96362 Federal Register / Vol. 81, No. 251 / Friday, December 30, 2016 / Rules and Regulations 

of hydraulic systems with only HyJet V 

hydraulic fluid, in accordance with the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin B787–81205–SB270026–00, 

Issue 002, dated June 13, 2016. 

Note 1 to paragraph (g) of this AD: Boeing 

Alert Service Bulletin B787–81205– 

SB270026–00, Issue 002, dated June 13, 2016, 

refers to Boeing Service Bulletin B787– 

81205–SB290022–00, Issue 001, dated 

September 4, 2014, as an additional source of 

guidance for installing markers to allow 

servicing of hydraulic systems with only 

HyJet V hydraulic fluid. 

Note 2 to paragraph (g) of this AD: Task 

1, Figure 1, and Task 2, Figure 1, of Boeing 

Service Bulletin B787–81205–SB290022–00, 

Issue 001, dated September 4, 2014, identify 

P/N 710Z7290–9##ALT1 for the left and right 

engine diagonal braces; however, the correct 

P/N is 710Z7290–9 with no ##ALT suffix. 

(h) Fluid Tests of the Left, Right, and Center 

Hydraulic Systems 

For airplanes identified in Boeing Alert 

Service Bulletin B787–81205–SB270026–00, 

Issue 002, dated June 13, 2016, as Group 1, 

Configuration 2, Group 2: Within 36 months 

after the effective date of this AD, do 

hydraulic fluid tests of the left, right, and 

center hydraulic systems, replace the 

hydraulic system fluid, if necessary, and do 

all applicable related investigative and 

corrective actions, in accordance with the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin B787–81205–SB270026–00, 

Issue 002, dated June 13, 2016. Do all 

applicable related investigative and 

corrective actions within 36 months after the 

effective date of this AD. 

(i) Credit for Previous Actions 

This paragraph provides credit for the 

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

this AD, if those actions were performed 

before the effective date of this AD using 

Boeing Alert Service Bulletin B787–81205– 

SB270026–00, Issue 001, dated November 25, 

2014. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (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 

paragraph (k)(1) of this AD. Information may 

be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@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) For service information that contains 

steps that are labeled as Required for 

Compliance (RC), the provisions of 

paragraphs (j)(3)(i) and (j)(3)(ii) apply. 

(i) The steps labeled as RC, including 

substeps under an RC step and any figures 

identified in an RC step, must be done to 

comply with the AD. If a step or sub-step is 

labeled ‘‘RC Exempt,’’ then the RC 

requirement is removed from that step or 

sub-step. An AMOC is required for any 

deviations to RC steps, including substeps 

and identified figures. 

(ii) Steps not labeled as RC may be 

deviated from using accepted methods in 

accordance with the operator’s maintenance 

or inspection program without obtaining 

approval of an AMOC, provided the RC steps, 

including substeps and identified figures, can 

still be done as specified, and the airplane 

can be put back in an airworthy condition. 

(4) 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 

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. 

(k) Related Information 

(1) For more information about this AD, 

contact Fnu Winarto, Aerospace Engineer, 

Systems and Equipment Branch, ANM–130S, 

FAA, Seattle ACO, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; phone: 425–917– 

6659; fax: 425–917–6590; email: 

fnu.winarto@faa.gov. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (l)(4) and (l)(5) of this AD. 

(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. 

(3) The following service information was 

approved for IBR on January 20, 2017 (81 FR 

90955, December 16, 2016). 

(i) Boeing Alert Service Bulletin B787– 

81205–SB270026–00, Issue 002, dated June 

13, 2016. 

(ii) Reserved. 

(4) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Contractual & Data 

Services (C&DS), 2600 Westminster Blvd., 

MC 110–SK57, Seal Beach, CA 90740; 

telephone 562–797–1717; Internet https://

www.myboeingfleet.com. 

(5) 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. 

(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 Renton, Washington, on 

December 22, 2016. 

