This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

66413 

Vol. 80, No. 209 

Thursday, October 29, 2015 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–1123; Directorate 

Identifier 2014–CE–037–AD; Amendment; 

39–18308; AD 2015–06–02 R2] 

RIN 2120–AA64 

Airworthiness Directives; GA 8 Airvan 

(Pty) Ltd Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for comments 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for GA 8 

Airvan (Pty) Ltd Model GA8–TC320 

airplanes. This AD revises AD 2015–06– 

02 R1, which required inspection to 

detect and correct the omission of steel 

washers at each isolator mount location. 

This AD retains the actions of AD 2014– 

06–02 R1 but corrects the AD number in 

the parenthetical of the compliance time 

in paragraph (f)(1) of the AD. This AD 

was prompted by reports of missing 

required engine mount fire seal washers, 

which could reduce the engine retention 

capability in the event of a fire. We are 

issuing this AD to require actions to 

address the unsafe condition on these 

products. 

DATES: This AD is effective December 3, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of April 24, 2015 (80 FR 14810, 

March 20, 2015). 

We must receive comments on this 

AD by December 14, 2015. 

ADDRESSES: You may send comments 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 GA 8 Airvan (Pty) Ltd, 

c/o GippsAero Pty Ltd, Attn: Technical 

Services, P.O. Box 881, Morwell 

Victoria 3840, Australia; telephone: + 61 

03 5172 1200; fax: +61 03 5172 1201; 

email: techpubs@gippsaero.com; 

Internet: http://www.gippsaero.com/

customer-support/technicalpublications.aspx. 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 locating Docket No. FAA– 

2014–1123. 

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– 

1123; 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 street address for 

the Docket Office (telephone (800) 647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

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: 

Discussion 

On July 7, 2015, we issued AD 2015– 

06–02 R1, Amendment 39–18209 (80 FR 

42010; July 16, 2015). That AD required 

actions intended to address an unsafe 

condition on GA 8 Airvan (Pty) Ltd 

Model GA8–TC320 airplanes and was 

based on mandatory continuing 

airworthiness information (MCAI) 

originated by the Civil Aviation Safety 

Authority (CASA), which is the aviation 

authority for Australia. The MCAI (AD 

No. AD/GA8/8, Amdt 1, dated March 

26, 2015) states: 

A recent review of the engine mount 

installation on the GA8–TC 320 aircraft has 

highlighted the omission of engine mount 

fire seal washers during the assembly 

process. 

The current engine mount configuration 

does not meet the certification basis for the 

aircraft, specifically regulation 23.865 of the 

Federal Aviation Regulations of the United 

States of America, where engine mounts 

located in designated fire zones are required 

to be suitably shielded so that they are 

capable of withstanding the effects of a fire. 

The Gippsland Aeronautics GA8–TC 320 

aircraft require the installation of an 

approved steel washer at each of the engine 

mount locations to address a potential risk of 

reduced engine retention capability in the 

event of a fire. 

You may examine the MCAI on the 

Internet at http://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2011–0127. 

Since we issued AD 2015–06–02 R1, 

it was determined that the incorrect 

retained AD number was referenced in 

the parenthetical of the compliance time 

in paragraph (f)(1) of the AD. To avoid 

any confusion, this AD revises AD 

2015–06–02 R1 to correct this reference. 

Related Service Information Under 1 

CFR Part 51 

We reviewed GippsAero Mandatory 

Service Bulletin SB–GA8–2014–115, 

Issue 1, dated October 6, 2014. The 

service bulletin describes procedures for 

inspecting the orientation of the engine 

isolator mounts to verify proper 

installation, re-installing if necessary, 

and installing steel washers on the 

forward side of each side of the engine 

isolator mounts. 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. 

FAA’s Determination and Requirements 

of the AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 


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66414 Federal Register / Vol. 80, No. 209 / Thursday, October 29, 2015 / Rules and Regulations 

bilateral agreement with this State of 

Design Authority, they have notified us 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all 

information provided by the State of 

Design Authority and determined the 

unsafe condition exists and is likely to 

exist or develop on other products of the 

same type design. 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that allows 

for the immediate adoption of this AD. 

