83 FR 14743 - Airworthiness Directives; Fokker Services B.V. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 67 (April 6, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 67 (April 6, 2018)
| Page Range | 14743-14745 | |
| FR Document | 2018-06822 |
[Federal Register Volume 83, Number 67 (Friday, April 6, 2018)] [Rules and Regulations] [Pages 14743-14745] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-06822] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0268; Product Identifier 2017-NM-096-AD; Amendment 39-19242; AD 2018-07-11] RIN 2120-AA64 Airworthiness Directives; Fokker Services B.V. Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F28 Mark 0100 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 interference between certain passenger service unit (PSU) panels, when in the deployed/open position, and the nearby emergency exit door cover. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective April 23, 2018. We must receive comments on this AD by May 21, 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- 0268; 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: Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3226. 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 2017-0113, dated June 28, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Fokker Services B.V. Model F28 Mark 0100 airplanes. The MCAI states: A report was received of an occurrence involving interference between certain Passenger Service Unit (PSU) panels, Part Number (P/ N) A546011-501 and P/N A546011-503, when in the deployed/open position, and the nearby emergency exit door cover. This condition, if not detected and corrected, could prevent a complete opening of the overwing emergency exit door, possibly obstructing the evacuation of occupants in case of an emergency landing. To address this potential unsafe condition, Fokker Services published Service Bulletin (SB) SBF100-25-131 (hereafter referred to as `the SB' in this AD) to provide inspection instructions. For the reasons described above, this [EASA] AD requires a one- time inspection to verify that the overwing emergency exit doors can be fully operated with the PSU-panels in the deployed/opened position and, depending on findings, accomplishment of applicable corrective action(s). This [EASA] AD also requires the reporting of findings. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0268. [[Page 14744]] 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 reasons 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-2018-0268; Product Identifier 2017-NM-096-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 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 ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Inspection................................. 1 work-hour x $85 per hour = $85... $0 $85 Reporting.................................. 1 work-hour x $85 per hour = $85... 0 85 ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. 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): 2018-07-11 Fokker Services B.V.: Amendment 39-19242; Docket No. FAA- 2018-0268; Product Identifier 2017-NM-096-AD. (a) Effective Date This AD becomes effective April 23, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Fokker Services B.V. Model F28 Mark 0100 airplanes, certificated in any category, serial numbers 11359, 11361, 11367, 11397, 11404, 11446, 11456, 11460, 11468, 11483, 11490, 11499, 11502, 11515 and 11520. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ furnishings. [[Page 14745]] (e) Reason This AD was prompted by a report of interference between certain passenger service unit (PSU) panels, when in the deployed/open position, and the nearby emergency exit door cover. We are issuing this AD to detect and correct interference between certain PSU panels and the nearby emergency exit door cover, which could prevent a complete opening of the overwing emergency exit door, and possibly obstruct the evacuation of occupants in case of an emergency landing. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions 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 actions 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 2017-0113, dated June 28, 2017. (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, 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 2017-0113, dated June 28, 2017, for related information. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0268. (2) For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3226. (j) Material Incorporated by Reference None. Issued in Des Moines, Washington, on March 22, 2018. Michael Kaszicki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-06822 Filed 4-5-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations 14743
(c) Applicability Burlington, MA 01803; phone: 781–238– Washington, DC, between 9 a.m. and 5
This AD applies to General Electric (GE) 7147; fax: 781–238–7199; email: p.m., Monday through Friday, except
CF6–80A, –80A1, –80A2, and –80A3 herman.mak@faa.gov. Federal holidays.
turbofan engines with low-pressure turbine (k) Material Incorporated by Reference
(LPT) stage 3 nozzles, part numbers (P/Ns) Examining the AD Docket
9290M52P05 and 9290M52P06, installed. None.
You may examine the AD docket on
Issued in Burlington, Massachusetts, on
(d) Subject
March 29, 2018. the internet at http://
Joint Aircraft System Component (JASC) www.regulations.gov by searching for
Robert Ganley,
Code 7250, Turbine Section. and locating Docket No. FAA–2018–
Manager, Engine and Propeller Standards
(e) Unsafe Condition
0268; or in person at the Docket
Branch, Aircraft Certification Service.
Operations office between 9 a.m. and 5
This AD was prompted by high cycle [FR Doc. 2018–06738 Filed 4–5–18; 8:45 am]
p.m., Monday through Friday, except
fatigue (HCF) cracking of the LPT stage 3 BILLING CODE 4910–13–P
nozzles resulting in LPT uncontainment. We Federal holidays. The AD docket
are issuing this AD to prevent cracking of the contains this AD, the regulatory
LPT stage 3 nozzles. The unsafe condition, if evaluation, any comments received, and
DEPARTMENT OF TRANSPORTATION other information. The street address for
not addressed, could result in LPT
uncontainment, damage to the engine, and
Federal Aviation Administration the Docket Operations office (telephone:
damage to the airplane. 800–647–5527) is in the ADDRESSES
(f) Compliance 14 CFR Part 39 section. Comments will be available in
Comply with this AD within the
the AD docket shortly after receipt.
[Docket No. FAA–2018–0268; Product
compliance times specified, unless already Identifier 2017–NM–096–AD; Amendment FOR FURTHER INFORMATION CONTACT: Tom
done. Rodriguez, Aerospace Engineer,
39–19242; AD 2018–07–11]
(g) Required Actions International Section, Transport
RIN 2120–AA64 Standards Branch, FAA, 2200 South
Within 36 months or during the next
engine shop visit after the effective date of 216th St., Des Moines, WA 98198;
Airworthiness Directives; Fokker
this AD, whichever occurs later, replace LPT telephone and fax: 206–231–3226.
