by 
reports of small cracks in additional areas outside those addressed in 
AD 2005-15-01, prior to the inspection threshold required by the AD 
2005-15-01. We are issuing this AD to prevent corrosion or fatigue 
cracking of certain structural elements, which could result in reduced 
structural integrity of the airplane.

DATES: This AD is effective October 1, 2013.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in the AD as of October 1, 
2013.
    The Director of the Federal Register approved the incorporation by 
reference of certain other publications listed in this AD as of August 
26, 2005 (70 FR 42262, July 22, 2005).

ADDRESSES: For service information identified in this AD, contact 
Lockheed Martin Corporation/Lockheed Martin Aeronautics Company, L-1011 
Technical Support Center, Dept. 6A4M, Zone 0579, 86 South Cobb Drive, 
Marietta, GA 30063-0579; telephone 770-494-5444; fax 770-494-5445; 
email L1011.support@lmco.com; Internet http://www.lockheedmartin.com/ams/tools/TechPubs.html. You may review copies of the referenced 
service information at the FAA, Transport Airplane Directorate, 1601 
Lind Avenue SW., Renton, Washington. For information on the 
availability of this material at the FAA, call 425-227-1221.

Examining the AD Docket

    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: Carl Gray, Aerospace Engineer, 
Airframe Branch, ACE-117A, FAA, Atlanta Aircraft Certification Office 
(ACO), 1701 Columbia Avenue, College Park, Georgia 30337; phone: 404-
474-5554; fax: 404-474-5605; email: carl.w.gray@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to supersede AD 2005-15-01, Amendment 39-14190 (70 FR 42262, 
July 22, 2005). AD 2005-15-01 applied to the specified products. The 
NPRM published in the Federal Register on October 16, 2012 (77 FR 
63275). The NPRM proposed to continue to require repetitive inspections 
to detect corrosion or fatigue cracking of certain structural elements 
of the airplane, corrective actions if necessary, and incorporation of 
certain structural modifications. The NPRM also proposed to require 
reducing certain compliance times for the initial inspection and the 
repetitive inspection interval for certain airplanes.

Comments

    We gave the public the opportunity to participate in developing 
this AD. The following presents the comments received on the proposal 
(77 FR 63275, October 16, 2012) and the FAA's response to each comment.

Request To Update Certain Address Information

    Lockheed Martin Corporation/Lockheed Martin Aeronautics Company 
requested that we revise the NPRM (77 FR 63275, October 16, 2012) to 
update its address information.
    We agree to update the address information in this final rule. We 
have included this updated information in the ADDRESSES section and 
paragraph (n)(5) of this AD.

Additional Change Made to This AD

    We have revised paragraph (g)(10) of this AD (in table 1 to 
paragraph (g) of this AD) to include paragraph identifiers for 
paragraphs (g)(10)(i) and (g)(10)(ii) of this AD. This change is for 
formatting purposes only.

Conclusion

    We reviewed the relevant data, considered the comment received, and 
determined that air safety and the public interest require adopting 
this AD with the change described previously--and minor editorial 
changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (77 FR 63275, October 16, 2012) for correcting the unsafe 
condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (77 FR 63275, October 16, 2012).
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of the AD.

Costs of Compliance

    We estimate that this AD affects 26 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

[[Page 52842]]



                                                 Estimated costs
----------------------------------------------------------------------------------------------------------------
                                                                                                 Cost on U.S.
              Action                    Labor cost        Parts cost      Cost per product        operators
----------------------------------------------------------------------------------------------------------------
Inspections [retained actions      129 work-hours x                 $0  $10,965 per          $285,090 per
 from AD 2005-15-01, Amendment 39-  $85 per hour =                       inspection cycle..   inspection cycle.
 14190 (70 FR 42262, July 22,       $10,965 per
 2005)].                            inspection cycle.
Modification [retained action      614 work-hours x           $142,275  $194,465...........  $5,056,090.
 from AD 2005-15-01, Amendment 39-  $85 per hour =
 14190 (70 FR 42262, July 22,       $52,190.
 2005)].
----------------------------------------------------------------------------------------------------------------

    We have received no definitive data that would enable us to provide 
cost estimates for the retained on-condition actions specified in this 
AD.

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 have 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 that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under 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.

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 airworthiness directive (AD) 
2005-15-01, Amendment 39-14190 (70 FR 42262, July 22, 2005), and adding 
the following new AD:

2013-15-18 Lockheed Martin Corporation/Lockheed Martin Aeronautics 
Company: Amendment 39-17534; Docket No. FAA-2012-1078; Directorate 
Identifier 2011-NM-012-AD.

(a) Effective Date

    This AD is effective October 1, 2013.

