Changes to Production Certificates and Approvals; Correction, 78650-78651 [2015-31639]
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78650
Federal Register / Vol. 80, No. 242 / Thursday, December 17, 2015 / Rules and Regulations
552a (l)(3)’’ and add ‘‘Section 552a
(i)(3)’’ in its place.
[FR Doc. 2015–31731 Filed 12–16–15; 8:45 am]
BILLING CODE 1505–01–D
FARM CREDIT ADMINISTRATION
12 CFR Part 652
Federal Agricultural Mortgage
Corporation Funding and Fiscal Affairs
CFR Correction
In Title 12 of the Code of Federal
Regulations, Parts 600 to 899, revised as
of January 1, 2015, on page 344, in
appendix A to subpart B to part 652, in
the table of contents, add ‘‘1.0
Introduction.’’.
[FR Doc. 2015–31730 Filed 12–16–15; 8:45 am]
BILLING CODE 1505–01–D
NATIONAL CREDIT UNION
ADMINISTRATION
12 CFR Part 747
Administrative Actions, Adjudicative
Hearings, Rules of Practice and
Procedure, and Investigations
CFR Correction
In Title 12 of the Code of Federal
Regulations, Parts 600 to 899, revised as
of January 1, 2015, on page 918, in
§ 747.616, remove the term ‘‘Office of
the Controller’’ and add the term ‘‘Office
of Chief Financial Officer’’ in its place.
[FR Doc. 2015–31732 Filed 12–16–15; 8:45 am]
BILLING CODE 1505–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 21 and 45
[Docket No. FAA–2013–0933; Amdt. Nos.
21–98A, 45–29A]
RIN 2120–AK20
Changes to Production Certificates
and Approvals; Correction
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
The Federal Aviation
Administration (FAA) is correcting a
final rule published on October 1, 2015.
In that rule, the FAA amended its
certification procedures and marking
requirements for aeronautical products
and articles. This action corrects the
effective date of the final rule to permit
Lhorne on DSK5TPTVN1PROD with RULES
SUMMARY:
VerDate Sep<11>2014
17:02 Dec 16, 2015
Jkt 238001
an earlier implementation of the rule’s
provisions that allow production
approval holders to issue authorized
release documents for aircraft engines,
propellers, and articles. It also permits
an earlier implementation date for
production certificate holders to
manufacture and install interface
components, and provides earlier relief
from the current requirement that fixedpitch wooden propellers be marked
using an approved fireproof method.
DATES: The final rule published October
1, 2015 (80 FR 59021), is effective
March 29, 2016, except for §§ 21.1(b)(1),
21.1(b)(5) through (9), 21.137(o), 21.142,
21.147, and 45.11(c), which are effective
January 4, 2016.
FOR FURTHER INFORMATION CONTACT: For
technical questions concerning this
action, contact Priscilla Steward or
Robert Cook, Aircraft Certification
Service, Production Certification
Section, AIR–112, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone (202) 267–1656; email:
priscilla.steward@faa.gov or telephone:
(202) 267–1590; email: robert.cook@
faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On October 1, 2015, the final rule,
‘‘Changes to Production Certificates and
Approvals,’’ 80 FR 59021, was
published in the Federal Register. In
that final rule the FAA revised the
regulations pertaining to certification
requirements for products and articles
in part 21 of title 14 of the Code of
Federal Regulations (14 CFR) and
removed certain marking requirements
in 14 CFR part 45 applicable to fixedpitch wooden propellers. The final rule
afforded production approval holders
(PAHs) a number of privileges not
currently permitted under current
regulations.
To provide PAHs privileges similar to
those afforded European and Canadian
approved manufacturers, § 21.137(o) of
the final rule permits a PAH to issue
authorized release documents for new
aircraft engines, propellers, and articles
that it produces, and also for used
aircraft engines, propellers, and articles
it rebuilds or alters in accordance with
§ 43.3(j), provided it establishes an
FAA-approved process in its quality
system for issuing those documents.