Robert D. Breneman, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–31693 Filed 12–29–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–3753; Directorate 

Identifier 2015–NE–26–AD; Amendment 39– 

18739; AD 2016–25–13] 

RIN 2120–AA64 

Airworthiness Directives; Safran 

Helicopter Engines, S.A. (Formerly 

Turbomeca S.A.) Turboshaft Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding 

airworthiness directive (AD) 2016–04– 

12, that applies to certain Safran 

Helicopter Engines, S.A. (formerly 

Turbomeca S.A.) Arriel 2B, 2B1, 2C, 

2C1, 2C2, 2D, 2E, 2S1, and 2S2 

turboshaft engines. AD 2016–04–12 

required spectrometric oil analysis 

(SOA) inspection of the engine 

accessory gearbox (AGB), and, 

depending on the results, removal of the 

engine AGB. This AD requires initial 

and repetitive wear inspections of the 

engine AGB cover. This AD was 

prompted by a report of an 

uncommanded in-flight shutdown 

(IFSD) of an Arriel 2S2 engine caused by 

rupture of the 41-tooth gear, which 

forms part of the bevel gear in the 

engine AGB. We are issuing this AD to 

correct the unsafe condition on these 

products. 

DATES: This AD is effective February 3, 

2017. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of February 3, 2017. 

ADDRESSES: For service information 

identified in this final rule, contact 

Safran Helicopter Engines, S.A. 40220 

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

00; fax: 33 0 5 59 74 45 15. You may 

view this service information at the 

FAA, Engine & Propeller Directorate, 

1200 District Avenue, 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 


srobinson on DSK5SPTVN1PROD with RULES
Federal Register / Vol. 81, No. 251 / Friday, December 30, 2016 / Rules and Regulations 96363 

searching for and locating Docket No. 

FAA–2015–3753. 

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–2015– 

3753; 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 

(MCAI), 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: 

Philip Haberlen, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 1200 District 

Avenue, Burlington, MA 01803; phone: 

781–238–7770; fax: 781–238–7199; 

email: philip.haberlen@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to supersede AD 2016–04–12, 

Amendment 39–18406 (81 FR 12583, 

March 10, 2016), (‘‘AD 2016–04–12’’). 

AD 2016–04–12 applied to the specified 

products. The NPRM published in the 

Federal Register on June 17, 2016 (81 

FR 39601). The NPRM proposed to 

require initial and repetitive 

spectrometric oil analysis (SOA) of the 

AGB, and wear inspections of the 

engine AGB cover. However, this AD 

only mandates wear inspections of the 

engine AGB cover and does not add 

requirements beyond the scope of the 

NPRM. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (81 

FR 39601, June 17, 2016). 

Since we issued AD 2016–04–12, the 

European Aviation Safety Agency 

(EASA) has issued MCAI European 

Aviation Safety Agency AD 2016– 

0055R1, dated October 11, 2016, to only 

specify that periodic wear inspections of 

the engine AGB cover are necessary. 

This AD removes the proposed 

requirements for initial and repetitive 

SOA of the AGB, which reduces the 

costs of compliance in this AD. 

Also since we issued AD 2016–04–12, 

Safran Helicopter Engines, S.A. has 

issued Mandatory Service Bulletin 

(MSB) No. 292 72 2861, Version D, 

dated September 23, 2016. The MSB 

only requires performing periodic wear 

inspections of the engine AGB cover. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting this AD 

with the changes described previously. 

We determined that these changes will 

not increase the economic burden on 

any operator or increase the scope of 

this AD. 

Related Service Information Under 

1 CFR Part 51 

Safran Helicopter Engines, S.A. has 

issued MSB No. 292 72 2861, Version D, 

dated September 23, 2016. The MSB 

describes procedures for performing 

periodic wear inspections of the engine 

AGB cover. 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. 

