Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations 14299 

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) 

2014–04–14, Amendment 39–17773 (79 

FR 11699, March 3, 2014), and adding 

the following new AD: 

2015–05–05 Agusta S.p.A.: Amendment 39– 

18115; Docket No. FAA–2014–0579; 

Directorate Identifier 2014–SW–020–AD. 

(a) Applicability 

This AD applies to the following 

helicopters, certificated in any category: 

(1) Agusta S.p.A. (Agusta) Model A109S 

and AW109SP helicopters, with a main rotor 

lag damper assembly (lag damper), part 

number (P/N) 109–0112–39–103 or 109– 

0112–39–105, installed on rod end assembly, 

P/N M004–01H007–041 with a serial number 

(S/N) 1 through 202; or rod end assembly, P/ 

N M004–01H007–045 with a S/N 1RW 

through 202RW or 4964 through 5011. 

(2) Agusta Model A119 and AW119 MKII 

helicopters, with a lag damper, P/N 109– 

0112–05–105 or 109–0112–05–107, installed 

on rod end assembly, P/N 109–0112–11–101 

with a S/N 1 through 78; or rod end 

assembly, P/N 109–0112–11–105 with a S/N 

1RW through 78RW; or rod end assembly, P/ 

N M004–01H007–045 with a S/N 1RW 

through 202RW or 4964 through 5011. 

(b) Unsafe Condition 

This AD defines the unsafe condition as a 

crack in a rod end assembly, which could 

result in fracture of the rod end assembly, 

damage to the main rotor, and subsequent 

loss of control of the helicopter. 

(c) Affected ADs 

This AD supersedes AD 2014–04–14, 

amendment 39–17773 (79 FR 11699, March 

3, 2014). 

(d) Effective Date 

This AD becomes effective April 23, 2015. 

(e) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has 

already been accomplished prior to that time. 

(f) Required Actions 

(1) Within 25 hours time-in-service or the 

next time maintenance of the helicopter 

involves removing the rod end assembly, 

whichever occurs first, remove the rod end 

assembly from service. 

(2) Do not install a rod end assembly, P/ 

N M004–01H007–041 with a S/N 1 through 

202; P/N M004–01H007–045 with a S/N 1RW 

through 202RW or 4964 through 5011; P/N 

109–0112–11–101 with a S/N 1 through 78; 

or P/N 109–0112–11–105 with a S/N 1RW 

through 78RW, on any helicopter. 

(g) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Safety Management 

Group, FAA, may approve AMOCs for this 

AD. Send your proposal to: Robert Grant, 

Aviation Safety Engineer, Safety Management 

Group, FAA, 2601 Meacham Blvd., Fort 

Worth, Texas 76137; telephone (817) 222– 

5110; email robert.grant@faa.gov. 

(2) For operations conducted under a 14 

CFR part 119 operating certificate or under 

14 CFR part 91, subpart K, we suggest that 

you notify your principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office or 

certificate holding district office, before 

operating any aircraft complying with this 

AD through an AMOC. 

(h) Additional Information 

(1) AgustaWestland S.p.A. Bollettino 

Tecnico (BT) No. 109S–49, BT No. 109SP– 

052, and BT No. 119–50, all Revision A, and 

all dated December 3, 2013, which are not 

incorporated by reference, contain additional 

information about the subject of this AD. For 

service information identified in this AD, 

contact AgustaWestland, Product Support 

Engineering, Via del Gregge, 100, 21015 

Lonate Pozzolo (VA) Italy, ATTN: Maurizio 

D’Angelo; telephone 39–0331–664757; fax 

39–0331–664680; or at http://

www.agustawestland.com/technicalbulletins. You may review a copy of the 

service information at the FAA, Office of the 

Regional Counsel, Southwest Region, 2601 

Meacham Blvd., Room 663, Fort Worth, 

Texas 76137. 

(2) The subject of this AD is addressed in 

the European Aviation Safety Agency (EASA) 

AD No. 2013–0290, dated December 9, 2013. 

You may view the EASA AD on the Internet 

at http://www.regulations.gov in Docket No. 

FAA–2014–0579. 

(i) Subject 

Joint Aircraft Service Component (JASC) 

Code: 6200, Main Rotor System. 

