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: https:// 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 https://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 https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains 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 https://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: https:// 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 https://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 https://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains 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).

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 https://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: https://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

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