Federal Register / Vol. 80, No. 201 / Monday, October 19, 2015 / Rules and Regulations 63083 

Branch, ANM–116, Transport Airplane 

Directorate, 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 International Branch, send it to ATTN: 

Vladimir Ulyanov, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone 425–227–1138; fax 425–227–1149. 

Information may be emailed to: 9-ANM-116- 

AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter 

must specifically reference this AD. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the European Aviation Safety Agency 

(EASA); or Airbus’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(k) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2015–0183, dated 

August 31, 2015, for related information. You 

may examine the MCAI on the Internet at 

http://www.regulations.gov by searching for 

and locating Docket No. FAA–2015–4203. 

(l) 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 this AD specifies otherwise. 

(i) Airbus Alert Operators Transmission 

A25L004–15, Rev 00, dated August 24, 2015. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Airbus SAS, Airworthiness 

Office—EAL, 1 Rond Point Maurice Bellonte, 

31707 Blagnac Cedex, France; telephone +33 

5 61 93 36 96; fax +33 5 61 93 45 80; email 

airworthiness.A330-A340@airbus.com; 

Internet http://www.airbus.com. 

(4) You may view this service information 

at the 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 October 

11, 2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–26603 Filed 10–16–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0277; Directorate 

Identifier 2015–NE–05–AD; Amendment 39– 

18262; AD 2015–18–04] 

RIN 2120–AA64 

Airworthiness Directives; CFM 

International S.A. Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to certain CFM International 

S.A. (CFM) CFM56–7B and CFM56–3 

turbofan engines. Four headings in the 

Compliance section are incorrect. This 

document corrects the errors. In all 

other respects, the original document 

remains the same. 

DATES: This final rule is effective on 

October 20, 2015. The effective date of 

AD 2015–18–04, Amendment 39–18262 

(80 FR 55235, September 15, 2015) 

remains October 20, 2015. 

ADDRESSES: 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: Kyle 

Gustafson, Aerospace Engineer, Engine 

Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7183; fax: 781–238– 

7199; email: kyle.gustafson@faa.gov. 

SUPPLEMENTARY INFORMATION: AD 2015– 

18–04, Amendment 39–18262 (80 FR 

55235, September 15, 2015), requires 

AGB/transfer gearbox (TGB) magnetic 

chip detector (MCD) inspection of the 

affected gearshafts until removal. 

As published, four headings in the 

Compliance section are incorrect. 

No other part of the final rule has 

been changed. 

The effective date of AD 2015–18–04 

remains October 20, 2015. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

■ 2. The FAA republishes airworthiness 

directive (AD) 2015–18–04, Amendment 

39–18262 (80 FR 55235, September 15, 

2015) as follows: 

2015–18–04 CFM International S.A.: 

Amendment 39–18262; Docket No. 

FAA–2015–0277; Directorate Identifier 

2015–NE–05–AD. 

(a) Effective Date 

This AD is effective October 20, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to CFM International S.A. 

(CFM) CFM56–7B and CFM56–3 engines 

with a 73-tooth or 41-tooth gearshaft installed 

in the accessory gearbox (AGB), that has a 

gearshaft serial number in Appendix A or 

Appendix B of CFM Service Bulletin (SB) No. 

CFM56–7B S/B 72–0964, Revision 1, dated 

December 15, 2014. 

(d) Unsafe Condition 

This AD was prompted by a report of an 

uncommanded in-flight shutdown on a CFM 

CFM56–7B engine following rupture of the 

73-tooth gearshaft located in the engine AGB. 

We are issuing this AD to prevent failure of 

certain AGB gearshafts, which could lead to 

failure of one or more engines, loss of thrust 

control, and damage to the airplane. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) Initial AGB/Transfer Gearbox (TGB)/

Magnetic Chip Detector (MCD) Inspection 

and Analysis for CFM56–7B Engines 

(i) For affected 73-tooth gearshafts, perform 

an AGB/TGB MCD inspection within 250 

flight hours (FHs) since last inspection, 

within 25 FHs from the effective date of this 

AD, or when the gearshaft accumulates 3,000 

FHs since new, whichever comes later. 

(ii) For affected 41-tooth gearshafts, 

perform an AGB/TGB MCD inspection within 

250 FHs since last inspection, within 25 FHs 

from the effective date of this AD, or when 

the gearshaft accumulates 6,000 FHs since 

new, whichever comes later. 

(iii) If any magnetic particles, including 

fuzz, are seen, determine with laboratory 

analysis if the particles are 73-tooth or 41- 

tooth gearshaft material. 

(iv) If the particles are 73-tooth or 41-tooth 

gearshaft material, remove the affected 

gearshaft(s) within 75 FHs since the AGB/

TGB MCD inspection. 


asabaliauskas on DSK5VPTVN1PROD with FRONTMATTER
63084 Federal Register / Vol. 80, No. 201 / Monday, October 19, 2015 / Rules and Regulations 

(2) Repetitive AGB/TGB MCD Inspection and 

Analysis for CFM56–7B Engines 

(i) For affected 73-tooth gearshafts, perform 

an AGB/TGB MCD inspection and laboratory 

analysis within every 500 FHs since the last 

AGB/TGB MCD inspection until affected 

gearshaft is removed. 

