83 FR 5304 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 26 (February 7, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 26 (February 7, 2018)
| Page Range | 5304-5306 | |
| FR Document | 2018-02354 |
[Federal Register Volume 83, Number 26 (Wednesday, February 7, 2018)] [Rules and Regulations] [Pages 5304-5306] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-02354] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0030; Product Identifier 2014-NM-161-AD; Amendment 39-19180; AD 2018-03-07] RIN 2120-AA64 Airworthiness Directives; Airbus Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-202, -203, -223, and -243 airplanes; and Model A340- 211, -212, -311, and -313 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by a report of a hard contact that was found between the constant speed motor/generator feeder line route 6G/6E and the optional cabin temperature control pipe on the upper shell between certain frames. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective February 22, 2018. We must receive comments on this AD by March 26, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, 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, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 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-2018- 0030; or in person at the Docket Operations office 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 Operations 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: Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425- 227-1149. SUPPLEMENTARY INFORMATION: Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2014-0161, dated July 10, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus Model A330-202, -203, -223, and - 243 airplanes; and Model A340-211, -212, -311, and -313 airplanes. The MCAI states: A hard contact was found on an A330 aeroplane during production between the Constant Speed Motor/Generator (CSM/G) feeder line route 6G/6E (Functional Item Number 1526VB) and the optional cabin temperature control pipe on the upper shell between Frame (FR)37.4 and FR38 on stringer 5, right hand (RH) side. This condition, if not corrected, may lead to chafing and, consequently, a short circuit when the emergency generation is activated, resulting in the loss of emergency generation. The loss of normal generation combined with the loss of emergency generation jeopardizes the aeroplane safe flight. To address this potential unsafe condition, Airbus developed a modification to provide adequate clearance between harness 1526VB and the affected (optional) air-conditioning temperature control pipe. A340-200/-300 aeroplanes equipped with this optional cabin temperature control pipe are also affected by this issue. The modification can be embodied in service through Airbus Service Bulletin (SB) A330-92-3125, or SB A340-92-4097, as applicable. For the reasons described above, this [EASA] AD requires modification of the CSM/G mounting with installation of new stacking and/or longer bracket, depending on aeroplane configuration. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0030. FAA's Determination and Requirements of This 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 bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of these same type designs. FAA's Determination of the Effective Date Since there are currently no domestic operators of this product, we find good cause that notice and opportunity for prior public comment are unnecessary. In addition, for the reason(s) stated above, we find that good cause exists for making this amendment effective in less than 30 days. 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-2018-0030; Product Identifier 2014-NM-161-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 [[Page 5305]] received by the closing date and may amend this AD based on 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 Currently, there are no affected U.S.-registered airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition, and doing the actions specified in those instructions. Based on the actions specified in the MCAI AD, we are providing the following cost estimates for an affected airplane that is placed on the U.S. Register in the future: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Parts cost Cost per product ---------------------------------------------------------------------------------------------------------------- Modification....................... Up to 17 work-hours x $85 Up to $256........... Up to $1,701. per hour = $1,445. ---------------------------------------------------------------------------------------------------------------- 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. 