(b) Affected ADs

    This AD supersedes AD 2005-15-01, Amendment 39-14190 (70 FR 
42262, July 22, 2005).

(c) Applicability

    This AD applies to all Lockheed Martin Corporation/Lockheed 
Martin Aeronautics Company Model L-1011-385-1, L-1011-385-1-14, L-
1011-385-1-15, and L-1011-385-3 airplanes, certificated in any 
category.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 51, Standard practices/structures; 52, Doors; 
53, Fuselage; 57, Wings.

(e) Unsafe Condition

    This AD was prompted by reports of small cracks in additional 
areas outside those addressed in AD 2005-15-01, Amendment 39-14190 
(70 FR 42262, July 22, 2005), prior to the inspection threshold 
required by AD 2005-15-01. We are issuing this AD to prevent 
corrosion or fatigue cracking of certain structural elements, which 
could result in reduced structural integrity of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Retained Inspections With Revised Service Information and Reduced 
Compliance Times

    This paragraph restates the inspections required by paragraph 
(a) of AD 2005-15-01, Amendment 39-14190 (70 FR 42262, July 22, 
2005), with revised service information and reduced compliance times 
for paragraph (g)(16) of this AD. At the time specified in the 
``Initial Compliance Time'' column of table 1 to paragraph (g) of 
this AD, perform structural inspections to detect corrosion or 
fatigue cracking of certain structural elements of the airplane, in 
accordance with the applicable service bulletins listed under 
``Service Bulletin Number, Revision, and Date'' in tables I and II 
of Lockheed Tristar L-1011 Service Bulletin 093-51-041, Revision 1, 
dated March 3, 2000; or Revision 2, dated March 30, 2010 (The 
applicable service bulletins are also identified in Table 1 to 
paragraph (g) of this AD.) As of the effective date of this AD, only 
Lockheed Tristar L-1011 Service Bulletin 093-51-041, Revision 2, 
dated March 30, 2010, may be used for the actions required by this 
paragraph. Thereafter, repeat the inspections at intervals specified 
in the ``Repetitive Intervals'' column of table 1 to paragraph (g) 
of this AD.

[[Page 52843]]



                                       Table 1 to Paragraph (g) of This AD
----------------------------------------------------------------------------------------------------------------
                                    Initial compliance time (whichever
                                     occurs later between the times in
                                   ``Inspection Threshold'' and ``Grace
 Lockheed TriStar L-1011 Service                 Period'')                    Repetitive      Terminating action
            Bulletin             ----------------------------------------      intervals
                                      Inspection
                                       threshold         Grace period
----------------------------------------------------------------------------------------------------------------
(1) 093-53-269, Revision 1,       Before the          Within 6,450        At intervals not    (None).
 dated October 28, 1997.           accumulation of     flight cycles or    to exceed 6,450
                                   8,000 total         5 years after       flight cycles or
                                   flight cycles or    August 26, 2005     5 years,
                                   15,000 total        (the effective      whichever occurs
                                   flight hours,       date of AD 2005-    first.
                                   whichever occurs    15-01, Amendment
                                   first.              39-14190 (70 FR
                                                       42262, July 22,
                                                       2005)), whichever
                                                       occurs first.
(2) 093-53-274, dated May 28,     Within 14 months    (None)............  At intervals not    (None).
 1997.                             after August 26,                        to exceed 14
                                   2005 (the                               months.
                                   effective date of
                                   AD 2005-15-01,
                                   Amendment 39-
                                   14190 (70 FR
                                   42262, July 22,
                                   2005)).
(3) 093-53-275, dated December    Within 6,450        (None)............  (None)............  (None).
 10, 1996.                         flight cycles or
                                   5 years after
                                   August 26, 2005
                                   (the effective
                                   date of AD 2005-
                                   15-01, Amendment
                                   39-14190 (70 FR
                                   42262, July 22,
                                   2005)), whichever
                                   occurs first.
(4) 093-53-276, dated June 17,    At the next         (None)............  At intervals not    (None).
 1996.                             Corrosion                               to exceed the
                                   Prevention and                          next CPCP
                                   Control Program                         inspection.
                                   (CPCP) inspection
                                   after August 26,
                                   2005 (the
                                   effective date of
                                   AD 2005-15-01,
                                   Amendment 39-
                                   14190 (70 FR
                                   42262, July 22,
                                   2005)).
(5) 093-57-085, Revision 1,       Before the          Within 1,800        At intervals not    Modification in
 dated December 1, 1997.           accumulation of     flight cycles or    to exceed 1,800     accordance with
                                   26,000 total        3,300 flight        flight cycles or    Lockheed TriStar
                                   flight cycles or    hours after         3,300 flight        L-1011 Service
                                   48,000 total        August 26, 2005     hours, whichever    Bulletin 093-57-
                                   flight hours,       (the effective      occurs first.       085, Basic Issue,
                                   whichever occurs    date of AD 2005-                        dated May 7,
                                   first.              15-01, Amendment                        1993; or Revision
                                                       39-14190 (70 FR                         1, dated December
                                                       42262, July 22,                         1, 1997.
                                                       2005)), whichever
                                                       occurs first.
(6) 093-57-208, Revision 1,       Before the          Within 6,450        At intervals not    (None).
 dated October 28, 1997.           accumulation of     flight cycles or    to exceed 6,450
                                   18,000 total        5 years after       flight cycles or
                                   flight cycles.      August 26, 2005     5 years,
                                                       (the effective      whichever occurs
                                                       date of AD 2005-    first.
                                                       15-01, Amendment
                                                       39-14190 (70 FR
                                                       42262, July 22,
                                                       2005)), whichever
                                                       occurs first.
(7) 093-52-210, dated July 19,    Within 5,000        (None)............  (None)............  (None).
 1991, including Lockheed LCC-     flight hours or
 7622-248, Corrosion Removal and   18 months after
 Refurbishment of C1-A Cargo       August 26, 2005
 Door Cam Latches, Latch           (the effective
 Bellcranks and Matched Latch      date of AD 2005-
 Support Assemblies, dated         15-01, Amendment
 February 27, 1990.                39-14190 (70 FR
                                   42262, July 22,
                                   2005)), whichever
                                   occurs first.
(8) 093-53-054, Revision 1,       Within 6,450        (None)............  (None)............  (None).
 dated August 12, 1975.            flight cycles or
                                   5 years after
                                   August 26, 2005
                                   (the effective
                                   date of AD 2005-
                                   15-01, Amendment
                                   39-14190 (70 FR
                                   42262, July 22,
                                   2005)), whichever
                                   occurs first.