(ii) For affected 41-tooth gearshafts, 

perform an AGB/TGB MCD inspection and 

laboratory analysis within every 500 FHs 

since the last AGB/TGB MCD inspection 

until affected gearshaft is removed. 

(iii) If any magnetic particles, including 

fuzz, are seen, determine with laboratory 

analysis if the particles are 73-tooth or 41- 

tooth gearshaft material. 

(iv) If the particles are 73-tooth or 41-tooth 

gearshaft material, remove the affected 

gearshaft(s) within 75 FHs since the AGB/

TGB MCD inspection. 

(f) Mandatory Terminating Action for 

CFM56–7B Engines 

(1) Remove the affected 73-tooth gearshaft 

prior to the gearshaft accumulating 6,000 FHs 

since new or within 50 FHs after the effective 

date of this AD, whichever comes later. 

(2) Remove the affected 41-tooth gearshaft 

prior to the gearshaft accumulating 9,000 FHs 

since new or within 50 FHs after the effective 

date of this AD, whichever comes later. 

(g) Installation Prohibition for CFM56–3 and 

CFM56–7B Engines 

After the effective date of this AD, do not 

install an affected gearshaft into an AGB. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs for this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. You may email your 

request to: ANE-AD-AMOC@faa.gov. 

(i) Related Information 

For more information about this AD, 

contact Kyle Gustafson, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7183; fax: 781–238–7199; 

email: kyle.gustafson@faa.gov. 

(j) 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 20, 2015. 

(i) CFM International Service Bulletin No. 

CFM56–7B S/B 72–0964, Revision 1, dated 

December 15, 2014. 

(ii) Reserved. 

(4) For CFM service information identified 

in this AD, contact CFM International Inc., 

Aviation Operations Center, 1 Neumann 

Way, M/D Room 285, Cincinnati, OH 45125; 

phone: 877–432–3272; fax: 877–432–3329; 

email: aviation.fleetsupport@ge.com. 

(5) You may view this service information 

at FAA, Engine & Propeller Directorate, 12 

New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(6) You may view this service information 

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 Burlington, Massachusetts, on 

October 6, 2015. 

Ann C. Mollica, 

Acting Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2015–26345 Filed 10–16–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2015–1835; Airspace 

Docket No. 14–AGL–7] 

Establishment of Class E Airspace; 

Hart/Shelby, MI 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action establishes Class 

E airspace at Hart/Shelby, MI. 

Controlled airspace is necessary to 

accommodate new Standard Instrument 

Approach Procedures (SIAPs) at Oceana 

County Airport. The FAA is proposing 

this action to enhance the safety and 

management of Instrument Flight Rules 

(IFR) operations at the airport. 

DATES: Effective 0901 UTC, December 

10, 2015. The Director of the Federal 

Register approves this incorporation by 

reference action under title 1, Code of 

Federal Regulations, part 51, subject to 

the annual revision of FAA Order 

7400.9 and publication of conforming 

amendments. 

ADDRESSES: FAA Order 7400.9Z 

Airspace Designations and Reporting 

Points and subsequent amendments can 

be viewed on line at http://

www.faa.gov/air_traffic/publications. 

For further information, you can contact 

the Airspace Policy and ATC 

Regulations Group, Federal Aviation 

Administration, 800 Independence 

Avenue SW., Washington, DC 29591; 

telephone: 202–267–8783. The order is 

also available for inspection 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/code_of_federalregulations/ibr_locations.html. 

FAA Order 7400.9, Airspace 

Designations and Reporting Points, is 

published yearly and effective on 

September 15. 

FOR FURTHER INFORMATION CONTACT: 

Rebecca Shelby, Central Service Center, 

Operations Support Group, Federal 

Aviation Administration, Southwest 

Region, 10101 Hillwood Parkway, Fort 

Worth, TX 76177; telephone: 817–222– 

5857. 

SUPPLEMENTARY INFORMATION: 

Authority for This Rulemaking 

The FAA’s authority to issue rules 

regarding aviation safety is found in 

Title 49 of the United States Code. 

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. 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 

Class E airspace at Oceana County 

Airport, Hart/Shelby, MI. 

History 

On July 28, 2015, the FAA published 

in the Federal Register a notice of 

proposed rulemaking (NPRM) to 

establish Class E airspace extending 

upward from 700 feet above the surface 

at Oceana County Airport, Hart/Shelby, 

MI., (80 FR 44895). 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 6005 of FAA 

Order 7400.9Z, dated August 6, 2015, 

and effective September 15, 2015, 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 the 

Order. 

Availability and Summary of 

Documents for Incorporation by 

Reference 

This document amends FAA Order 

7400.9Z, airspace Designations and 

Reporting Points, dated August 6, 2015, 

and effective September 15, 2015. FAA 

Order 7400.9Z is publicly available as 

listed in the ADDRESSES section of this 

document. FAA Order 7400.9Z lists 

Class A, B, C, D, and E airspace areas, 


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