Costs of Compliance 

We estimate that this AD affects 250 

engines installed on helicopters of U.S. 

registry. We also estimate that it will 

take 1 hour to perform the engine AGB 

cover wear inspection. The average 

labor rate is $85 per hour. Required 

parts for the wear inspection cost about 

$3,100 per engine. We estimate that 5 

engines will require AGB replacement at 

a cost of $44,397 per engine. We also 

estimate that it will take about 2 hours 

to replace the engine AGB. Based on 

these figures, we estimate the cost of 

this AD on U.S. operators to be 

$1,019,085. 

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 

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 part 39 of the Federal 

Aviation Regulations (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) 

AD 2016–04–12, Amendment 39–18406 

(81 FR 12583, March 10, 2016), and 

adding the following new AD: 

2016–25–13 Safran Helicopter Engines, 

S.A. (Type Certificate previously held by 

Turbomeca S.A.): Amendment 39– 

18739; Docket No. FAA–2015–3753; 

Directorate Identifier 2015–NE–26–AD. 

(a) Effective Date 

This AD is effective February 3, 2017. 

(b) Affected ADs 

This AD supersedes AD 2016–04–12, 

Amendment 39–18406 (81 FR 12583, March 

10, 2016). 


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96364 Federal Register / Vol. 81, No. 251 / Friday, December 30, 2016 / Rules and Regulations 

(c) Applicability 

This AD applies to Safran Helicopter 

Engines, S.A. Arriel 2B, 2B1, 2C, 2C1, 2C2, 

2D, 2E, 2S1, and 2S2 turboshaft engines with 

an engine accessory gearbox (AGB), part 

number 0292120650, with a machined front 

casing. 

(d) Unsafe Condition 

This AD was prompted by a report of an 

uncommanded in-flight shutdown (IFSD) of 

an Arriel 2S2 engine caused by rupture of the 

41-tooth gear, which forms part of the bevel 

gear in the engine AGB. We are issuing this 

AD to prevent failure of the engine AGB, 

uncommanded IFSD, damage to the engine, 

and damage to the helicopter. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) Initial Wear Inspection 

(i) For all affected engines, perform a wear 

inspection of the engine AGB cover before 

the engine AGB, module M01, exceeds 850 

engine hours (EH) since new or since last 

overhaul (SLO), or within 50 EHs after April 

14, 2016, or before the next flight after the 

effective date of this AD, whichever occurs 

latest. 

(ii) Reserved. 

(2) Repetitive Wear Inspection Intervals 

(i) For Arriel 2E engines, repeat the engine 

AGB cover wear inspection within every 800 

EH since last inspection (SLI). 

(ii) For all affected engines, except for 

Arriel 2E engines, repeat the engine AGB 

cover wear inspection within every 600 EH 

SLI. 

(3) Inspection Criteria 

(i) Use paragraph 2.4.2 of Safran Helicopter 

Engines, S.A. Mandatory Service Bulletin 

(MSB) No. 292 72 2861, Version D, dated 

September 23, 2016, to do the inspections 

required by paragraphs (e)(1) and (e)(2) of 

this AD. 

(ii) Reserved. 

(4) Corrective Actions Based on the Results 

of the Most Recent Wear Inspection 

(i) If the wear measured from the most 

recent wear inspection is 0.15 mm or less, no 

further action is required. However, you must 

still comply with the repetitive inspection 

requirements of paragraph (e)(2) of this AD. 

(ii) If the most recent wear inspection was 

performed while the engine was in service, 

and the wear is greater than 0.15 mm, do the 

following: 

(A) If the wear measured from the most 

recent wear inspection is greater than 0.15 

mm, but 0.30 mm or less, remove the engine 

AGB from service within 200 EH SLI and 

replace with a part eligible for installation. 

(B) If the wear measured from the most 

recent wear inspection is greater than 0.30 

mm, but 0.40 mm or less, remove the engine 

AGB from service within 25 EH SLI and 

replace with a part eligible for installation. 