Issued in Fort Worth, Texas, on March 4, 

2015. 

Bruce E. Cain, 

Acting Directorate Manager, Rotorcraft 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–05715 Filed 3–18–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–1001; Directorate 

Identifier 2014–CE–034–AD; Amendment 

39–18103; AD 2015–04–01] 

RIN 2120–AA64 

Airworthiness Directives; Short 

Brothers & Harland Ltd. Airplanes 

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 all Short Brothers & 

Harland Ltd. Model SC–7 Series 3 

airplanes. The amendment number in 

the Agency Identification Numbers in 

the preamble section of the AD is 

incorrect. Although no other part of the 

preamble or regulatory information has 

been corrected, we are publishing the 

entire rule in the Federal Register. 

DATES: This final rule is effective March 

30, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 


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14300 Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations 

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1001; or in person at 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 service information identified in 

this AD, contact Short Brothers & 

Harland Ltd. service information 

identified in this proposed AD, contact 

Airworthiness, Short Brothers PLC, P.O. 

Box 241, Airport Road, Belfast, BT3 9DZ 

Northern Ireland, United Kingdom; 

phone: +44–2890–462469, fax: 44– 

2890–733647, email: 

michael.mulholland@

aero.bombardier.com, internet: None; 

and for SAFRAN Messier-BuggattiDowty service information contact 

Messier-Dowty Limited, Cheltenham 

Road, Gloucester GL2 9QH, ENGLAND; 

phone: +44(0)1452 712424; fax: 

+44(0)1452 713821; email: americacsc@

safranmbd.com, Internet: http://

www.safranmbd.com. You may view 

this referenced service information at 

the FAA, Small Airplane Directorate, 

901 Locust, Kansas City, Missouri 

64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1001. 

FOR FURTHER INFORMATION CONTACT: 

Doug Rudolph, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329– 

4059; fax: (816) 329–4090; email: 

doug.rudolph@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2015–04–01, 

Amendment 39–18003 (80 FR 9382, 

February 23, 2015), currently requires a 

visual inspection of the NLG sliding 

tube and a fluorescent penetrant 

inspection of the sliding tube. If any 

crack is detected during either 

inspection, before further flight, obtain 

FAA-approved repair instructions 

approved specifically for compliance 

with this AD by reporting the findings, 

and incorporating those instructions for 

Short Brothers & Harland Ltd. Model 

SC–7 Series 3 airplanes, all serial 

numbers, certificated in any category. 

As published, the amendment number 

in the Agency Identification Numbers in 

the preamble section of the AD is 

incorrect. It has been corrected in this 

document. 

Although no other part of the 

preamble or regulatory information has 

been corrected, we are publishing the 

entire rule in the Federal Register. 

The effective date of this AD remains 

March 30, 2015. 

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 AD: 

2015–04–01 Short Brothers & Harland Ltd: 

Amendment 39–18103; Docket No. 

FAA–2014–1001; Directorate Identifier 

2014–CE–034–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective on March 30, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Short Brothers & 

Harland Ltd. Model SC–7 Series 3 airplanes, 

all serial numbers, certificated in any 

category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 32: Landing Gear. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

originated by an aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as fatigue 

cracking which could lead to structural 

failure of the nose landing gear (NLG). We are 

issuing this AD to detect and correct fatigue 

cracking which, if not detected and 

corrected, could lead to structural failure of 

the NLG, possibly resulting in loss of control 

of the airplane during take-off or landing. 

(f) Actions and Compliance 

Unless already done, comply with this AD 

within the compliance times specified in 

paragraphs (f)(1) through (f)(5) of this AD. 

(1) Within 30 days after March 30, 2015 

(the effective date of this AD), accomplish a 

visual inspection of the NLG sliding tube 

following the instructions of paragraph 3.A of 

SAFRAN Messier-Buggatti-Dowty Service 

Bulletin No. 32–17M, dated November 1, 

2014. 

Note 1 to paragraphs (f)(1), (f)(2), (f)(4), 

and (f)(5) of this AD: Instructions provided 

by SAFRAN Messier-Buggatti-Dowty Service 

Bulletin No. 32–17M, dated November 1, 

2014, are referenced in Shorts Service 

Bulletin Number 32–74, dated November 1, 

2014. 

