Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations 30345 

implementing its Targeted Community 

Lending Plan; and 

(iv) Establish quantitative targeted 

community lending performance goals. 

(b) Notice. A Bank shall provide 

annually to each of its members a 

written notice: 

(1) Identifying CICA programs and 

other Bank activities that may provide 

opportunities for a member to meet the 

community support requirements and to 

engage in targeted community lending; 

and 

(2) Summarizing targeted community 

lending and affordable housing 

activities undertaken by members, 

housing associates, nonprofit housing 

developers, community groups, or other 

entities in the Bank’s district that may 

provide opportunities for a member to 

meet the community support 

requirements and to engage in targeted 

community lending. 

§ 1290.7 Bank Advisory Council Annual 

Reports. 

Each Annual Report submitted by a 

Bank’s Advisory Council to FHFA 

pursuant to section 10(j)(11) of the Bank 

Act (12 U.S.C. 1430(j)(11)) must include 

an analysis of the Bank’s targeted 

community lending and affordable 

housing activities. 

Dated: May 19, 2015. 

Melvin L. Watt, 

Director, Federal Housing Finance Agency. 

[FR Doc. 2015–12807 Filed 5–27–15; 8:45 am] 

BILLING CODE 8070–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0940; Directorate 

Identifier 2014–NE–15–AD; Amendment 39– 

18162; AD 2015–10–06] 

RIN 2120–AA64 

Airworthiness Directives; Lycoming 

Engines Reciprocating Engines (Type 

Certificate Previously Held by Textron 

Lycoming Division, AVCO Corporation) 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Lycoming TIO–540–AJ1A reciprocating 

engines. This AD was prompted by 

several reports of cracked engine 

exhaust pipes. This AD requires 

inspection of the engine exhaust pipes 

for cracks and replacement of the 

turbocharger mounting bracket. We are 

issuing this AD to prevent failure of the 

exhaust system due to cracking, which 

could lead to uncontrolled engine fire, 

harmful exhaust gases entering the 

cabin resulting in crew incapacitation, 

and damage to the airplane. 

DATES: This AD is effective July 2, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 2, 2015. 

ADDRESSES: For service information 

identified in this AD, contact Lycoming 

Engines, 652 Oliver Street, 

Williamsport, PA 17701; phone: 800– 

258–3279; fax: 570–327–7101; Internet: 

www.lycoming.com/Lycoming/

SUPPORT/TechnicalPublications/

ServiceBulletins.aspx. You may view 

this service information at the 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. It is also available on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2014–0940. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0940; 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: 

Norm Perenson, Aerospace Engineer, 

New York Aircraft Certification Office, 

FAA, Engine & Propeller Directorate, 

1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; phone: 516–228– 

7337; fax: 516–794–5531; email: 

norman.perenson@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain Lycoming TIO–540– 

AJ1A reciprocating engines. The NPRM 

published in the Federal Register on 

February 2, 2015 (80 FR 5489). The 

NPRM was prompted by several reports 

of cracked engine exhaust pipes. The 

NPRM proposed to require inspection of 

the engine exhaust pipes for cracks and 

replacement of the turbocharger 

mounting bracket. We are issuing this 

AD to prevent failure of the exhaust 

system due to cracking, which could 

lead to uncontrolled engine fire, 

harmful exhaust gases entering the 

cabin resulting in crew incapacitation, 

and damage to the airplane. 

Related Service Information Under CFR 

Part 51 

We reviewed Lycoming Engines 

Mandatory Service Bulletin No. 614A, 

dated October 10, 2014. This service 

bulletin describes procedures for 

exhaust system inspection and 

turbocharger mounting bracket 

replacement. It also provides for the 

return of the turbocharger mounting 

bracket to Lycoming. This service 

information is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section of this AD. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (80 

FR 5489, February 2, 2015) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this AD 

as proposed. 

Costs of Compliance 

We estimate that this AD affects about 

111 engines installed on airplanes of 

U.S. registry. We also estimate that it 

will take about 8 hours per engine to 

comply with this AD. The average labor 

rate is $85 per hour. Parts replacement 

will cost about $6,782 per engine. Based 

on these figures, we estimate the cost of 

this AD on U.S. operators to be 

$828,282. Our cost estimate is exclusive 

of possible warranty coverage. 

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 


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30346 Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations 

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 

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 to the extent that it justifies 

making a regulatory distinction, 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 adding 

the following new airworthiness 

directive (AD): 

2015–10–06 Lycoming Engines (Type 

Certificate previously held by Textron 

Lycoming Division, AVCO Corporation): 

Amendment 39–18162; Docket No. 