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 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2018-03-07 Airbus: Amendment 39-19180; Docket No. FAA-2018-0030; Product Identifier 2014-NM-161-AD. (a) Effective Date This AD becomes effective February 22, 2018. (b) Affected ADs None. (c) Applicability This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Airbus Model A330-202, -203, -223, and -243 airplanes, all manufacturer serial numbers on which Airbus modification 45775, 45790, 45795, 46165, 46779, 48099, 48454, 52131, 52802, 53730, 53819, 54310, 54410, 54420, 54530, 55231, 55630, 56080, 56260, 56620, 57186, 57430, 200774, 201071, 201298, 201888, 202558, or 203045 has been embodied in production, except those on which Airbus modification 203395 has been embodied in production. (2) Airbus Model A340-211, -212, -311, and -313 airplanes, all manufacturer serial numbers on which Airbus modification 40413, 40550, 40901, 42021, 43590, or 46487 has been embodied in production, except those on which Airbus modification 203395 has been embodied in production. (d) Subject Air Transport Association (ATA) of America Code 92, Electrical system installation. (e) Reason This AD was prompted by a report of a hard contact that was found between the constant speed motor/generator feeder line route 6G/6E and the optional cabin temperature control pipe on the upper shell between certain frames. We are issuing this AD to prevent chafing, which can lead to a short circuit when the emergency generation is activated and a consequent loss of emergency generation. The loss of normal generation combined with the loss of emergency generation could adversely affect the airplane's continued safe flight and landing. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Action(s) Within 30 days after the effective date of this AD, request instructions from the Manager, International Section, Transport Standards Branch, FAA, to address the unsafe condition specified in paragraph (e) of this AD; and accomplish the action(s) at the times specified in, and in accordance with, those instructions. Guidance can be found in Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) AD 2014-0161, dated July 10, 2014. (h) Alternative Methods of Compliance (AMOCs) The Manager, International Section, Transport Standards Branch, 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, [[Page 5306]] send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (i)(2) of this AD. Information may be emailed to: [email protected]. 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. (i) Related Information (1) Refer to MCAI EASA AD 2014-0161, dated July 10, 2014, for related information. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0030. (2) For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425-227-1149. (j) Material Incorporated by Reference None. Issued in Renton, Washington, on January 26, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-02354 Filed 2-6-18; 8:45 am] BILLING CODE 4910-13-P
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paragraph (i)(2) of this AD. Information may We must receive comments on this This condition, if not corrected, may lead
be emailed to: 9-ANM-116-AMOC- AD by March 26, 2018. to chafing and, consequently, a short circuit
REQUESTS@faa.gov. Before using any when the emergency generation is activated,
ADDRESSES: You may send comments,
approved AMOC, notify your appropriate resulting in the loss of emergency generation.
principal inspector, or lacking a principal using the procedures found in 14 CFR The loss of normal generation combined with
inspector, the manager of the local flight 11.43 and 11.45, by any of the following the loss of emergency generation jeopardizes
standards district office/certificate holding methods: the aeroplane safe flight.
district office. • Federal eRulemaking Portal: Go to To address this potential unsafe condition,
(i) Related Information
http://www.regulations.gov. Follow the Airbus developed a modification to provide
instructions for submitting comments. adequate clearance between harness 1526VB
(1) Refer to MCAI EASA AD 2015–0126, • Fax: 202–493–2251. and the affected (optional) air-conditioning
dated July 1, 2015, for related information. • Mail: U.S. Department of temperature control pipe. A340–200/–300
You may examine the MCAI on the internet aeroplanes equipped with this optional cabin
at http://www.regulations.gov by searching
Transportation, Docket Operations, M–
temperature control pipe are also affected by
for and locating Docket No. FAA–2018–0029. 30, West Building Ground Floor, Room this issue. The modification can be embodied
(2) For more information about this AD, W12–140, 1200 New Jersey Avenue SE, in service through Airbus Service Bulletin
contact Vladimir Ulyanov, Aerospace Washington, DC 20590. (SB) A330–92–3125, or SB A340–92–4097, as
Engineer, International Section, Transport • Hand Delivery: U.S. Department of applicable.
Standards Branch, FAA, 1601 Lind Avenue Transportation, Docket Operations, M– For the reasons described above, this
SW, Renton, WA 98057–3356; telephone: 30, West Building Ground Floor, Room [EASA] AD requires modification of the
425–227–1138; fax: 425–227–1149. W12–140, 1200 New Jersey Avenue SE, CSM/G mounting with installation of new
(j) Material Incorporated by Reference Washington, DC, between 9 a.m. and 5 stacking and/or longer bracket, depending on
p.m., Monday through Friday, except aeroplane configuration.
None.
Federal holidays. You may examine the MCAI on the
Issued in Renton, Washington, on January internet at http://www.regulations.gov
25, 2018. Examining the AD Docket
by searching for and locating Docket No.