Authorized release documents would
typically be issued using FAA Form
8130–3, Airworthiness Release
Certificate, Airworthiness Approval Tag.
The final rule also allows a PAH that
meets the requirements of § 21.147(c) to
apply for an amendment to its
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Frm 00002
Fmt 4700
Sfmt 4700
production certificate for the purpose of
manufacturing and installing interface
components. The term ‘‘interface
component’’ is also specifically defined
in § 21.1(a)(5).
Additionally, the final rule amends
part 45 to exclude fixed-pitch wooden
propellers from the requirement that a
propeller, propeller blade, or propeller
hub be marked using an approved
fireproof method. This exclusion allows
manufacturers to mark their products in
a practical manner that takes into
account the inherent nature of wooden
propellers.
Finally, the rule revises the definition
of ‘‘airworthiness approval,’’ in
§ 21.1(b)(1), by expanding it to account
for the issuance of an airworthiness
approval in instances where an aircraft,
aircraft engine, propeller, or article does
not conform to its approved design or
may not be in a condition for safe
operation at the time the airworthiness
approval is generated and that
nonconformity or condition is specified
on the airworthiness approval
document.
The FAA issued the final rule with an
effective date of 180 days after its
publication in the Federal Register to
allow sufficient time for industry
compliance with new requirements
contained in the rule. This effective
date, however, also delayed the
implementation date of certain
provisions that removed regulatory
burdens that were no longer necessary
or appropriate in the current global
manufacturing environment.
Accordingly, the FAA is amending the
effective date of the final rule to January
4, 2016 for the following sections:
• § 21.1(b)(1) which revises the
definition of airworthiness approval
• § 21.1(b)(5), which defines interface
component
• § 21.137(o), which establishes
provisions for the issuance of
authorized release documents by PAHs
• § 21.142, which codifies provisions
for the inclusion of interface
components in a production limitation
record
• § 21.147, which specifies the
requirements that must be met to amend
a production certificate to include
interface components
• § 45.11(c), which excludes fixedpitch wooden propellers from the
requirement that they be marked using
an approved fireproof method.
The FAA also notes that Change 5 to
the Maintenance Annex Guidance
(MAG), which implements certain
provisions of the Aviation Safety
Agreement between the United States
and the European Union requires that
FAA Form 8130–3 be issued by a U.S.
E:\FR\FM\17DER1.SGM
17DER1
Federal Register / Vol. 80, No. 242 / Thursday, December 17, 2015 / Rules and Regulations
PAH for new parts that will be installed
in articles for which a dual
airworthiness release is to be issued. In
order to serve European customers
many U.S. repair stations will be
required to possess parts documentation
that U.S. PAHs cannot currently issue
and which can only be obtained from
the FAA or its designees.
Although the FAA and EASA have
agreed to delay the implementation of
Change 5 to the MAG until March 29,
2016, correcting the effective date of
§ 21.137(o) will provide PAHs with the
ability to establish a system for the
issuance of authorized release
documents to meet EASA requirements
without increasing staff in the form of
Organization Designation Authority
(ODA) unit members or Designated
Manufacturing Inspection
Representatives (DMIRs), or incurring
the cost of hiring additional Designated
Airworthiness Representatives (DARs).
Additionally, correcting the effective
date of §§ 21.142, 21.147, and 45.11(c)
will alleviate the current need for PAHs
to request new exemptions or renew
current exemptions to manufacture and
install interface components and
appropriately mark wooden propellers.
The remaining sections of the final
rule become effective on March 29,
2016, its originally published effective
date.
Correction
In FR Doc. 2015–24950, beginning on
page 59021 in the Federal Register of
October 1, 2015, in the second column,
correct the DATES section to read as
follows:
DATES: This final rule is effective
March 29, 2016, except for §§ 21.1(b)(1),
21.1(b)(5) through (9), 21.137(o), 21.142,
21.147 and 45.11(c), which are effective
on January 4, 2016.