FAA–2014–0940; Directorate Identifier 

2014–NE–15–AD. 

(a) Effective Date 

This AD is effective July 2, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Lycoming TIO–540– 

AJ1A reciprocating engines listed by engine 

serial number (S/N) in Figure 1 to paragraph 

(c) of this AD and to any TIO–540–AJ1A 

reciprocating engine with a replacement 

turbocharger mounting bracket installed that 

was purchased between April 5, 2012 and 

May 29, 2014. 

FIGURE 1 TO PARAGRAPH (c)—LYCOMING TIO–540–AJ1A ENGINE S/NS

L–6748–61E L–13828–61E L–13832–61E L–13843–61E 

L–13817–61E L–13831–61E L–13833–61E L–13847–61E 

L–13819–61E L–13823–61E L–13839–61E L–13855–61E 

L–13856–61E L–13947–61E L–14011–61E RL–2551–61E 

L–13857–61E L–13948–61E L–14013–61E RL–2848–61E 

L–13866–61E L–13949–61E L–14014–61E RL–3450–61E 

L–13867–61E L–13950–61E L–14015–61E RL–4138–61E 

L–13873–61E L–13960–61E L–14017–61E RL–7243–61E 

L–13882–61E L–13961–61E L–14024–61E RL–7512–61E 

L–13883–61E L–13962–61E L–14025–61E RL–8435–61E 

L–13884–61E L–13967–61E L–14026–61E RL–8767–61E 

L–13885–61E L–13973–61E L–14028–61E RL–8914–61E 

L–13886–61E L–13975–61E L–14034–61E RL–8979–61E 

L–13895–61E L–13976–61E L–14054–61E RL–9399–61E 

L–13896–61E L–13979–61E L–14055–61E RL–9466–61E 

L–13898–61E L–13981–61E L–14056–61E RL–9618–61E 

L–13900–61E L–13983–61E L–14057–61E RL–9663–61E 

L–13902–61E L–13984–61E L–14062–61E RL–10098–61E 

L–13907–61E L–13993–61E L–14063–61E RL–10194–61E 

L–13913–61E L–13996–61E L–14066–61E RL–10249–61E 

L–13915–61E L–13997–61E L–14067–61E RL–10615–61E 

L–13930–61E L–13998–61E L–14069–61E RL–11011–61E 

L–13931–61E L–13999–61E L–14071–61E RL–12121–61E 

L–13934–61E L–14000–61E L–14076–61E RL–12163–61E 

L–13936–61E L–14001–61E L–14077–61E RL–12343–61E 

L–13938–61E L–14003–61E RL–1726–61E RL–13352–61E 

L–13939–61E L–14004–61E RL–1810–61E RL–13601–61E 

L–13946–61E L–14005–61E RL–1862–61E .......................................................

(d) Unsafe Condition 

This AD was prompted by several reports 

of cracked engine exhaust pipes. We are 

issuing this AD to prevent failure of the 

exhaust system due to cracking, which could 

lead to uncontrolled engine fire, harmful 

exhaust gases entering the cabin resulting in 

crew incapacitation, and damage to the 

airplane. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) For affected engines with an S/N listed 

in Figure 1 to paragraph (c) of this AD with 

400 hours or less time since new (TSN) or 

time since last overhaul (TSLO), and for any 

TIO–540–AJ1A reciprocating engine with a 

replacement turbocharger mounting bracket 

installed that was purchased between April 

5, 2012 and May 29, 2014, that has 

accumulated 400 hours or less time-inservice (TIS), within 25 hours after the 

effective date of this AD, replace the 

turbocharger mounting bracket with a part 

eligible for installation, and inspect the 

exhaust pipes for cracks. Use Lycoming 

Engines Mandatory Service Bulletin (MSB) 

No. 614A, dated October 10, 2014, Exhaust 

System Disassembly and Removal, 

paragraphs 1 through 22 to replace the 

bracket, and Exhaust System Inspection, 

paragraphs 1 through 5 to do the inspection. 