(2) Within 90 days after March 30, 2015 

(the effective date of this AD), do a 

fluorescent penetrant inspection of the 

sliding tube following the instructions of 

paragraph 3.B of SAFRAN Messier-BuggattiDowty Service Bulletin No. 32–17M, dated 

November 1, 2014. 

(3) If any crack is detected during the 

inspection required by paragraph (f)(1) or 

(f)(2) of this AD, before further flight, obtain 

FAA-approved repair instructions approved 

specifically for compliance with this AD by 

reporting the findings to Short Brothers & 

Harland Ltd. and incorporating those 

instructions. You can find contact 

information for Short Brothers & Harland Ltd. 

in paragraph (h) of this AD. 

(4) Within 30 days after any inspection 

required by paragraphs (f)(1) and (f)(2) of this 

AD or within 30 days after March 30, 2015 

(the effective date of this AD), whichever 

occurs later, report the inspection results to 

Short Brothers & Harland Ltd. by completing 

the Inspection Results Proforma following 

the instructions of paragraph 3.C.(2) of 

SAFRAN Messier-Buggatti-Dowty Service 

Bulletin No. 32–17M, dated November 1, 

2014. You can find contact information for 

Short Brothers & Harland Ltd. in paragraph 

(h) of this AD. 

(5) From March 30, 2015 (the effective date 

of this AD), you may install a sliding tube on 

an NLG provided that, before next flight after 

installation, the NLG sliding tube passes the 

inspections in paragraphs (f)(1) and (f)(2) of 

this AD following the instructions of 

paragraph 3 of SAFRAN Messier-BuggattiDowty Service Bulletin No. 32–17M, dated 

November 1, 2014. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Doug Rudolph, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4059; fax: (816) 329– 

4090; email: doug.rudolph@faa.gov. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(2) Airworthy Product: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer or other source, 

use these actions if they are FAA-approved. 

Corrective actions are considered FAAapproved if they are approved by the State 

of Design Authority (or their delegated 

agent). You are required to assure the product 

is airworthy before it is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 


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Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations 14301 

1 29 CFR 2550.404a–5; 75 FR 64910. 

2 29 CFR 2550.404a–5(h)(1). 

3The specified applicability date was 

subsequently delayed by amendment published on 

July 19, 2011. 76 FR 42539. Under the amendment, 

the initial disclosures required on or before the date 

on which a participant or beneficiary can first direct 

his or her investments must be furnished no later 

than the later of 60 days after such applicability 

date or 60 days after the effective date of 29 CFR 

2550.408b–2(c). 29 CFR 2550.404a–5(j)(3)(i)(A). 

4FAB 2012–02R supersedes FAB 2012–02 issued 

on May 7, 2012. Changes in the superseding 

bulletin did not affect Question 35. 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(h) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No.: 2014–0246, dated 

November 12, 2014; and Shorts Service 

Bulletin Number 32–74, dated November 1, 

2014, for related information. The MCAI can 

be found in the AD docket on the Internet at: 

http://www.regulations.gov/

#!documentDetail;D=FAA-2014-1001-0002. 

For Short Brothers & Harland Ltd. service 

information identified in this AD, contact 

Airworthiness, Short Brothers PLC, P.O. Box 

241, Airport Road, Belfast, BT3 9DZ Northern 

Ireland, United Kingdom; phone: +44–2890– 

462469, fax: 44–2890–733647, email: 

michael.mulholland@aero.bombardier.com, 

internet: None. 

(i) 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) SAFRAN Messier-Buggatti-Dowty 

Service Bulletin No. 32–17M, dated 

November 1, 2014. 

(ii) Reserved. 

(3) For SAFRAN Messier-Buggatti-Dowty 

service information identified in this AD, 

contact Messier-Dowty Limited, Cheltenham 

Road, Gloucester GL2 9QH, ENGLAND; 

phone: +44(0)1452 712424; fax: +44(0)1452 

713821; email: americacsc@safranmbd.com, 

Internet: http://www.safranmbd.com. 

(4) You may view this service information 

at the FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. In 

addition, you can access this service 

information on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2014–1001. 

