Federal Register / Vol. 80, No. 224 / Friday, November 20, 2015 / Rules and Regulations 72579 

(i) Regulator Replacement 

Within 12 months after the effective date 

of this AD, unless already accomplished as 

specified in paragraph (h)(1) of this AD, 

replace each affected flightcrew oxygen mask 

regulator identified in paragraph (h) of this 

AD with a part identified in paragraph (i)(1) 

or (i)(2) of this AD. After replacement of all 

affected flightcrew oxygen mask regulators 

on an airplane, the actions specified in 

paragraph (h)(2) of this AD are no longer 

required, the AFM revision specified in 

paragraph (h)(2)(i) of this AD may be 

removed from the AFM, and the placard 

identified in paragraph (h)(2)(ii) of this AD 

may be removed from the airplane. 

(1) A serviceable part, not having a part 

number and serial number listed in 

Appendix 1 of Zodiac Aerospace Service 

Bulletin MCF–SBU–35–001, Revision 1, 

dated December 3, 2012. 

(2) A part that has been tested and passed 

the test in accordance with paragraph 3.A.(4) 

of the Accomplishment Instructions of 

Zodiac Aerospace Service Bulletin MCF– 

SBU–35–001, Revision 1, dated December 3, 

2012. 

(j) Credit for Previous Actions 

This paragraph provides credit for actions 

required by paragraphs (g), (h)(1)(ii), and 

(i)(2) of this AD, if those actions were 

performed before the effective date of this AD 

using Zodiac Aerospace Service Bulletin 

MCF–SBU–35–001, dated October 25, 2012, 

which is not incorporated by reference in this 

AD. 

(k) Parts Installation Limitation 

As of the effective date of this AD, no 

person may install any flightcrew oxygen 

mask regulator with a part number and serial 

number listed in Appendix 1 of Zodiac 

Aerospace Service Bulletin MCF–SBU–35– 

001, Revision 1, dated December 3, 2012, on 

any airplane, unless the regulator has been 

tested and passed the test, in accordance 

with paragraph 3.A.(4) of the 

Accomplishment Instructions of Zodiac 

Aerospace Service Bulletin MCF–SBU–35– 

001, Revision 1, dated December 3, 2012. 

(l) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Boston Aircraft Certification 

Office (ACO), ANE–150, 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 ACO, send it to ATTN: Ian Lucas, 

Aerospace Engineer, Boston Aircraft 

Certification Office, ANE–150, FAA, 12 New 

England Executive Park, Burlington, MA 

01803; phone: 781–238–7757; fax: 781–238– 

7170; email: ian.lucas@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. 

(m) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2012–0254R1, dated 

December 21, 2012, for related information. 

This MCAI may be found in the AD docket 

on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2015-0927-0004. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified 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 this AD specifies otherwise. 

(i) Zodiac Aerospace Service Bulletin 

MCF–SBU–35–001, Revision 1, dated 

December 3, 2012. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Zodiac Services, Technical 

Publication Department, Zodiac 

Aerotechnics, Oxygen Systems Europe, 61 

Rue Pierre Curie—CS20001, 78373 Plaisir 

Cedex, France; phone: (33) 01 61 24 23 23; 

fax: (33) 01 30 55 71 61; email: yann.laine@

zodiacaerospace.com; Internet: http://

www.zodiacaerospace.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 

November 3, 2015. 

Dionne Palermo, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–28883 Filed 11–19–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0932; Directorate 

Identifier 2014–NM–205–AD; Amendment 

39–18326; AD 2015–23–10] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 747–8 

series airplanes. This AD was prompted 

by a report of improperly installed 

outboard stowage bin modules in the 

passenger compartment found during 

maintenance. Further investigation 

revealed that certain attachment bracket 

bushings were missing or had moved 

out of the holes. This AD requires 

installing a spacer on the end of each 

quick-release pin that attaches the 

outboard stowage bin module to the 

lateral support tie rods of the main deck 

passenger compartment. We are issuing 

this AD to prevent detachment of the 

quick-release pin, which could result in 

separation of the lateral support tie rod 

and subsequent detachment of the 

module and consequent injuries to 

passengers or flightcrew. 

DATES: This AD is effective December 

28, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of December 28, 2015. 

ADDRESSES: 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. You may view 

this referenced 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. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0932. 

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– 

0932; 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 

Docket 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. 


tkelley on DSK3SPTVN1PROD with RULES
72580 Federal Register / Vol. 80, No. 224 / Friday, November 20, 2015 / Rules and Regulations 

FOR FURTHER INFORMATION CONTACT: 

Stanley Chen, Aerospace Engineer, 

Cabin Safety and Environmental 

Systems Branch, ANM–150S, FAA, 

Seattle Aircraft Certification Office, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; phone: 425–917–6585; fax: 

425–917–6590; email: stanley.chen@

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 The Boeing Company 

Model 747–8 airplanes. The NPRM 

published in the Federal Register on 

April 29, 2015 (80 FR 23739). The 

NPRM was prompted by a report of 

improperly installed outboard stowage 

bin modules in the passenger 

compartment found during 

maintenance. Further investigation 

revealed that certain attachment bracket 

bushings were missing or had moved 

out of the holes. The NPRM proposed to 

require installing a spacer on the end of 

each quick-release pin that attaches the 

outboard stowage bin module to the 

lateral support tie rods of the main deck 

passenger compartment. We are issuing 

this AD to prevent detachment of the 

quick-release pin, which could result in 

separation of the lateral support tie rod 

and subsequent detachment of the 

module and consequent injuries to 

passengers or flightcrew. 

