Federal Register / Vol. 78, No. 189 / Monday, September 30, 2013 / Rules and Regulations 59805 

‘‘Compliance,’’ of Boeing Special Attention 

Service Bulletin 737–53–1294, Revision 1, 

dated June 14, 2013: Do detailed and high 

frequency eddy current (HFEC) inspections 

of the skin for cracking in the area around the 

eight fasteners securing the STA 540 

bulkhead chords between stringers S–22 and 

S–23, and do all applicable corrective 

actions, in accordance with Parts 1, 2, 3, 4, 

and 5 of the Accomplishment Instructions of 

Boeing Special Attention Service Bulletin 

737–53–1294, Revision 1, dated June 14, 

2013, except as required by paragraphs (i)(1) 

and (i)(4) of this AD. If no cracking is found, 

repeat the detailed and HFEC inspections at 

the intervals specified in table 1 of paragraph 

1.E., ‘‘Compliance,’’ of Boeing Special 

Attention Service Bulletin 737–53–1294, 

Revision 1, dated June 14, 2013, except as 

required by paragraph (g)(2) of this AD, until 

the optional preventive modification 

specified in paragraph (h) of this AD is done. 

Do all applicable corrective actions before 

further flight. 

(2) For airplanes that have incorporated 

Boeing Business Jet Lower Cabin Altitude 

Supplemental Type Certificate (STC) 

ST01697SE (http://rgl.faa.gov/Regulatory_

and_Guidance_Library/rgstc.nsf/0/

0812969A86AF879B8625766400600105?

OpenDocument&Highlight=st01697se) (6,500 

feet maximum cabin altitude in lieu of 8,000 

feet), the flight-cycle related compliance 

times are different from those specified in 

Boeing Special Attention Service Bulletin 

737–53–1294, Revision 1, dated June 14, 

2013. All initial compliance times specified 

in total flight cycles or flight cycles must be 

reduced to half of those specified in Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013. All 

repetitive interval compliance times 

specified in flight cycles must be reduced to 

one-quarter of those specified in Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013. 

(h) Optional Preventive Modification 

Accomplishing the preventive 

modification, including an HFEC inspection 

for cracking of the skin and STA 540 

bulkhead chords, and all applicable repairs, 

in accordance with paragraph 3.B, Part 2 or 

Part 4 (left side), and Part 3 or Part 5 (right 

side), of the Accomplishment Instructions of 

Boeing Special Attention Service Bulletin 

737–53–1294, Revision 1, dated June 14, 

2013, terminates the inspection requirements 

of paragraph (g) of this AD for the side on 

which the modification is done, except as 

required by paragraphs (i)(1) and (i)(4) of this 

AD. 

(i) Exceptions to Service Bulletin 

Specifications 

(1) If any cracking is found during any 

inspection required by this AD, and Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013, 

specifies to contact Boeing for appropriate 

action: Before further flight, repair using a 

method approved in accordance with the 

procedures specified in paragraph (l) of this 

AD. 

(2) Where Boeing Special Attention Service 

Bulletin 737–53–1294, Revision 1, dated June 

14, 2013, specifies to do the action after the 

original issue date of that service bulletin, 

this AD requires the compliance time after 

the effective date of this AD. 

(3) Where the Condition column of table 1 

of paragraph 1.E., ‘‘Compliance,’’ of Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013, 

specifies a condition as of the original issue 

date of that service bulletin, this AD specifies 

the condition as of the effective date of this 

AD. 

(4) The access and restoration instructions 

identified in the Work Instructions of Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013, are not 

required by this AD. Operators may perform 

those actions in accordance with approved 

maintenance procedures. 

(j) Post-Repair Inspections 

The post-repair inspections, specified in 

table 2 of paragraph 1.E., ‘‘Compliance,’’ of 

Boeing Special Attention Service Bulletin 

737–53–1294, Revision 1, dated June 14, 

2013, are not required by this AD. 

Note 1 to paragraph (j) of this AD: The 

damage tolerance inspections specified in 

table 2 of paragraph 1.E., ‘‘Compliance,’’ of 

Boeing Special Attention Service Bulletin 

737–53–1294, Revision 1, dated June 14, 

2013, may be used in support of compliance 

with Section 121.1109(c)(2) or 129.109(b)(2) 

of the Federal Aviation Regulations (14 CFR 

121.1109(c)(2) or 14 CFR 129.109(b)(2)). The 

corresponding actions specified in the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 737–53– 

1294, Revision 1, dated June 14, 2013, are not 

required by this AD. 