(C) If the wear measured from the most 

recent wear inspection is greater than 0.40 

mm, remove the engine AGB from service 

before further flight and replace with a part 

eligible for installation. 

(iii) If the most recent wear inspection was 

performed on the engine during an engine 

shop visit, and the wear is greater than 0.15 

mm, remove the engine AGB before further 

flight and replace with a part eligible for 

installation. 

(f) Credit for Previous Action 

If you have previously performed a wear 

inspection of the engine AGB cover prior to 

the effective date of this AD in accordance 

with the instructions given in Turbomeca 

MSB No. 292 72 2861, Version C, dated 

March 9, 2016, or Turbomeca MSB No. 292 

72 2861, Version B, dated February 2, 2016, 

then you may take credit for that wear 

inspection as the ‘‘most recent’’ wear 

inspection for the purposes of paragraph 

(e)(4) of this AD. 

(g) Definition 

For the purpose of this AD, an engine shop 

visit is defined as the induction of an engine 

into the shop for maintenance involving the 

separation of any major mating engine 

flanges, except that the separation of engine 

flanges solely for the purposes of 

transportation without subsequent engine 

maintenance does not constitute an engine 

shop visit. 

(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 

(1) For more information about this AD, 

contact Philip Haberlen, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 1200 District Avenue, 

Burlington, MA 01803; phone: 781–238– 

7770; fax: 781–238–7199; email: 

philip.haberlen@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2016–0055R1, dated 

October 11, 2016, for more information. You 

may examine the MCAI in the AD docket on 

the Internet at http://www.regulations.gov/ 

document?D=FAA-2015-3753-0006. 

(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) Safran Helicopter Engines, S.A. 

Mandatory Service Bulletin No. 292 72 2861, 

Version D, dated September 23, 2016. 

(ii) Reserved. 

(3) For Safran Helicopter Engines, S.A. 

service information identified in this AD, 

contact Safran Helicopter Engines, S.A. 

40220 Tarnos, France; phone: 33 0 5 59 74 

40 00; fax: 33 0 5 59 74 45 15. 

(4) You may view this service information 

at FAA, Engine & Propeller Directorate, 1200 

District Avenue, Burlington, MA. For 

information on the availability of this 

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

(5) 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 

November 29, 2016. 

Colleen M. D’Alessandro, 

Manager, Engine & Propeller Directorate, 

Aircraft Certification Service. 

[FR Doc. 2016–31695 Filed 12–29–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Parts 11 and 101 

[Docket No. FDA–2011–F–0172] 

RIN 0910–AG57 

Food Labeling; Nutrition Labeling of 

Standard Menu Items in Restaurants 

and Similar Retail Food 

Establishments; Extension of 

Compliance Date 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; extension of 

compliance date. 

SUMMARY: The Food and Drug 

Administration (FDA or we) is 

extending the compliance date for the 

final rule requiring disclosure of certain 

nutrition information for standard menu 

items in certain restaurants and retail 

food establishments. The final rule 

appeared in the Federal Register of 

December 1, 2014, and on May 5, 2016, 

we stated in the Federal Register that 

the enforcement of the final rule would 

begin on May 5, 2017. We are taking this 

action to clarify and confirm that the 

compliance date for the final rule is May 

5, 2017. 

DATES: Effective date: This final rule is 

effective December 30, 2016. 

Compliance date: Covered 

establishments must comply with the 

rule published December 1, 2014 (79 FR 

71156) by May 5, 2017. 

FOR FURTHER INFORMATION CONTACT: 

Ashley Rulffes, Center for Food Safety 

and Applied Nutrition (HFS–820), Food 

and Drug Administration, 5001 Campus 

Dr., College Park, MD 20740, 240–402– 

2371, email: ashley.rulffes@fda.hhs.gov. 

SUPPLEMENTARY INFORMATION: 

I. Background 

In the Federal Register of December 1, 

2014 (79 FR 71156), we published a 

final rule requiring disclosure of certain 

nutrition information for standard menu 


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