(6) 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 Kansas City, Missouri, on March 

11, 2015. 

Robert Busto, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–06235 Filed 3–18–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF LABOR 

Employee Benefits Security 

Administration 

29 CFR Part 2550 

RIN 1210–AB68 

Fiduciary Requirements for Disclosure 

in Participant-Directed Individual 

Account Plans—Timing of Annual 

Disclosure 

AGENCY: Employee Benefits Security 

Administration, Department of Labor. 

ACTION: Direct final rule. 

SUMMARY: This direct final rule amends 

the Department of Labor’s ‘‘participantlevel fee disclosure’’ regulation. The 

amendment makes a technical 

adjustment to a timing requirement in 

the current regulation. As amended, the 

regulation provides plan administrators 

with flexibility as to when they must 

furnish annual disclosures to 

participants and beneficiaries. 

DATES: Effective date: This rule is 

effective June 17, 2015, without further 

action or notice, unless significant 

adverse comment is received by April 

20, 2015. If significant adverse comment 

is received, the Employee Benefits 

Security Administration (EBSA) will 

publish a timely withdrawal of the rule 

in the Federal Register. 

Applicability date: The amendment is 

applicable to disclosures made on or 

after June 17, 2015. 

ADDRESSES: You may submit comments, 

identified by RIN 1210–AB68, by one of 

the following methods: 

• Federal eRulemaking Portal: http:// 

www.regulations.gov. Follow the 

instructions for submitting comments. 

• Email: e-ORI@dol.gov. Include RIN 

1210–AB68 in the subject line of the 

message. 

• Mail or personal delivery: Office of 

Regulations and Interpretations, 

Employee Benefits Security 

Administration, Room N–5655, U.S. 

Department of Labor, 200 Constitution 

Avenue NW., Washington, DC 20210. 

Instructions: All submissions received 

must include the agency name and 

Regulation Identifier Number (RIN) for 

this rulemaking. Comments received, 

including any personal information 

provided, will be posted without change 

to http://www.regulations.gov and 

http://www.dol.gov/ebsa, and made 

available for public inspection at the 

Public Disclosure Room, N–1513, 

Employee Benefits Security 

Administration, 200 Constitution 

Avenue NW., Washington, DC 20210. 

Persons submitting comments 

electronically are encouraged not to 

submit paper copies. 

FOR FURTHER INFORMATION CONTACT: Eric 

A. Raps, Office of Regulations and 

Interpretations, Employee Benefits 

Security Administration, Department of 

Labor, at (202) 693–8532. This is not a 

toll-free number. 

SUPPLEMENTARY INFORMATION: 

In General 

On October 20, 2010, the Department 

of Labor (Department) published a final 

regulation requiring plan administrators 

to disclose certain plan and investmentrelated information, including fee and 

expense information, to participants and 

beneficiaries in participant-directed 

individual account plans.1 The 

regulation requires certain information 

to be furnished on or before the date on 

which a participant can first direct his 

or her investments and ‘‘at least 

annually thereafter.’’ The regulation 

defines this term as ‘‘at least once in any 

12-month period, without regard to 

whether the plan operates on a calendar 

or fiscal year basis.’’ 2 The regulation 

was effective on December 20, 2010, but 

was not applicable until plan years 

beginning on or after November 1, 

2011.3

On July 30, 2012, the Department’s 

Employee Benefits Security 

Administration (EBSA) issued Field 

Assistance Bulletin 2012–02R (FAB 

2012–02R) providing guidance on 

frequently asked questions. Q&A 35 

clarified that, for most plans, including 

calendar year plans, the first initial 

disclosures under the new regulation 

were required no later than August 30, 

2012. FAB 2012–02R did not, however, 

specifically address the deadline for 

subsequent annual disclosures.4

In Field Assistance Bulletin 2013–02, 

issued July 22, 2013, the Department 

made clear that the regulation requires 

annual disclosures to be made no more 

than one year exactly (e.g., 365 days) 

after the prior annual disclosures. 

Specifically, FAB 2013–02, in relevant 

part, states ‘‘[f]or example, a plan 

administrator that furnished the first 

required chart on August 25, 2012, must 

furnish the next comparative chart no 


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