Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations 52841 

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 

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: 


pmangrum on DSK3VPTVN1PROD with RULES
52842 Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. operators 

Inspections [retained actions 

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.

$0 $10,965 per inspection cycle. $285,090 per inspection 

cycle. 

Modification [retained action 

from AD 2005–15–01, 

Amendment 39–14190 (70 

FR 42262, July 22, 2005)].

614 work-hours × $85 per 

hour = $52,190.

$142,275 $194,465 ................................ $5,056,090. 

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 

■ 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. 

(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. 


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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’’) Repetitive 

intervals 

Terminating 

action 

Inspection threshold Grace period 

(1) 093–53–269, Revision 

1, dated October 28, 

1997.

Before the accumulation of 

8,000 total flight cycles 

or 15,000 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.

At intervals not to exceed 

6,450 flight cycles or 5 

years, whichever occurs 

first.

(None). 

(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)).

(None) ............................... At intervals not to exceed 

14 months.

(None). 

(3) 093–53–275, dated December 10, 1996.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) ............................... (None) ............................... (None). 

(4) 093–53–276, dated 

June 17, 1996.

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)).

(None) ............................... At intervals not to exceed 

the next CPCP inspection.

(None). 

(5) 093–57–085, Revision 

1, dated December 1, 

1997.

Before the accumulation of 

26,000 total flight cycles 

or 48,000 total flight 

hours, whichever occurs 

first.

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.

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. 

(6) 093–57–208, Revision 

1, dated October 28, 

1997.

Before the accumulation of 

18,000 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.

At intervals not to exceed 

6,450 flight cycles or 5 

years, whichever occurs 

first.

(None). 

(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.

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.

(None) ............................... (None) ............................... (None). 

(8) 093–53–054, Revision 

1, dated August 12, 

1975.

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) ............................... (None) ............................... (None). 


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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 

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.

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. 

(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 I: At intervals not to 

exceed 1,600 flight cycles or 3,000 flight 

hours, whichever occurs 

first.

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. 

(ii) Part II: Before the accumulation of 30,000 

flight cycles or 55,000 

total flight hours, 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.

Part II: At intervals not to 

exceed 5,000 flight cycles or 9,200 flight 

hours, whichever occurs 

first.

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. 

(11) 093–53–086, Revision 

5, dated April 12, 1990.

Before the accumulation of 

9,000 flight cycles or 

10,000 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.

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. 

(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.

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.

At intervals not to exceed 

2,200 flight cycles or 

4,000 flight hours, 

whichever occurs first.

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. 

(13) Change Notification 

093–53–260, CN4, dated 

May 8, 1998.

Before the accumulation of 

8,000 total flight cycles 

or 20,000 total flight 

hours, 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.

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. 

(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)).

(None) ............................... 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. 


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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 

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.

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. 

(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.

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. 

(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.

At intervals not to exceed 

6,450 flight cycles or 5 

years, whichever occurs 

first.

Repair or modification in 

accordance with Lockheed TriStar L–1011 

Service Bulletin 093–57– 

213, Basic Issue, dated 

December 9, 1994. 

(ii) For Model L–1011– 

385–3: Before the accumulation of 10,000 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.

At intervals not to exceed 

6,450 flight cycles or 5 

years, whichever occurs 

first.

Repair or modification in 

accordance with Lockheed TriStar L–1011 

Service Bulletin 093–57– 

213, Basic Issue, dated 

December 9, 1994. 

(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 


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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. 

(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. 


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Federal Register / Vol. 78, No. 166 / Tuesday, August 27, 2013 / Rules and Regulations 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/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 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: 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: 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: 

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. 

The Rule 

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 


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