[[Page 52844]]

 
(9) 093-53-070, Revision 3,       Before the          Within 1,500        At intervals not    Modification in
 dated September 19, 1989.         accumulation of     flight hours        to exceed 3,000     accordance with
                                   6,000 total         after August 26,    flight hours.       Lockheed TriStar
                                   flight hours.       2005 (the                               L-1011 Service
                                                       effective date of                       Bulletin 093-53-
                                                       AD 2005-15-01,                          070, Basic Issue,
                                                       Amendment 39-                           dated September
                                                       14190 (70 FR                            26, 1974;
                                                       42262, July 22,                         Revision 1, dated
                                                       2005)).                                 January 23, 1975;
                                                                                               Revision 2, dated
                                                                                               July 7, 1975; or
                                                                                               Revision 3, dated
                                                                                               September 19,
                                                                                               1989.
(10) 093-53-085, Revision 3,      (i) Part I: Before  Part I: Within      Part I: At          Modification in
 dated December 15, 1989.          the accumulation    1,600 flight        intervals not to    accordance with
                                   of 20,000 flight    cycles or 3,000     exceed 1,600        Lockheed TriStar
                                   cycles or 37,000    flight hours        flight cycles or    L-1011 Service
                                   total flight        after August 26,    3,000 flight        Bulletin 093-53-
                                   hours, whichever    2005 (the           hours, whichever    085, Basic Issue,
                                   occurs first.       effective date of   occurs first.       dated September
                                                       AD 2005-15-01,                          29, 1975;
                                                       Amendment 39-                           Revision 1, dated
                                                       14190 (70 FR                            September 3,
                                                       42262, July 22,                         1976; or Revision
                                                       2005)), whichever                       2, dated February
                                                       occurs first.                           8, 1988.
                                  (ii) Part II:       Part II: Within     Part II: At         Modification in
                                   Before the          5,000 flight        intervals not to    accordance with
                                   accumulation of     cycles or 9,200     exceed 5,000        Lockheed TriStar
                                   30,000 flight       flight hours        flight cycles or    L-1011 Service
                                   cycles or 55,000    after August 26,    9,200 flight        Bulletin 093-53-
                                   total flight        2005 (the           hours, whichever    085, Basic Issue,
                                   hours, whichever    effective date of   occurs first.       dated September
                                   occurs first.       AD 2005-15-01,                          29, 1975;
                                                       Amendment 39-                           Revision 1, dated
                                                       14190 (70 FR                            September 3,
                                                       42262, July 22,                         1976; or Revision
                                                       2005)), whichever                       2, dated February
                                                       occurs first.                           8, 1988.
(11) 093-53-086, Revision 5,      Before the          Within 1,600        At intervals not    Modification in
 dated April 12, 1990.             accumulation of     flight cycles or    to exceed 1,600     accordance with
                                   9,000 flight        3,000 flight        flight cycles or    Lockheed TriStar
                                   cycles or 10,000    hours after         3,000 flight        L-1011 Service
                                   flight hours,       August 26, 2005     hours, whichever    Bulletin 093-53-
                                   whichever occurs    (the effective      occurs first.       086, Basic Issue,
                                   first.              date of AD 2005-                        dated September
                                                       15-01, Amendment                        26, 1975;
                                                       39-14190 (70 FR                         Revision 1, dated
                                                       42262, July 22,                         November 12,
                                                       2005)), whichever                       1975; Revision 2,
                                                       occurs first.                           dated December
                                                                                               12, 1976;
                                                                                               Revision 3, dated
                                                                                               July 19, 1977;
                                                                                               Revision 4, dated
                                                                                               July 8, 1985; or
                                                                                               Revision 5, dated
                                                                                               April 12, 1990.
(12) 093-53-110, Revision 1,      Before the          Within 2,200        At intervals not    Modification in
 dated May 7, 1993.                accumulation of     flight cycles or    to exceed 2,200     accordance with
                                   22,000 total        4,000 flight        flight cycles or    Lockheed TriStar
                                   flight cycles or    hours after         4,000 flight        L-1011 Service
                                   40,000 total        August 26, 2005     hours, whichever    Bulletin 093-53-
                                   flight hours,       (the effective      occurs first.       110, Basic Issue,
                                   whichever occurs    date of AD 2005-                        dated August 19,
                                   first.              15-01, Amendment                        1991; or Revision
                                                       39-14190 (70 FR                         1, dated May 7,
                                                       42262, July 22,                         1993.
                                                       2005)), whichever
                                                       occurs first.
(13) Change Notification 093-53-  Before the          Within 800 flight   At intervals not    Inspection and
 260, CN4, dated May 8, 1998.      accumulation of     cycles or 1,500     to exceed 800       modification in
                                   8,000 total         flight hours        flight cycles or    accordance with
                                   flight cycles or    after August 26,    1,500 flight        Part 2.A. of
                                   20,000 total        2005 (the           hours, whichever    Lockheed TriStar
                                   flight hours,       effective date of   occurs first.       L-1011 Service
                                   whichever occurs    AD 2005-15-01,                          Bulletin 093-53-
                                   first.              Amendment 39-                           260, Basic Issue,
                                                       14190 (70 FR                            dated May 15,
                                                       42262, July 22,                         1991.
                                                       2005)), whichever
                                                       occurs first.
(14) Change Notification 093-53-  Within 12 months    (None)............  At intervals not    Modification in
 266, CN1, dated July 10, 1992.    after August 26,                        to exceed 90 days.  accordance with
                                   2005 (the                                                   Lockheed TriStar
                                   effective date of                                           L-1011 Service
                                   AD 2005-15-01,                                              Bulletin 093-53-
                                   Amendment 39-                                               266, Basic Issue,
                                   14190 (70 FR                                                dated March 2,
                                   42262, July 22,                                             1992.
                                   2005)).

[[Page 52845]]