Comment 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comment 

received on the NPRM (80 FR 23739, 

April 29, 2015) and the FAA’s response 

to each comment. 

Request To Revise Costs of Compliance 

Section 

Boeing asked that we add the parts 

cost to the cost table in the NPRM (80 

FR 23739, April 29, 2015). Boeing stated 

that the parts cost per spacer is $80, 

which increases the cost per product to 

$1,100, and the cost on U.S. operators 

to up to $2,200. 

We agree with the commenter for the 

reason provided. We have included the 

parts cost and changed the amount of 

the cost per product and the cost on 

U.S. operators specified in the ‘‘Costs of 

Compliance’’ section of this final rule. 

Conclusion 

We reviewed the relevant data, 

considered the comment received, and 

determined that air safety and the 

public interest require adopting this AD 

with the changes described previously 

and minor editorial changes. We have 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (80 FR 

23739, April 29, 2015) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (80 FR 23739, 

April 29, 2015). 

Related Service Information Under 

1 CFR Part 51 

We reviewed Boeing Special 

Attention Service Bulletin 747–25– 

3649, dated July 24, 2014. The service 

information describes procedures for 

installing a spacer on the end of each 

quick-release pin that attaches the 

outboard stowage bin module to the 

lateral support tie rods of the main deck 

passenger compartment. 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. 

Costs of Compliance 

We estimate that this AD affects 2 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. 

operators 

Spacer installations .............................. Up to 12 work-hours × $85 per hour = 

Up to $1,020.

$80 per spacer ..... Up to $1,100 ......... Up to $2,200 

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, 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): 

2015–23–10 The Boeing Company: 

Amendment 39–18326; Docket No. 


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Federal Register / Vol. 80, No. 224 / Friday, November 20, 2015 / Rules and Regulations 72581 

FAA–2015–0932; Directorate Identifier 

2014–NM–205–AD. 

(a) Effective Date 

This AD is effective December 28, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 747–8 series airplanes, certificated in 

any category, as identified in Boeing Special 

Attention Service Bulletin 747–25–3649, 

dated July 24, 2014. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25, Equipment/Furnishings. 

(e) Unsafe Condition 

This AD was prompted by a report of 

improperly installed outboard stowage bin 

modules in the passenger compartment 

found during maintenance. Further 

investigation revealed that certain attachment 

bracket bushings were missing or had moved 

out of the holes. We are issuing this AD to 

prevent detachment of the quick-release pin, 

which could result in separation of the lateral 

support tie rod and subsequent detachment 

of the module and consequent injuries to 

passengers or flightcrew. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Installation 

Within 36 months after the effective date 

of this AD: Install a spacer on the end of each 

quick-release pin that attaches the outboard 

stowage bin module to the lateral support tie 

rods of the main deck passenger 

compartment, in accordance with the 

Accomplishment Instructions of Boeing 

Special Attention Service Bulletin 747–25– 

3649, dated July 24, 2014. 

(h) 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 Seattle ACO, send it to 

the attention of the person identified in 

paragraph (i) 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 (h)(3)(i) and (h)(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. 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. 

(i) Related Information 

For more information about this AD, 

contact Stanley Chen, Aerospace Engineer, 

Cabin Safety and Environmental Systems 

Branch, ANM–150S, FAA, Seattle Aircraft 

Certification Office, 1601 Lind Avenue SW., 

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

6585; fax: 425–917–6590; email: 

stanley.chen@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) Boeing Special Attention Service 

Bulletin 747–25–3649, dated July 24, 2014. 

(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 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 

November 4, 2015. 

Dionne Palermo, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–28897 Filed 11–19–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 150 

[Docket No. FDA–1997–P–0007 (formerly 

Docket No. 1997P–0142)] 

Artificially Sweetened Fruit Jelly and 

Artificially Sweetened Fruit Preserves 

and Jams; Revocation of Standards of 

Identity 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule. 

SUMMARY: The Food and Drug 

Administration (FDA or we) is revoking 

the standards of identity for artificially 

sweetened jelly, preserves, and jams. 

We are taking this action primarily in 

response to a citizen petition submitted 

by the International Jelly and Preserve 

Association (IJPA). We also are taking 

this action because these standards are 

obsolete and unnecessary in light of our 

regulations for foods named by use of a 

nutrient content claim and a 

standardized term. This action will 

promote honesty and fair dealing in the 

interest of consumers. 

DATES: The final rule is effective on 

November 20, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Terri Wenger, Center for Food Safety 

and Applied Nutrition (HFS–820), Food 

and Drug Administration, 5100 Paint 

Branch Pkwy., College Park, MD 20740, 

240–402–2371. 

SUPPLEMENTARY INFORMATION: 

I. Background 

For more than 50 years, we have 

maintained standards of identity for 

fruit jelly (jelly) (§ 150.140 (21 CFR 

150.140)) and fruit preserves and jams 

(preserves and jams) (§ 150.160). The 

standards establish the common or 

usual name for these products and 

provide that these products may contain 

nutritive sweeteners (e.g., sugar). In 

1959, we added new standards of 

identity for artificially sweetened fruit 

jelly (artificially sweetened jelly) 

(§ 150.141) and artificially sweetened 

fruit preserves and jams (artificially 

sweetened preserves and jams) 

(§ 150.161) (24 FR 8896; October 31, 

1959) that permit the use of nonnutritive sweeteners (e.g., saccharin). 

Notably, §§ 150.141 and 150.161 limit 

the types of non-nutritive sweeteners 

that can be used in products that are 

governed by those standards of identity. 

Under §§ 150.141 and 150.161, such 

products may only use saccharin, 


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