Michael Kaszycki, You may examine the AD docket on FAA–2018–0030.
Acting Director, System Oversight Division, the internet at http://
Aircraft Certification Service. www.regulations.gov by searching for FAA’s Determination and Requirements
[FR Doc. 2018–02350 Filed 2–6–18; 8:45 am] and locating Docket No. FAA–2018– of This AD
BILLING CODE 4910–13–P 0030; or in person at the Docket This product has been approved by
Operations office between 9 a.m. and 5 the aviation authority of another
p.m., Monday through Friday, except country, and is approved for operation
DEPARTMENT OF TRANSPORTATION Federal holidays. The AD docket in the United States. Pursuant to our
contains this AD, the regulatory bilateral agreement with the State of
Federal Aviation Administration evaluation, any comments received, and Design Authority, we have been notified
other information. The street address for of the unsafe condition described in the
14 CFR Part 39 MCAI. We are issuing this AD because
the Docket Operations office (telephone:
[Docket No. FAA–2018–0030; Product 800–647–5527) is in the ADDRESSES we evaluated all pertinent information
Identifier 2014–NM–161–AD; Amendment section. Comments will be available in and determined the unsafe condition
39–19180; AD 2018–03–07] the AD docket shortly after receipt. exists and is likely to exist or develop
RIN 2120–AA64 FOR FURTHER INFORMATION CONTACT: on other products of these same type
Vladimir Ulyanov, Aerospace Engineer, designs.
Airworthiness Directives; Airbus International Section, Transport FAA’s Determination of the Effective
Airplanes Standards Branch, FAA, 1601 Lind Date
AGENCY: Federal Aviation Avenue SW, Renton, WA 98057–3356;
telephone: 425–227–1138; fax: 425– Since there are currently no domestic
Administration (FAA), DOT. operators of this product, we find good
227–1149.
ACTION: Final rule; request for cause that notice and opportunity for
SUPPLEMENTARY INFORMATION:
comments. prior public comment are unnecessary.
Discussion In addition, for the reason(s) stated
SUMMARY: We are adopting a new
The European Aviation Safety Agency above, we find that good cause exists for
airworthiness directive (AD) for certain
(EASA), which is the Technical Agent making this amendment effective in less
Airbus Model A330–202, –203, –223,
for the Member States of the European than 30 days.
and –243 airplanes; and Model A340–
211, –212, –311, and –313 airplanes. Union, has issued EASA AD 2014–0161, Comments Invited
This AD requires contacting the FAA to dated July 10, 2014 (referred to after this
This AD is a final rule that involves
obtain instructions for addressing the as the Mandatory Continuing
requirements affecting flight safety, and
unsafe condition on these products, and Airworthiness Information, or ‘‘the
we did not precede it by notice and
doing the actions specified in those MCAI’’), to correct an unsafe condition
opportunity for public comment. We
instructions. This AD was prompted by for certain Airbus Model A330–202,
invite you to send any written relevant
a report of a hard contact that was found –203, –223, and –243 airplanes; and
data, views, or arguments about this AD.
between the constant speed motor/ Model A340–211, –212, –311, and –313
Send your comments to an address
generator feeder line route 6G/6E and airplanes. The MCAI states:
listed under the ADDRESSES section.