The FAA has found that the risk to the 

flying public justifies waiving notice 

and comment prior to adoption of this 

rule because the change does not affect 

compliance and the actions have 

already been proposed in prior 

rulemaking actions. Therefore, we 

determine that notice and opportunity 

for public comment before issuing this 

AD are impraticable. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2014–1123; 

Directorate Identifier 2014–CE–037– 

AD’’ at the beginning of your comments. 

We specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this AD because of those 

comments. 

We will post all comments we 

receive, without change, to http://

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD will affect 

13 products of U.S. registry. We also 

estimate that it would take about 5 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts would cost about $10 per 

product. 

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 

We 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 

the 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) 

2015–06–02 R1 (80 FR 42010, July 16, 

2015) and adding the following new AD: 

2015–06–02 R2 GA 8 Airvan (Pty) Ltd: 

Amendment 39–18308; Docket No. 

FAA–2014–1123; Directorate Identifier 

2014–CE–037–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective December 3, 2015. 

(b) Affected ADs 

This AD replaces AD 2015–06–02 R1, 

Amendment 39–18209 (80 FR 42010, July 16, 

2015) (‘‘AD 2015–06–02 R1’’). 

(c) Applicability 

This AD applies to GA 8 Airvan (Pty) Ltd 

GA8–TC320 airplanes, all serial numbers up 

to and including GA8–TC 320–14–205, 

certificated in any category. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 71: Power Plant. 

(e) Reason 

AD 2015–06–02, Amendment 39–18120 

(80 FR 14810, March 20, 2015) (‘‘AD 2015– 

06–02’’) 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 missing 

required engine mount fire seal washers, 

which could reduce the engine retention 

capability in the event of a fire. We issued 

AD 2015–06–02 R1, Amendment 39–18209 to 

retain the actions of AD 2015–06–02 and to 

revise the applicable airplane serial numbers. 

We are issuing this AD to correct the AD 

number in the parenthetical of the 

compliance time in paragraph (f)(1) of the AD 

and to detect and correct the omission of 

steel washers at each isolator mount location, 

which, if not corrected, could result in 

reduced engine retention capability in the 

event of a fire. 

(f) Actions and Compliance 

Unless already done, comply with this AD 

within the compliance times specified in 

paragraphs (f)(1) through (f)(3) of this AD: 

(1) Within the next 300 hours time-inservice after April 24, 2015 (the effective date 

retained from AD 2015–06–02 and AD 2015– 

06–02 R1) or within the next 12 months after 

April 24, 2015 (the effective date retained 

from AD 2015–06–02 and AD 2015–06–02 

R1), whichever occurs first, inspect the 

orientation of the engine isolator mounts to 

verify that the mounts have been installed 

properly following the Accomplishment 

Instructions in GippsAero Mandatory Service 

Bulletin SB–GA8–2014–115, Issue 1, dated 

October 6, 2014. 

(2) Before reinstalling the engine isolator 

mounts following the inspection required in 

paragraph (f)(1) of this AD, before further 

flight, install a part number J–2218–61 steel 

washer on the forward side of each of the 

four engine isolator mounts, following the 

Accomplishment Instructions in GippsAero 

Mandatory Service Bulletin SB–GA8–2014– 

115, Issue 1, dated October 6, 2014. 

(3) If during the inspection required in 

paragraph (f)(1) of this AD, any of the engine 

isolator mounts are found to not comply with 


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Federal Register / Vol. 80, No. 209 / Thursday, October 29, 2015 / Rules and Regulations 66415 

the specifications found in the 

Accomplishment Instructions of GippsAero 

Mandatory Service Bulletin SB–GA8–2014– 

115, Issue 1, dated October 6, 2014, before 

further flight, re-install the isolators to the 

correct orientation, or if damage is found, 

replace with airworthy parts. 

(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 FAA-approved 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. 

(h) Related Information 

Refer to MCAI Civil Aviation Safety 

Authority (CASA) AD No. AD/GA8/8, Amdt 

1, dated March 26, 2015. The MCAI can be 

found in the AD docket on the Internet at: 

http://www.regulations.gov/

#!documentDetail;D=FAA-2014-1123-0007. 

(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. 