(k) Credit for Previous Actions 

This paragraph provides credit for the 

actions required by paragraphs (g), (h), and 

(j) of this AD, if those actions were performed 

before the effective date of this AD using 

Boeing Special Attention Service Bulletin 

737–53–1294, dated March 31, 2011, which 

is not incorporated by reference in this AD. 

(l) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle 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, it may be emailed 

to: 9-ANM-Seattle-ACO-AMOC-Requests@

faa.gov. 

(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. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair 

required by this AD if it is approved by the 

Boeing Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Seattle 

Aircraft Certification Office (ACO) to make 

those findings. For a repair method to be 

approved, the repair must meet the 

certification basis of the airplane and the 

approval must specifically refer to this AD. 

(m) Related Information 

(1) For more information about this AD, 

contact Alan Pohl, Aerospace Engineer, 

Airframe Branch, ANM–120S, FAA, Seattle 

Aircraft Certification Office, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

phone: 425–917–6450; fax: 425–917–6590; 

email: alan.pohl@faa.gov. 

(2) Service information referenced in this 

AD that is not incorporated by reference in 

this AD may be obtained at the addresses 

identified in paragraphs (n)(3) and (n)(4) of 

this AD. 

(n) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Boeing Special Attention Service 

Bulletin 737–53–1294, Revision 1, dated June 

14, 2013. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Data & Services 

Management, P. O. Box 3707, MC 2H–65, 

Seattle, WA 98124–2207; telephone 206– 

544–5000, extension 1; fax 206–766–5680; 

Internet https://www.myboeingfleet.com. 

(4) You may view this service information 

at FAA, Transport Airplane Directorate, 1601 

Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Renton, Washington, on 

September 9, 2013. 

Jeffrey E. Duven, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2013–22676 Filed 9–27–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2013–0517; Airspace 

Docket No. 13–ANM–15] 

Establishment of Class E Airspace; 

Cody, WY 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

mstockstill on DSK4VPTVN1PROD with RULES

59806 Federal Register / Vol. 78, No. 189 / Monday, September 30, 2013 / Rules and Regulations 

SUMMARY: This action establishes Class 

E airspace at the Cody VHF OmniDirectional Radio Range/Distance 

Measuring Equipment (VOR/DME) 

navigation aid, Cody, WY, to facilitate 

vectoring of Instrument Flight Rules 

(IFR) aircraft under control of Salt Lake 

City Air Route Traffic Control Center 

(ARTCC). This improves the safety and 

management of IFR operations within 

the National Airspace System. 

DATES: Effective date, 0901 UTC, 

December 12, 2013. The Director of the 

Federal Register approves this 

incorporation by reference action under 

1 CFR Part 51, subject to the annual 

revision of FAA Order 7400.9 and 

publication of conforming amendments. 

FOR FURTHER INFORMATION CONTACT: 

Eldon Taylor, Federal Aviation 

Administration, Operations Support 

Group, Western Service Center, 1601 

Lind Avenue SW., Renton, WA, 98057; 

telephone (425) 203–4537. 

SUPPLEMENTARY INFORMATION: 

History 

On July 3, 2013, the FAA published 

in the Federal Register a notice of 

proposed rulemaking (NPRM) to 

establish controlled airspace at Cody, 

WY (78 FR 40078). Interested parties 

were invited to participate in this 

rulemaking effort by submitting written 

comments on the proposal to the FAA. 

No comments were received. 

Class E airspace designations are 

published in paragraph 6006, of FAA 

Order 7400.9X dated August 7, 2013, 

and effective September 15, 2013, which 

is incorporated by reference in 14 CFR 

Part 71.1. The Class E airspace 

designations listed in this document 

will be published subsequently in that 

Order. 

The Rule 

This action amends Title 14 Code of 

Federal Regulations (14 CFR) Part 71 by 

establishing Class E en route domestic 

airspace extending upward from 1,200 

feet above the surface, at the Cody VOR/ 

DME navigation aid, Cody, WY, to 

accommodate IFR aircraft under control 

of Salt Lake City ARTCC by vectoring 

aircraft from en route airspace to 

terminal areas. This action ensures the 

safety and management of IFR 

operations. 