sradovich on DSK3GMQ082PROD with RULES
the optional cabin temperature control A hard contact was found on an A330 Include ‘‘Docket No. FAA–2018–0030;
pipe on the upper shell between certain aeroplane during production between the Product Identifier 2014–NM–161–AD’’
frames. We are issuing this AD to Constant Speed Motor/Generator (CSM/G)
feeder line route 6G/6E (Functional Item
at the beginning of your comments. We
address the unsafe condition on these specifically invite comments on the
products. Number 1526VB) and the optional cabin
temperature control pipe on the upper shell overall regulatory, economic,
DATES: This AD becomes effective between Frame (FR)37.4 and FR38 on environmental, and energy aspects of
February 22, 2018. stringer 5, right hand (RH) side. this AD. We will consider all comments
VerDate Sep<11>2014 17:31 Feb 06, 2018 Jkt 244001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\07FER1.SGM 07FER1](https://thefederalregister.org/doc/83_FR_5330/page/1.svg)
![Federal Register / Vol. 83, No. 26 / Wednesday, February 7, 2018 / Rules and Regulations 5305
received by the closing date and may will also post a report summarizing each instructions for addressing the unsafe
amend this AD based on those substantive verbal contact we receive condition, and doing the actions
comments. about this AD. specified in those instructions. Based on
We will post all comments we Costs of Compliance the actions specified in the MCAI AD,
receive, without change, to http:// we are providing the following cost
Currently, there are no affected U.S.- estimates for an affected airplane that is
www.regulations.gov, including any registered airplanes. This AD requires
personal information you provide. We placed on the U.S. Register in the future:
contacting the FAA to obtain
ESTIMATED COSTS
Cost per
Action Labor cost Parts cost product
Modification ........................................ Up to 17 work-hours × $85 per hour = $1,445 ... Up to $256 ....................................... Up to $1,701.
Authority for This Rulemaking 2. Is not a ‘‘significant rule’’ under the 201298, 201888, 202558, or 203045 has been
DOT Regulatory Policies and Procedures embodied in production, except those on
Title 49 of the United States Code which Airbus modification 203395 has been
specifies the FAA’s authority to issue (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in embodied in production.
rules on aviation safety. Subtitle I, (2) Airbus Model A340–211, –212, –311,
section 106, describes the authority of Alaska; and and –313 airplanes, all manufacturer serial
4. Will not have a significant numbers on which Airbus modification
the FAA Administrator. ‘‘Subtitle VII:
economic impact, positive or negative, 40413, 40550, 40901, 42021, 43590, or 46487
Aviation Programs,’’ describes in more
on a substantial number of small entities has been embodied in production, except
detail the scope of the Agency’s
under the criteria of the Regulatory those on which Airbus modification 203395
authority. has been embodied in production.
We are issuing this rulemaking under Flexibility Act.
the authority described in ‘‘Subtitle VII, List of Subjects in 14 CFR Part 39 (d) Subject
Part A, Subpart III, Section 44701: Air transportation, Aircraft, Aviation Air Transport Association (ATA) of
General requirements.’’ Under that America Code 92, Electrical system
safety, Incorporation by reference, installation.
section, Congress charges the FAA with Safety.
promoting safe flight of civil aircraft in (e) Reason
air commerce by prescribing regulations Adoption of the Amendment This AD was prompted by a report of a
for practices, methods, and procedures Accordingly, under the authority hard contact that was found between the
the Administrator finds necessary for delegated to me by the Administrator, constant speed motor/generator feeder line
safety in air commerce. This regulation the FAA amends 14 CFR part 39 as route 6G/6E and the optional cabin
is within the scope of that authority follows: temperature control pipe on the upper shell
because it addresses an unsafe condition between certain frames. We are issuing this
that is likely to exist or develop on PART 39—AIRWORTHINESS AD to prevent chafing, which can lead to a
short circuit when the emergency generation
products identified in this rulemaking DIRECTIVES is activated and a consequent loss of
action. emergency generation. The loss of normal
This AD is issued in accordance with ■ 1. The authority citation for part 39
generation combined with the loss of
authority delegated by the Executive continues to read as follows: emergency generation could adversely affect
Director, Aircraft Certification Service, Authority: 49 U.S.C. 106(g), 40113, 44701. the airplane’s continued safe flight and
as authorized by FAA Order 8000.51C. landing.
In accordance with that order, issuance § 39.13 [Amended]
(f) Compliance
of ADs is normally a function of the ■ 2. The FAA amends § 39.13 by adding
Comply with this AD within the
Compliance and Airworthiness the following new airworthiness compliance times specified, unless already
Division, but during this transition directive (AD): done.
period, the Executive Director has 2018–03–07 Airbus: Amendment 39–19180;
delegated the authority to issue ADs (g) Required Action(s)
Docket No. FAA–2018–0030; Product
applicable to transport category Identifier 2014–NM–161–AD. Within 30 days after the effective date of
airplanes to the Director of the System this AD, request instructions from the
(a) Effective Date Manager, International Section, Transport
Oversight Division.