 
(15) Change Notification 093-57-  Before the          Within 1,600        At intervals not    Modification in
 058, R5-CN1, dated May 3, 1993.   accumulation of     flight cycles or    to exceed 1,600     accordance with
                                   20,000 total        3,000 flight        flight cycles or    Lockheed TriStar
                                   flight cycles or    hours after         3,000 flight        L-1011 Service
                                   37,000 total        August 26, 2005     hours, whichever    Bulletin 093-57-
                                   flight hours,       (the effective      occurs first.       058, Basic Issue,
                                   whichever occurs    date of AD 2005-                        dated September
                                   first.              15-01, Amendment                        16, 1975;
                                                       39-14190 (70 FR                         Revision 1, dated
                                                       42262, July 22,                         December 1, 1976;
                                                       2005)), whichever                       Revision 2, dated
                                                       occurs first.                           June 30, 1978;
                                                                                               Revision 3, dated
                                                                                               October 19, 1978;
                                                                                               Revision 4, dated
                                                                                               July 6, 1981; or
                                                                                               Revision 5, dated
                                                                                               June 9, 1983.
(16) Change Notification 093-57-  At the applicable   At the applicable   At the applicable   Modification in
 195, R3-CN1, dated August 22,     time specified in   time specified in   time specified in   accordance with
 1995; or Lockheed TriStar L-      paragraph (j) of    paragraph (j) of    paragraph (k) of    Lockheed TriStar
 1011 Service Bulletin 093-57-     this AD.            this AD.            this AD.            L-1011 Service
 195, Revision 4, dated March                                                                  Bulletin 093-57-
 17, 2010.                                                                                     195, Revision 2,
                                                                                               dated July 27,
                                                                                               1990; Revision 3,
                                                                                               dated June 30,
                                                                                               1992; or Revision
                                                                                               4, dated March
                                                                                               17, 2010.
(17) Change Notification 093-57-  (i) For Model L-    Within 6,450        At intervals not    Repair or
 213, CN1, dated February 20,      1011-385-1, L-      flight cycles or    to exceed 6,450     modification in
 1996.                             1011-385-1-14, L-   5 years after       flight cycles or    accordance with
                                   1011-385-1-15:      August 26, 2005     5 years,            Lockheed TriStar
                                   Before the          (the effective      whichever occurs    L-1011 Service
                                   accumulation of     date of AD 2005-    first.              Bulletin 093-57-
                                   15,000 total        15-01, Amendment                        213, Basic Issue,
                                   flight cycles.      39-14190 (70 FR                         dated December 9,
                                                       42262, July 22,                         1994.
                                                       2005)), whichever
                                                       occurs first.
                                  (ii) For Model L-   Within 6,450        At intervals not    Repair or
                                   1011-385-3:         flight cycles or    to exceed 6,450     modification in
                                   Before the          5 years after       flight cycles or    accordance with
                                   accumulation of     August 26, 2005     5 years,            Lockheed TriStar
                                   10,000 total        (the effective      whichever occurs    L-1011 Service
                                   flight cycles.      date of AD 2005-    first.              Bulletin 093-57-
                                                       15-01, Amendment                        213, Basic Issue,
                                                       39-14190 (70 FR                         dated December 9,
                                                       42262, July 22,                         1994.
                                                       2005)), whichever
                                                       occurs first.
----------------------------------------------------------------------------------------------------------------

(h) Retained Corrective Action With a Certain Compliance Method Removed 
and Revised Service Information

    This paragraph restates the corrective action required by 
paragraph (b) of AD 2005-15-01, Amendment 39-14190 (70 FR 42262, 
July 22, 2005), with a certain compliance method removed and revised 
service information. If any cracking or corrosion is detected during 
any inspection required by paragraph (g) of this AD, prior to 
further flight, accomplish the actions specified in paragraph 
(h)(1), (h)(2), or (h)(3) of this AD.
    (1) Repair in accordance with the applicable service bulletin 
referenced in table I or II of Lockheed Tristar L-1011 Service 
Bulletin 093-51-041, Revision 1, dated March 3, 2000; or Revision 2, 
dated March 30, 2010.
    (2) Accomplish the terminating modification in accordance with 
the applicable service bulletin referenced in table I or II of 
Lockheed Tristar L-1011 Service Bulletin 093-51-041, Revision 1, 
dated March 3, 2000; or Revision 2, dated March 30, 2010.
    (3) Repair in accordance with a method approved by the Manager, 
Atlanta Aircraft Certification Office (ACO), FAA. Information on 
additional methods of compliance can be obtained from the Manager, 
Atlanta ACO.

(i) Retained Terminating Action

    This paragraph restates the terminating action required by 
paragraph (c) of AD 2005-15-01, Amendment 39-14190 (70 FR 42262, 
July 22, 2005). Within 5 years or 5,000 flight cycles after August 
26, 2005 (the effective date of AD 2005-15-01), whichever occurs 
first, install the terminating modification referenced in the 
applicable service bulletin listed in table 1 to paragraph (g) of 
this AD, in accordance with the applicable service bulletin listed 
in table 1 to paragraph (g) of this AD. Such installation 
constitutes terminating action for the applicable structural 
inspection required by paragraph (g) of this AD.

(j) Newly Revised Initial Inspection Compliance Time for Certain 
Airplanes

    For airplanes identified in Lockheed TriStar L-1011 Service 
Bulletin 093-57-195, Revision 4, dated March 17, 2010: Do the 
initial inspection required by paragraph (g)(16) of this AD at the 
applicable time specified in paragraph (j)(1) or (j)(2) of this AD.
    (1) For airplanes having serial numbers (S/Ns) 1002 through 1109 
inclusive: At the earlier of the times specified in paragraphs 
(j)(1)(i) and (j)(1)(ii) of this AD.
    (i) Before the accumulation of 20,000 total flight cycles, or 
within 2,200 flight cycles after August 26, 2005 (the effective date 
of AD 2005-15-01, Amendment 39-14190 (70 FR 42262, July 22, 2005)), 
whichever occurs later.
    (ii) Before the accumulation of 15,000 total flight cycles, or 
within 2,200 flight cycles after the effective date of this AD, 
whichever occurs later.
    (2) For airplanes having S/Ns 1110 through 1250 inclusive: At 
the earlier of the times specified in paragraphs (j)(2)(i) and 
(j)(2)(ii) of this AD.
    (i) Before the accumulation of 30,000 total flight cycles, or 
within 2,200 flight cycles after August 26, 2005 (the effective date 
of AD 2005-15-01, Amendment 39-14190 (70 FR 42262, July 22, 2005)), 
whichever occurs later.
    (ii) Before the accumulation of 15,000 total flight cycles, or 
within 2,200 flight cycles

[[Page 52846]]

after the effective date of this AD, whichever occurs later.