Issued under authority provided by 49
U.S.C. 106(f), 44701(a), and 44703 in
Washington, DC, on December 11, 2015.
Lirio Liu,
Director, Office of Rulemaking.
[FR Doc. 2015–31639 Filed 12–16–15; 8:45 am]
BILLING CODE P
DEPARTMENT OF COMMERCE
658, in § 762.1, in paragraph (b), remove
‘‘§ 762.7’’ and add ‘‘§ 762.2’’ in its place,
and remove ‘‘§ 762.6’’ and add ‘‘§ 762.7’’
in its place.
[FR Doc. 2015–31733 Filed 12–16–15; 8:45 am]
BILLING CODE 1505–01–D
DEPARTMENT OF COMMERCE
Bureau of Industry and Security
15 CFR Part 772
Definitions of Terms
CFR Correction
In Title 15 of the Code of Federal
Regulations, Parts 300 to 799, revised as
of January 1, 2015, on pages 723, 727,
and 733, in § 772.1, remove the
definitions of ‘‘fault tolerance’’, ‘‘laser
duration’’ and ‘‘positioning accuracy’’.
[FR Doc. 2015–31737 Filed 12–16–15; 8:45 am]
BILLING CODE 1505–01–D
CONSUMER PRODUCT SAFETY
COMMISSION
16 CFR Part 1251
[Docket No. CPSC–2011–0081]
Toys: Determination Regarding Heavy
Elements Limits for Unfinished and
Untreated Wood
U.S. Consumer Product Safety
Commission.
AGENCY:
ACTION:
Final rule.
The Consumer Product Safety
Commission (‘‘Commission,’’ or
‘‘CPSC’’) is issuing a final rule
determining that unfinished and
untreated trunk wood does not contain
heavy elements that would exceed the
limits specified in the Commission’s toy
standard, ASTM F963–11. Based on this
determination, unfinished and
untreated trunk wood in toys does not
require third party testing for the heavy
element limits in ASTM F963.
SUMMARY:
The rule is effective on January
19, 2016.
DATES:
Bureau of Industry and Security
John
W. Boja, Lead Compliance Officer,
Office of Compliance, U.S. Consumer
Product Safety Commission, 4330 East
West Hwy., Room 610M, Bethesda, MD
20814; 301–504–7300: email: jboja@
cpsc.gov.
FOR FURTHER INFORMATION CONTACT:
Lhorne on DSK5TPTVN1PROD with RULES
15 CFR Part 762
Recordkeeping
CFR Correction
In Title 15 of the Code of Federal
Regulations, Parts 300 to 799, revised as
of January 1, 2015, on pages 657 and
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15:06 Dec 16, 2015
Jkt 238001
SUPPLEMENTARY INFORMATION:
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Fmt 4700
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78651
A. Background
1. Third Party Testing and Burden
Reduction
Section 14(a) of the Consumer
Product Safety Act, (‘‘CPSA’’), as
amended by the Consumer Product
Safety Improvement Act of 2008
(‘‘CPSIA’’), requires that manufacturers
of products subject to a consumer
product safety rule or similar rule, ban,
standard or regulation enforced by the
CPSC, must certify that the product
complies with all applicable CPSCenforced requirements. 15 U.S.C.
2063(a). For children’s products,
certification must be based on testing
conducted by a CPSC-accepted third
party conformity assessment body. Id.
Public Law 112–28 (August 12, 2011)
directed the CPSC to seek comment on
‘‘opportunities to reduce the cost of
third party testing requirements
consistent with assuring compliance
with any applicable consumer product
safety rule, ban, standard, or
regulation.’’ Public Law 112–28 also
authorized the Commission to issue new
or revised third party testing regulations
if the Commission determines ‘‘that
such regulations will reduce third party
testing costs consistent with assuring
compliance with the applicable
consumer product safety rules, bans,
standards, and regulations.’’ Id.