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Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations 30347 

(2) For affected engines with an S/N listed 

in Figure 1 to paragraph (c) of this AD with 

more than 400 hours TSN or TSLO, and for 

any TIO–540–AJ1A reciprocating engine with 

a replacement turbocharger mounting bracket 

installed that was purchased between April 

5, 2012 and May 29, 2014, that has 

accumulated more than 400 hours TIS, 

replace the turbocharger mounting bracket 

with a part eligible for installation, and 

inspect the exhaust pipes for cracks at the 

next engine overhaul, separation of the 

crankcase halves, or twelve years from the 

effective date of this AD, whichever comes 

first. Use Lycoming Engines MSB No. 614A, 

dated October 10, 2014, Exhaust System 

Disassembly and Removal, paragraphs 1 

through 22 to replace the bracket, and 

Exhaust System Inspection, paragraphs 1 

through 5 to do the inspection. 

(f) Installation Prohibition 

After the effective date of this AD, do not 

return to service any TIO–540–AJ1A engine 

with a turbocharger mounting bracket that 

was removed from an engine identified in 

Figure 1 to paragraph (c) of this AD or that 

was purchased between April 5, 2012 and 

May 29, 2014. 

(g) Credit for Previous Action 

(1) If, before the effective date of this AD, 

you replaced the turbocharger mounting 

bracket with one eligible for installation you 

may take credit for your prior corrective 

action. No further turbocharger mounting 

bracket replacement is required. 

(2) If, before the effective date of this AD, 

you performed the crack inspection using 

either of the following: 

(i) Lycoming Engines MSB No. 614A, dated 

October 10, 2014, Exhaust System Inspection, 

paragraphs 1 through 5, or 

(ii) Cessna Service Letter No. SEL–78–01, 

dated May 30, 2014, you may take credit for 

your prior corrective action. No further 

inspection is required. However, you must 

still replace the turbocharger mounting 

bracket. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, New York Aircraft 

Certification Office, FAA, may approve 

AMOCs to this AD. Use the procedures found 

in 14 CFR 39.19 to make your request. 

(i) Related Information 

For more information about this AD, 

contact Norm Perenson, Aerospace Engineer, 

New York Aircraft Certification Office, FAA, 

Engine & Propeller Directorate, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 11590; 

phone: 516–228–7337; fax: 516–794–5531; 

email: norman.perenson@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. 

(i) Lycoming Engines Mandatory Service 

Bulletin No. 614A, dated October 10, 2014. 

(ii) Reserved. 

(3) For Lycoming Engines service 

information identified in this AD, contact 

Lycoming Engines, 652 Oliver Street, 

Williamsport, PA 17701; phone: 800–258– 

3279; fax: 570–327–7101; Internet: 

www.lycoming.com/Lycoming/SUPPORT/

TechnicalPublications/ServiceBulletins.aspx. 

(4) 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. 

(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 Burlington, Massachusetts, on 

May 12, 2015. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2015–12651 Filed 5–27–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–1003; Directorate 

Identifier 2013–NE–33–AD; Amendment 39– 

18163; AD 2015–10–07] 

RIN 2120–AA64 

Airworthiness Directives; Turbomeca 

S.A. Turboshaft Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are superseding 

airworthiness directive (AD) 2014–01– 

01 for all Turbomeca S.A. Arrius 2F 

turboshaft engines. AD 2014–01–01 

required a one-time inspection of the 

ejector assembly nozzle of certain serial 

number (S/N) lubricating devices and, if 

a discrepancy was found, removal and 

replacement of the affected ejector 

assembly nozzle with a part eligible for 

installation. This AD requires the same 

action as AD 2014–01–01 and expands 

the list of affected S/N lubricating 

devices. This AD was prompted by the 

determination that additional 

lubricating devices, identifiable by S/N, 

may have an incorrect bonding of the 

nozzle on the ejector assembly. We are 

issuing this AD to prevent failure of the 

ejector assembly nozzle, which could 

lead to an in-flight shutdown (IFSD) of 

the engine, damage to the engine, and 

damage to the helicopter. 

DATES: This AD is effective June 12, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of June 12, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain other publication listed in 

this AD as of February 6, 2014 (79 FR 

3481, January 22, 2014). 

We must receive any comments on 

this AD by July 13, 2015. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590, 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

For service information identified in 

this AD, contact Turbomeca S.A., 40220 

Tarnos, France; phone: 33 (0)5 59 74 40 

00; telex: 570 042; fax: 33 (0)5 59 74 45 

15. You may view this service 

information at the 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. 

It is also available on the Internet at 

http://www.regulations.gov by searching 

for and locating Docket No. FAA–2013– 

1003. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2013– 

1003; 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 mandatory 

continuing airworthiness information, 

regulatory evaluation, any comments 

received, and other information. The 

address for the Docket Office (phone: 

800–647–5527) is in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Philip Haberlen, Aerospace Engineer, 


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