(k) Newly Revised Repetitive Intervals for Certain Airplanes

    For airplanes identified in paragraph (j) of this AD, repeat the 
inspection required by paragraph (j) of this AD thereafter at the 
applicable times specified in paragraph (k)(1) or (k)(2) of this AD.
    (1) For airplanes having S/Ns 1002 through 1156 inclusive: 
Repeat the inspection at intervals not to exceed 2,200 flight 
cycles.
    (2) For airplanes having S/Ns 1157 through 1250 inclusive: 
Repeat the inspection one time within 2,200 flight cycles after the 
most recent inspection, and thereafter at intervals not to exceed 
1,750 flight cycles.

(l) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Atlanta ACO, FAA, has the authority to approve 
AMOCs for this AD, if requested using the procedures found in 14 CFR 
39.19. In accordance with 14 CFR 39.19, send your request to your 
principal inspector or local Flight Standards District Office, as 
appropriate. If sending information directly to the manager of the 
ACO, send it to the attention of the person identified in the 
Related Information section of this AD.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.

(m) Related Information

    For more information about this AD, contact Carl Gray, Aerospace 
Engineer, Airframe Branch, ACE-117A, FAA, Atlanta Aircraft 
Certification Office (ACO), 1701 Columbia Avenue, College Park, 
Georgia 30337; phone: 404-474-5554; fax: 404-474-5605; email: 
carl.w.gray@faa.gov.