2063(d)(3)(B).
2. CPSC’s Toy Standard
Section 106 of the CPSIA states that
the provisions of ASTM International
(‘‘ASTM’’), Consumer Safety
Specifications for Toy Safety (‘‘ASTM
F963,’’ or ‘‘toy standard’’), ‘‘shall be
considered to be consumer product
safety standards issued by the
Commission under section 9 of the
CPSA (15 U.S.C. 2058).’’ 1 Thus, toys
subject to ASTM F963–11, the current
mandatory version of the standard, must
be tested by a CPSC-accepted third party
conformity assessment body and
demonstrate compliance with all
applicable CPSC requirements for the
manufacturer to issue a Children’s
Product Certificate (‘‘CPC’’) before the
toys can be entered into commerce.
The toy standard has numerous
requirements. Among them, section
4.3.5 requires that surface coating
materials and accessible substrates of
toys 2 that can be sucked, mouthed, or
1 ASTM F963–11 is a consumer product safety
standard, except for section 4.2 and Annex 4, or any
provision that restates or incorporates an existing
mandatory standard or ban promulgated by the
Commission or by statute.
2 ASTM F963–11 contains the following note
regarding the scope of the solubility requirement:
Continued
E:\FR\FM\17DER1.SGM
17DER1
Agencies
[Federal Register Volume 80, Number 242 (Thursday, December 17, 2015)]
[Rules and Regulations]
[Pages 78650-78651]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-31639]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 21 and 45
[Docket No. FAA-2013-0933; Amdt. Nos. 21-98A, 45-29A]
RIN 2120-AK20
Changes to Production Certificates and Approvals; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The Federal Aviation Administration (FAA) is correcting a
final rule published on October 1, 2015. In that rule, the FAA amended
its certification procedures and marking requirements for aeronautical
products and articles. This action corrects the effective date of the
final rule to permit an earlier implementation of the rule's provisions
that allow production approval holders to issue authorized release
documents for aircraft engines, propellers, and articles. It also
permits an earlier implementation date for production certificate
holders to manufacture and install interface components, and provides
earlier relief from the current requirement that fixed-pitch wooden
propellers be marked using an approved fireproof method.
DATES: The final rule published October 1, 2015 (80 FR 59021), is
effective March 29, 2016, except for Sec. Sec. 21.1(b)(1), 21.1(b)(5)
through (9), 21.137(o), 21.142, 21.147, and 45.11(c), which are
effective January 4, 2016.
FOR FURTHER INFORMATION CONTACT: For technical questions concerning
this action, contact Priscilla Steward or Robert Cook, Aircraft
Certification Service, Production Certification Section, AIR-112,
Federal Aviation Administration, 800 Independence Avenue SW.,
Washington, DC 20591; telephone (202) 267-1656; email:
priscilla.steward@faa.gov or telephone: (202) 267-1590; email:
robert.cook@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On October 1, 2015, the final rule, ``Changes to Production
Certificates and Approvals,'' 80 FR 59021, was published in the Federal
Register. In that final rule the FAA revised the regulations pertaining
to certification requirements for products and articles in part 21 of
title 14 of the Code of Federal Regulations (14 CFR) and removed
certain marking requirements in 14 CFR part 45 applicable to fixed-
pitch wooden propellers. The final rule afforded production approval
holders (PAHs) a number of privileges not currently permitted under
current regulations.
To provide PAHs privileges similar to those afforded European and
Canadian approved manufacturers, Sec. 21.137(o) of the final rule
permits a PAH to issue authorized release documents for new aircraft
engines, propellers, and articles that it produces, and also for used
aircraft engines, propellers, and articles it rebuilds or alters in
accordance with Sec. 43.3(j), provided it establishes an FAA-approved
process in its quality system for issuing those documents. Authorized
release documents would typically be issued using FAA Form 8130-3,
Airworthiness Release Certificate, Airworthiness Approval Tag.