This AD becomes effective February 22, Standards Branch, FAA, to address the
Regulatory Findings 2018. unsafe condition specified in paragraph (e) of
this AD; and accomplish the action(s) at the
We determined that this AD will not (b) Affected ADs times specified in, and in accordance with,
have federalism implications under None. those instructions. Guidance can be found in
Executive Order 13132. This AD will Mandatory Continuing Airworthiness
not have a substantial direct effect on (c) Applicability
Information (MCAI) European Aviation
the States, on the relationship between This AD applies to the airplanes identified Safety Agency (EASA) AD 2014–0161, dated
the national government and the States, in paragraphs (c)(1) and (c)(2) of this AD, July 10, 2014.
sradovich on DSK3GMQ082PROD with RULES
or on the distribution of power and certificated in any category.
(1) Airbus Model A330–202, –203, –223, (h) Alternative Methods of Compliance
responsibilities among the various and –243 airplanes, all manufacturer serial (AMOCs)
levels of government. numbers on which Airbus modification The Manager, International Section,
For the reasons discussed above, I 45775, 45790, 45795, 46165, 46779, 48099, Transport Standards Branch, FAA, has the
certify that this AD: 48454, 52131, 52802, 53730, 53819, 54310, authority to approve AMOCs for this AD, if
1. Is not a ‘‘significant regulatory 54410, 54420, 54530, 55231, 55630, 56080, requested using the procedures found in 14
action’’ under Executive Order 12866; 56260, 56620, 57186, 57430, 200774, 201071, CFR 39.19. In accordance with 14 CFR 39.19,
VerDate Sep<11>2014 17:31 Feb 06, 2018 Jkt 244001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\07FER1.SGM 07FER1](https://thefederalregister.org/doc/83_FR_5330/page/2.svg)
![5306 Federal Register / Vol. 83, No. 26 / Wednesday, February 7, 2018 / Rules and Regulations
send your request to your principal inspector DEPARTMENT OF ENERGY NE, Washington, DC 20426, (202) 502–
or local Flight Standards District Office, as 6219, Norman.Richardson@ferc.gov.
appropriate. If sending information directly Federal Energy Regulatory SUPPLEMENTARY INFORMATION:
to the International Section, send it to the Commission On February 28, 2017, the
attention of the person identified in
Commission issued an Annual Update
paragraph (i)(2) of this AD. Information may 18 CFR Part 11 to Fee Schedule for the Use of
be emailed to: 9-ANM-116-AMOC-
[Docket No. RM11–6–000] Government Lands for Hydropower
REQUESTS@faa.gov. Before using any
Licensees in the above-captioned
approved AMOC, notify your appropriate Annual Update to Fee Schedule for the proceeding. Pursuant to Annual Charges
principal inspector, or lacking a principal Use of Government Lands by for the Use of Government Lands in
inspector, the manager of the local flight Hydropower Licensees; Correction
standards district office/certificate holding
Alaska, Order No. 838, 83 FR 1 (Jan. 2,
district office. AGENCY: Federal Energy Regulatory 2018), FERC Stats. & Regs. ¶ 61,281
Commission,DOE. (2017), this document updates the per-
(i) Related Information acre rental fees for the State of Alaska,
ACTION: Correcting amendment.