(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.
    (3) The following service information was approved for IBR on 
October 1, 2013.
    (i) Lockheed TriStar L-1011 Service Bulletin 093-57-195, 
Revision 4, dated March 17, 2010.
    (ii) Lockheed Tristar L-1011 Service Bulletin 093-51-041, 
Revision 2, dated March 30, 2010.
    (iii) Lockheed TriStar L-1011 Service Bulletin 093-53-269, 
Revision 1, dated October 28, 1997.
    (iv) Lockheed TriStar L-1011 Service Bulletin 093-53-274, dated 
May 28, 1997.
    (v) Lockheed TriStar L-1011 Service Bulletin 093-53-275, dated 
December 10, 1996.
    (vi) Lockheed TriStar L-1011 Service Bulletin 093-53-276, dated 
June 17, 1996.
    (vii) Lockheed TriStar L-1011 Service Bulletin 093-57-208, 
Revision 1, dated October 28, 1997.
    (viii) Lockheed TriStar L-1011 Service Bulletin 093-52-210, 
dated July 19, 1991, including Lockheed LCC-7622-248, Corrosion 
Removal and Refurbishment of C1-A Cargo Door Cam Latches, Latch 
Bellcranks and Matched Latch Support Assemblies, dated February 27, 
1990. Pages 1 and 3-8 of this document are dated February 27, 1990. 
Page 2 is dated February 19, 1990. Page 9 is dated January 4, 1990. 
Pages 10 and 11 are dated January 5, 1990.
    (ix) Lockheed TriStar L-1011 Service Bulletin 093-53-054, 
Revision 1, dated August 12, 1975.
    (x) Lockheed TriStar L-1011 Service Bulletin 093-53-085, 
Revision 3, dated December 15, 1989. Pages 3, 4, 7-14, and 16-23 are 
dated February 8, 1988. Pages 1, 2, 5, 6, and 15 are dated December 
15, 1989.
    (xi) Lockheed TriStar L-1011 Service Bulletin Change 
Notification 093-53-260, CN4, dated May 8, 1998.
    (xii) Lockheed TriStar L-1011 Service Bulletin Change 
Notification 093-53-266, CN1, dated July 10, 1992.
    (xiii) Lockheed TriStar L-1011 Service Bulletin Change 
Notification 093-57-058, R5-CN1, dated May 3, 1993.
    (xiv) Lockheed TriStar L-1011 Service Bulletin Change 
Notification 093-57-195, R3-CN1, dated August 22, 1995.
    (xv) Lockheed TriStar L-1011 Service Bulletin Change 
Notification 093-57-213, CN1, dated February 20, 1996.
    (xvi) Lockheed TriStar L-1011 Service Bulletin 093-57-195, 
Revision 2, dated July 27, 1990.
    (xvii) Lockheed TriStar L-1011 Service Bulletin 093-57-195, 
Revision 3, dated June 30, 1992. Pages 1-6, 23-28, 33, 34, 41, 42, 
and 45-52 of this document are identified as Revision 3, dated June 
30, 1992; Pages 7-22, 29-32, 35-40, 43, and 44 are identified as 
Revision 2, dated July 27, 1990.
    (xviii) Lockheed TriStar L-1011 Service Bulletin 093-57-213, 
dated December 9, 1994.
    (4) The following service information was approved for IBR on 
August 26, 2005 (70 FR 42262, July 22, 2005).
    (i) Lockheed TriStar L-1011 Service Bulletin 093-51-041, 
Revision 1, dated March 3, 2000.
    (ii) Lockheed TriStar L-1011 Service Bulletin 093-53-070, Basic 
Issue, dated September 26, 1974.
    (iii) Lockheed TriStar L-1011 Service Bulletin 093-53-070, 
Revision 1, dated January 23, 1975. Pages 1, 4-7, and 13-17 of this 
document are identified as Revision 1, dated January 23, 1975. Pages 
2, 3, and 8-12 of this document are identified as Basic Issue, dated 
September 26, 1974.
    (iv) Lockheed TriStar L-1011 Service Bulletin 093-53-070, 
Revision 2, dated July 7, 1975. Pages 1, 2, 7, and 9-14 of this 
document are identified as Revision 2, dated July 7, 1975. Pages 3 