The final rule also allows a PAH that meets the requirements of
Sec. 21.147(c) to apply for an amendment to its production certificate
for the purpose of manufacturing and installing interface components.
The term ``interface component'' is also specifically defined in Sec.
21.1(a)(5).
Additionally, the final rule amends part 45 to exclude fixed-pitch
wooden propellers from the requirement that a propeller, propeller
blade, or propeller hub be marked using an approved fireproof method.
This exclusion allows manufacturers to mark their products in a
practical manner that takes into account the inherent nature of wooden
propellers.
Finally, the rule revises the definition of ``airworthiness
approval,'' in Sec. 21.1(b)(1), by expanding it to account for the
issuance of an airworthiness approval in instances where an aircraft,
aircraft engine, propeller, or article does not conform to its approved
design or may not be in a condition for safe operation at the time the
airworthiness approval is generated and that nonconformity or condition
is specified on the airworthiness approval document.
The FAA issued the final rule with an effective date of 180 days
after its publication in the Federal Register to allow sufficient time
for industry compliance with new requirements contained in the rule.
This effective date, however, also delayed the implementation date of
certain provisions that removed regulatory burdens that were no longer
necessary or appropriate in the current global manufacturing
environment. Accordingly, the FAA is amending the effective date of the
final rule to January 4, 2016 for the following sections:
Sec. 21.1(b)(1) which revises the definition of
airworthiness approval
Sec. 21.1(b)(5), which defines interface component
Sec. 21.137(o), which establishes provisions for the
issuance of authorized release documents by PAHs
Sec. 21.142, which codifies provisions for the inclusion
of interface components in a production limitation record
Sec. 21.147, which specifies the requirements that must
be met to amend a production certificate to include interface
components
Sec. 45.11(c), which excludes fixed-pitch wooden
propellers from the requirement that they be marked using an approved
fireproof method.
The FAA also notes that Change 5 to the Maintenance Annex Guidance
(MAG), which implements certain provisions of the Aviation Safety
Agreement between the United States and the European Union requires
that FAA Form 8130-3 be issued by a U.S.
[[Page 78651]]
PAH for new parts that will be installed in articles for which a dual
airworthiness release is to be issued. In order to serve European
customers many U.S. repair stations will be required to possess parts
documentation that U.S. PAHs cannot currently issue and which can only
be obtained from the FAA or its designees.
Although the FAA and EASA have agreed to delay the implementation
of Change 5 to the MAG until March 29, 2016, correcting the effective
date of Sec. 21.137(o) will provide PAHs with the ability to establish
a system for the issuance of authorized release documents to meet EASA
requirements without increasing staff in the form of Organization
Designation Authority (ODA) unit members or Designated Manufacturing
Inspection Representatives (DMIRs), or incurring the cost of hiring
additional Designated Airworthiness Representatives (DARs).
Additionally, correcting the effective date of Sec. Sec. 21.142,
21.147, and 45.11(c) will alleviate the current need for PAHs to
request new exemptions or renew current exemptions to manufacture and
install interface components and appropriately mark wooden propellers.
The remaining sections of the final rule become effective on March
29, 2016, its originally published effective date.
Correction
In FR Doc. 2015-24950, beginning on page 59021 in the Federal
Register of October 1, 2015, in the second column, correct the DATES
section to read as follows:
DATES: This final rule is effective March 29, 2016, except for
Sec. Sec. 21.1(b)(1), 21.1(b)(5) through (9), 21.137(o), 21.142,
21.147 and 45.11(c), which are effective on January 4, 2016.
Issued under authority provided by 49 U.S.C. 106(f), 44701(a),
and 44703 in Washington, DC, on December 11, 2015.
Lirio Liu,
Director, Office of Rulemaking.
[FR Doc. 2015-31639 Filed 12-16-15; 8:45 am]
BILLING CODE P