(1) Refer to MCAI EASA AD 2014–0161, as reflected in the caption below.
dated July 10, 2014, for related information. SUMMARY: This document contains List of Subjects in 18 CFR Part 11
You may examine the MCAI on the internet corrections to the final rule (RM11–6–
at http://www.regulations.gov by searching 000) which published in the Federal Public lands.
for and locating Docket No. FAA–2018–0030. Register on Tuesday, March 7, 2017 (82 Accordingly, 18 CFR part 11 is
(2) For more information about this AD, FR 12717). The Final Rule provided the corrected by making the following
contact Vladimir Ulyanov, Aerospace annual update to the fee schedule in correcting amendment:
Engineer, International Section, Transport Appendix A to Part 11, which lists per-
Standards Branch, FAA, 1601 Lind Avenue acre rental fees by county (or other PART 11—[AMENDED]
SW, Renton, WA 98057–3356; telephone: geographic area) for use of government
425–227–1138; fax: 425–227–1149. lands by hydropower licensees and ■ 1. The authority citation for part 11
updated Appendix A to Part 11 with the continues to read as follows:
(j) Material Incorporated by Reference
fee schedule of per-acre rental fees by Authority: 16 U.S.C. 792–828c; 42 U.S.C.
None. county (or other geographic area) from 7101–7352.
Issued in Renton, Washington, on January October 1, 2016, through September 30,
2017 (Fiscal Year 2017). ■ 2. Appendix A to Part 11 is amended
26, 2018.
by:
Michael Kaszycki, DATES: Effective February 7, 2018, and
■ a. Revising the entries under
Acting Director, System Oversight Division,
is applicable beginning October 1, 2016.
‘‘Alaska’’; and
Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT:
■ b. Removing footnote 1.
Norman Richardson, Financial
[FR Doc. 2018–02354 Filed 2–6–18; 8:45 am] The revisions read as follows:
Management Division, Office of the
BILLING CODE 4910–13–P
Executive Director, Federal Energy Appendix A to Part 11—Fee Schedule
Regulatory Commission, 888 First Street for FY 2017
State County Fee/acre/yr
* * * * * * *
Alaska ............................................ Aleutian Islands Area ............................................................................. $1.02
Statewide per-acre ................................................................................. $36.53
* * * * * * *
ACTION: Notice of enforcement of Sector Mobile or a designated
Issued: February 1, 2018. regulation. representative.
Kimberly D. Bose, DATES: The regulation in 33 CFR
Secretary. SUMMARY: The Coast Guard will enforce 100.801, Table 7, line 4, will be
[FR Doc. 2018–02412 Filed 2–6–18; 8:45 am] a special local regulation on the Black enforced from 6 a.m. through 4:30 p.m.
BILLING CODE 6717–01–P
Warrior River extending the entire on March 24, 2018.
width of the channel from mile marker FOR FURTHER INFORMATION CONTACT: If
339.0 to mile marker 341.5 in you have questions about this notice of
DEPARTMENT OF HOMELAND Tuscaloosa, AL on March 24, 2018, to enforcement, call or email call or email
SECURITY provide for the safety of life on LT Kyle D. Berry, Sector Mobile,
navigable waterways during the Rowing Waterways Management Division, U.S.
Coast Guard Competition marine event. Our Coast Guard; telephone 251–441–5940,
regulation for Recurring Marine Events email Kyle.D.Berry@uscg.mil.
sradovich on DSK3GMQ082PROD with RULES
33 CFR Part 100 in Captain of the Port Sector Mobile SUPPLEMENTARY INFORMATION: The Coast
Zone identifies the regulated area for Guard will enforce a special local
[Docket No. USCG–2018–0013]
this rowing event. During the regulation for the annual ‘‘Rowing
Special Local Regulation; Black enforcement period, no vessel may Competition/University of South
Warrior River, Tuscaloosa, AL transit this regulated area without Alabama’’, listed in 33 CFR 100.801,
approval from the Captain of the Port Table 7, line 4, from 6 a.m. through 4:30
AGENCY: Coast Guard, DHS. p.m. on March 24, 2018. This action is
VerDate Sep<11>2014 17:31 Feb 06, 2018 Jkt 244001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\07FER1.SGM 07FER1](https://thefederalregister.org/doc/83_FR_5330/page/3.svg)
Document Created: 2018-10-26 13:56:28
Document Modified: 2018-10-26 13:56:28
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD becomes effective February 22, 2018. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425- 227-1149. | |
| FR Citation | 83 FR 5304 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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