and 8 of this document are identified as Basic Issue, dated 
September 26, 1974. Pages 4-6 and 15-17 of this document are 
identified as Revision 1, dated January 23, 1975.
    (v) Lockheed TriStar L-1011 Service Bulletin 093-53-070, 
Revision 3, dated September 19, 1989. Pages 1-6 and 8-10 of this 
document are identified as Revision 3, dated September 19, 1989. 
Page 7 of this document is identified as Basic Issue, dated 
September 26, 1974.
    (vi) Lockheed TriStar L-1011 Service Bulletin 093-53-085, Basic 
Issue, dated September 29, 1975.
    (vii) Lockheed TriStar L-1011 Service Bulletin 093-53-085, 
Revision 1, dated September 3, 1976. Pages 1-3, 6, 9-11, and 15 of 
this document are identified as Revision 1, dated September 3, 1976. 
Pages 4, 5, 7, 8, 12-14, and 16 of this document are identified as 
Basic Issue, dated September 29, 1975.
    (viii) Lockheed TriStar L-1011 Service Bulletin 093-53-085, 
Revision 2, dated February 8, 1988.
    (ix) Lockheed TriStar L-1011 Service Bulletin 093-53-086, Basic 
Issue, dated September 26, 1975.
    (x) Lockheed TriStar L-1011 Service Bulletin 093-53-086, 
Revision 1, dated November 12, 1975. Pages 1, 2, 11, and 15 of this 
document are identified as Revision 1, dated November 12, 1975. 
Pages 3-10, 12-14, and 16 of this document are identified as Basic 
Issue, dated September 26, 1975.
    (xi) Lockheed TriStar L-1011 Service Bulletin 093-53-086, 
Revision 2, dated December 12, 1976. Pages 1, 2, 7, 15, and 16 of 
this document are identified as Revision 2, dated December 12, 1976. 
Pages 3-6, 8-10, and 12-14 of this document are identified as Basic 
Issue, dated September 26, 1975. Page 11 of this document is 
identified as Revision 1, dated November 12, 1975.
    (xii) Lockheed TriStar L-1011 Service Bulletin 093-53-086, 
Revision 3, dated July 19, 1977. Pages 1, 2, 4, 7, 10, 11, and 15 of 
this document are identified as Revision 3, dated July 19, 1977. 
Pages 3, 5, 6, 8, 9, and 12-14 of this document are identified as 
Basic Issue, dated September 26, 1975. Page 16 of this document is 
identified as Revision 2, dated December 12, 1976.
    (xiii) Lockheed TriStar L-1011 Service Bulletin 093-53-086, 
Revision 4, dated July 8, 1985. Pages 1-4, 15, and 16 of this 
document are identified as Revision 4, dated July 8, 1985. Pages 5, 
6, 8, 9, and 12-14 of this document are identified as Basic Issue, 
dated September 26, 1975. Pages 7, 10, and 11 of this document are 
identified as Revision 3, dated July 19, 1977.
    (xiv) Lockheed TriStar L-1011 Service Bulletin 093-53-086, 
Revision 5, dated April 12, 1990. Pages 1-9 and 13 of this document 
are identified as Revision 5, dated April 12, 1990. Pages 10-12 of 
this document are identified as Basic Issue, dated September 26, 
1975. Page 14 of this document is identified as Revision 4, dated 
July 8, 1985.
    (xv) Lockheed TriStar L-1011 Service Bulletin 093-53-110, Basic 
Issue, dated August 19, 1991.
    (xvi) Lockheed TriStar L-1011 Service Bulletin 093-53-110, 
Revision 1, dated May 7, 1993. Pages 1-7 and 9-12 of this document 
are identified as Revision 1, dated May 7, 1993. Page 8 of this 
document is identified as Basic Issue, dated August 19, 1991.
    (xvii) Lockheed TriStar L-1011 Service Bulletin 093-53-260, 
Basic Issue, dated May 15, 1991.
    (xviii) Lockheed TriStar L-1011 Service Bulletin 093-53-266, 
Basic Issue, dated March 2, 1992.