The FAA has determined this 

regulation only involves an established 

body of technical regulations for which 

frequent and routine amendments are 

necessary to keep them operationally 

current. Therefore, this regulation: (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); and (3) 

does not warrant preparation of a 

regulatory evaluation as the anticipated 

impact is so minimal. Since this is a 

routine matter that only affects air traffic 

procedures and air navigation, it is 

certified this rule, when promulgated, 

does not have a significant economic 

impact on a substantial number of small 

entities under the criteria of the 

Regulatory Flexibility Act. The FAA’s 

authority to issue rules regarding 

aviation safety is found in Title 49 of the 

U.S. Code. Subtitle 1, Section 106 

discusses the authority of the FAA 

Administrator. Subtitle VII, Aviation 

Programs, describes in more detail the 

scope of the agency’s authority. This 

rulemaking is promulgated under the 

authority described in Subtitle VII, Part 

A, Subpart I, Section 40103. Under that 

section, the FAA is charged with 

prescribing regulations to assign the use 

of airspace necessary to ensure the 

safety of aircraft and the efficient use of 

airspace. This regulation is within the 

scope of that authority as it establishes 

controlled airspace at the Cody VOR/

DME, Cody WY. 

Environmental Review 

The FAA has determined that this 

action qualifies for categorical exclusion 

under the National Environmental 

Policy Act in accordance with FAA 

Order 1050.1E, ‘‘Environmental 

Impacts: Policies and Procedures,’’ 

paragraph 311a. This airspace action is 

not expected to cause any potentially 

significant environmental impacts, and 

no extraordinary circumstances exist 

that warrant preparation of an 

environmental assessment. 

List of Subjects in 14 CFR Part 71 

Airspace, Incorporation by reference, 

Navigation (air) 

Adoption of the Amendment 

In consideration of the foregoing, the 

Federal Aviation Administration 

amends 

14 CFR Part 71 as follows: 

PART 71—DESIGNATION OF CLASS A, 

B, C, D AND E AIRSPACE AREAS; AIR 

TRAFFIC SERVICE ROUTES; AND 

REPORTING POINTS 

■ 1. The authority citation for 14 CFR 

Part 71 continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40103, 40113, 

40120; E. O. 10854, 24 FR 9565, 3 CFR, 1959– 

1963 Comp., p. 389. 

§ 71.1 [Amended] 

■ 2. The incorporation by reference in 

14 CFR Part 71.1 of the Federal Aviation 

Administration Order 7400.9X, Airspace 

Designations and Reporting Points, 

dated August 7, 2013, and effective 

September 15, 2013 is amended as 

follows: 

Paragraph 6006 En Route Domestic 

Airspace Areas. 

* * * * * 

ANM WY E6 Cody, WY [New] 

Cody VOR/DME, WY 

(Lat. 44°37′14′′ N., long. 108°57′54′′ W.) 

That airspace extending upward from 

1,200 feet above the surface within an area 

bounded by lat. 44°09′15′′ N., long. 

110°08′46′′ W.; to lat. 44°19′00′′ N., long. 

112°04′36′′ W.; to lat. 44°39′25′′ N., long. 

111°52′32′′ W.; to lat. 45°32′41′′ N., long. 

111°17′39′′ W.; to lat. 45°34′50′′ N., long. 

109°56′10′′ W.; to lat. 45°03′06′′ N., long. 

109°22′15′′ W.; to lat. 44°43′20′′ N., long. 

108°52′32′′ W.; to lat. 45°08′46′′ N., long. 

107°33′33′′ W.; to lat. 46°00′00′′ N., long. 

106°58′05′′ W.; to lat. 45°48′16′′ N., long. 

106°34′25′′ W.; to lat. 44°38′58′′ N., long. 

106°53′16′′ W.; to lat. 44°09′12′′ N., long. 

108°02′32′′ W.; to lat. 42°52′37′′ N., long. 

107°47′58′′ W.; to lat. 42°15′53′′ N., long. 

108°06′44′′ W.; to lat. 41°26′15′′ N., long. 

109°19′46′′ W.; to lat. 41°41′49′′ N., long. 

109°29′35′′ W.; to lat. 43°09′38′′ N., long. 

110°26′52′′ W., thence to the point of 

beginning. 

Issued in Seattle, Washington, on 

September 19, 2013. 

Christopher Ramirez, 

Acting Manager, Operations Support Group, 

Western Service Center. 

[FR Doc. 2013–23668 Filed 9–27–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2012–1185; Airspace 

Docket No. 12–AAL–8] 

Establishment of Class E Airspace; 

White Mountain, AK 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action establishes Class 

E airspace at White Mountain Airport, 

White Mountain, AK, to accommodate 

aircraft using new Area Navigation 

(RNAV) Global Positioning System 

(GPS) standard instrument approach 

procedures at the airport. This improves 

the safety and management of 

Instrument Flight Rules (IFR) operations 

at the airport. 

DATES: Effective date, 0901 UTC, 

December 12, 2013. The Director of the 

Federal Register approves this 

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