(3) The following service information was 

approved for IBR on April 24, 2015 (80 FR 

14810, March 20, 2015). 

(i) GippsAero Mandatory Service Bulletin 

SB–GA8–2014–115, Issue 1, dated October 6, 

2014. 

(ii) Reserved. 

(4) For GippsAero service information 

identified in this AD, contact GA 8 Airvan 

(Pty) Ltd, c/o GippsAero Pty Ltd, Attn: 

Technical Services, P.O. Box 881, Morwell 

Victoria 3840, Australia; telephone: + 61 03 

5172 1200; fax: +61 03 5172 1201; email: 

techpubs@gippsaero.com; Internet: http://

www.gippsaero.com/customer-support/

technical-publications.aspx. 

(5) 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–2014–1123. 

(6) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

theavailability 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 

October 22, 2015. 

Melvin Johnson, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–27438 Filed 10–28–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 73 

[Docket No. FDA–2014–C–1552] 

Listing of Color Additives Exempt 

From Certification; Spirulina Extract; 

Confirmation of Effective Date 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; confirmation of 

effective date. 

SUMMARY: The Food and Drug 

Administration (FDA or we) is 

confirming the effective date of 

September 22, 2015, for the final rule 

that appeared in the Federal Register of 

August 21, 2015, and that amended the 

color additive regulations to expand the 

permitted use of spirulina extract as a 

color additive to include use in coating 

formulations applied to dietary 

supplement and drug tablets and 

capsules. 

DATES: Effective date of final rule 

published in the Federal Register of 

August 21, 2015 (80 FR 50762), 

confirmed: September 22, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Molly A. Harry, Center for Food Safety 

and Applied Nutrition (HFS–265), Food 

and Drug Administration, 5100 Paint 

Branch Pkwy., College Park, MD 20740– 

3835, 240–402–1075. 

SUPPLEMENTARY INFORMATION: In the 

Federal Register of August 21, 2015 (80 

FR 50762), we amended the color 

additive regulations in § 73.530 

Spirulina extract (21 CFR 73.530) to 

expand the permitted use of spirulina 

extract as a color additive to include use 

in coating formulations applied to 

dietary supplement tablets and 

capsules. We also amended the color 

additive regulations to add § 73.1530 

Spirulina extract (21 CFR 73.1530) to 

provide for the safe use of spirulina 

extract as a color additive in coating 

formulations applied to drug tablets and 

capsules. 

We gave interested persons until 

September 21, 2015, to file objections or 

requests for a hearing. We received no 

objections or requests for a hearing on 

the final rule. Therefore, we find that 

the effective date of the final rule that 

published in the Federal Register of 

August 21, 2015, should be confirmed. 

List of Subjects in 21 CFR Part 73 

Color additives, Cosmetics, Drugs, 

Foods, Medical devices. 

Therefore, under the Federal Food, 

Drug, and Cosmetic Act (21 U.S.C. 321, 

341, 342, 343, 348, 351, 352, 355, 361, 

362, 371, 379e) and under authority 

delegated to the Commissioner of Food 

and Drugs, and redelegated to the 

Director, Center for Food Safety and 

Applied Nutrition, we are giving notice 

that no objections or requests for a 

hearing were filed in response to the 

August 21, 2015, final rule. 

Accordingly, the amendments issued 

thereby became effective September 22, 

2015. 

Dated: October 21, 2015. 

Susan Bernard, 

Director, Office of Regulations, Policy and 

Social Sciences, Center for Food Safety and 

Applied Nutrition. 

[FR Doc. 2015–27369 Filed 10–28–15; 8:45 am] 

BILLING CODE 4164–01–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[TD 9733] 

RIN 1545–BJ49 

United States Property Held by 

Controlled Foreign Corporations in 

Transactions Involving Partnerships; 

Rents and Royalties Derived in the 

Active Conduct of a Trade or 

Business; Correction 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Final and temporary 

regulations; correcting amendment. 

SUMMARY: This document contains 

corrections to final and temporary 

regulations (TD 9733) that were 

published in the Federal Register on 

September 2, 2015 (80 FR 52976). The 

temporary regulations are regarding the 

treatment as United States property of 


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