[[Page 52847]]

    (xix) Lockheed TriStar L-1011 Service Bulletin 093-57-058, Basic 
Issue, dated September 16, 1975.
    (xx) Lockheed TriStar L-1011 Service Bulletin 093-57-058, 
Revision 1, dated December 1, 1976. Pages 1, 2, 4, 7, 8, 11, and 15-
19 of this document are identified as Revision 1, dated December 1, 
1976. Pages 3, 5, 6, 9, 10, and 12-14 of this document are 
identified as Basic Issue, dated September 16, 1975.
    (xxi) Lockheed TriStar L-1011 Service Bulletin 093-57-058, 
Revision 2, dated June 30, 1978. Pages 1-4, 7, 8, 11, and 15-19 of 
this document are identified as Revision 2, dated June 30, 1978. 
Pages 5, 6, 9, 10, and 12-14 of this document are identified as 
Basic issue, dated September 16, 1975.
    (xxii) Lockheed TriStar L-1011 Service Bulletin 093-57-058, 
Revision 3, dated October 19, 1978. Pages 1-3, 7, 8, 11, and 15-19 
of this document are identified as Revision 3, dated October 19, 
1978. Page 4 of this document is identified as Revision 2, dated 
June 30, 1978. Pages 5, 6, 9, 10, and 12-14 of this document are 
identified as Basic Issue, dated September 16, 1975.
    (xxiii) Lockheed TriStar L-1011 Service Bulletin 093-57-058, 
Revision 4, dated July 6, 1981. Pages 1-3 and 19 of this document 
are identified as Revision 4, dated July 6, 1981. Pages 4 and 15 of 
this document are identified as Revision 2, dated June 30, 1978. 
Pages 5, 6, 9, 10, and 12-14 of this document are identified as 
Basic Issue, dated September 16, 1975. Pages 7, 8, 11, and 16-18 of 
this document are identified as Revision 3, dated October 19, 1978.
    (xxiv) Lockheed TriStar L-1011 Service Bulletin 093-57-058, 
Revision 5, dated June 9, 1983. Pages 1, 3, 4, and 7 of this 
document are identified as Revision 5, dated June 9, 1983. Page 2 of 
this document is identified as Revision 4, dated July 6, 1981. Pages 
5, 6, 9, 10, and 12-14 of this document are identified as Basic 
Issue, dated September 16, 1975. Pages 8, 11, and 16-19 of this 
document are identified as Revision 3, dated October 19, 1978. Page 
15 of this document is identified as Revision 2, dated June 30, 
1978.
    (xxv) Lockheed TriStar L-1011 Service Bulletin 093-57-085, Basic 
Issue, dated May 7, 1993. This document was incorrectly identified 
as ``Revision 1'' in the ``Service bulletin'' column of Table 2--
Material Incorporated by Reference in AD 2005-15-01, Amendment 39-
14190 (70 FR 42262, July 22, 2005).
    (xxvi) Lockheed TriStar L-1011 Service Bulletin 093-57-085, 
Revision 1, dated December 1, 1997. Pages 1-7, 9, and 10 of this 
document are identified as Revision 1, dated December 1, 1997. Pages 
8 and 11-17 are identified as Basic issue, dated May 7, 1993.
    (5) For Lockheed service information identified in this AD, 
contact Lockheed Martin Corporation/Lockheed Martin Aeronautics 
Company, L1011 Technical Support Center, Dept. 6A4M, Zone 0579, 86 
South Cobb Drive, Marietta, GA 30063-0579; telephone 770-494-5444; 
fax 770-494-5445; email L1011.support@lmco.com; Internet http://www.lockheedmartin.com/ams/tools/TechPubs.html.
    (6) You may view this service information at FAA, Transport 
Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For 
information on the availability of this material at the FAA, call 
425-227-1221.
    (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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.


    Issued in Renton, Washington, on July 21, 2013.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2013-20731 Filed 8-26-13; 8:45 am]
BILLING CODE 4910-13-P