Services B.V. Airplanes
stage 3 nozzles, P/Ns 9290M52P05 and SUPPLEMENTARY INFORMATION:
9290M52P06, with a part eligible for AGENCY: Federal Aviation
installation. Administration (FAA), DOT. Discussion
(h) Definition ACTION: Final rule; request for The European Aviation Safety Agency
(1) For the purpose of this AD, an engine comments. (EASA), which is the Technical Agent
shop visit is defined as the induction of an for the Member States of the European
engine into the shop for maintenance
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain Union, has issued EASA AD 2017–0113,
involving the separation of any major mating dated June 28, 2017 (referred to after
engine flanges. The separation of engine Fokker Services B.V. Model F28 Mark
flanges is not considered an engine shop visit 0100 airplanes. This AD requires this as the Mandatory Continuing
for the following purposes: contacting the FAA to obtain Airworthiness Information, or ‘‘the
(i) Transportation of an engine not attached instructions for addressing the unsafe MCAI’’), to correct an unsafe condition
to an aircraft without subsequent engine condition on these products, and doing for certain Fokker Services B.V. Model
maintenance. the actions specified in those F28 Mark 0100 airplanes. The MCAI
(ii) Removing the turbine rear frame (TRF) states:
for repair of TRF cracking.
instructions. This AD was prompted by
(iii) Removing the top or bottom high- interference between certain passenger A report was received of an occurrence
pressure compressor (HPC) case for HPC service unit (PSU) panels, when in the involving interference between certain
airfoil maintenance. deployed/open position, and the nearby Passenger Service Unit (PSU) panels, Part
(iv) Removing only the accessory gearbox emergency exit door cover. We are Number (P/N) A546011–501 and P/N
and/or transfer gearbox. A546011–503, when in the deployed/open
issuing this AD to address the unsafe
(2) Reserved. position, and the nearby emergency exit door
condition on these products. cover.
(i) Alternative Methods of Compliance DATES: This AD becomes effective April This condition, if not detected and
(AMOCs) 23, 2018. corrected, could prevent a complete opening
(1) The Manager, ECO Branch, FAA, has We must receive comments on this of the overwing emergency exit door,
the authority to approve AMOCs for this AD, AD by May 21, 2018. possibly obstructing the evacuation of
if requested using the procedures found in 14 ADDRESSES: You may send comments, occupants in case of an emergency landing.
CFR 39.19. In accordance with 14 CFR 39.19, To address this potential unsafe condition,
using the procedures found in 14 CFR
send your request to your principal inspector Fokker Services published Service Bulletin
11.43 and 11.45, by any of the following (SB) SBF100–25–131 (hereafter referred to as
or local Flight Standards District Office, as
appropriate. If sending information directly methods: ‘the SB’ in this AD) to provide inspection
to the manager of the ECO Branch, send it to • Federal eRulemaking Portal: Go to instructions.
the attention of the person identified in http://www.regulations.gov. Follow the For the reasons described above, this
paragraph (j) of this AD. You may email your instructions for submitting comments. [EASA] AD requires a one-time inspection to
request to: ANE-AD-AMOC@faa.gov. • Fax: 202–493–2251. verify that the overwing emergency exit
(2) Before using any approved AMOC, • Mail: U.S. Department of doors can be fully operated with the PSU-
notify your appropriate principal inspector, Transportation, Docket Operations, panels in the deployed/opened position and,
or lacking a principal inspector, the manager depending on findings, accomplishment of
daltland on DSKBBV9HB2PROD with RULES
M–30, West Building Ground Floor,
of the local Flight Standards District Office/ Room W12–140, 1200 New Jersey applicable corrective action(s). This [EASA]
Certificate Holding District Office. AD also requires the reporting of findings.
Avenue SE, Washington, DC 20590.
(j) Related Information • Hand Delivery: U.S. Department of You may examine the MCAI on the
For more information about this AD, Transportation, Docket Operations, M– internet at http://www.regulations.gov
contact Herman Mak, Aerospace Engineer, 30, West Building Ground Floor, Room by searching for and locating Docket No.
ECO Branch, FAA, 1200 District Avenue, W12–140, 1200 New Jersey Avenue SE, FAA–2018–0268.
VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 E:\FR\FM\06APR1.SGM 06APR1](https://thefederalregister.org/doc/83_FR_14810/page/1.svg)
![14744 Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations
FAA’s Determination and Requirements In addition, for the reasons stated above, amend this AD based on those
of This AD we find that good cause exists for comments.
This product has been approved by making this amendment effective in less We will post all comments we
the aviation authority of another than 30 days. receive, without change, to http://
country, and is approved for operation Comments Invited www.regulations.gov, including any
in the United States. Pursuant to our personal information you provide. We
bilateral agreement with the State of This AD is a final rule that involves
will also post a report summarizing each
Design Authority, we have been notified requirements affecting flight safety, and
substantive verbal contact we receive
of the unsafe condition described in the we did not precede it by notice and
about this AD.
MCAI. We are issuing this AD because opportunity for public comment. We
we evaluated all pertinent information invite you to send any written relevant Costs of Compliance
and determined the unsafe condition data, views, or arguments about this AD.
exists and is likely to exist or develop Send your comments to an address Currently, there are no affected U.S.-
on other products of these same type listed under the ADDRESSES section. registered airplanes. This AD requires
designs. Include ‘‘Docket No. FAA–2018–0268; contacting the FAA to obtain
Product Identifier 2017–NM–096–AD’’ instructions for addressing the unsafe
FAA’s Determination of the Effective at the beginning of your comments. We condition, and doing the actions
Date specifically invite comments on the specified in those instructions. Based on
Since there are currently no domestic overall regulatory, economic, the actions specified in the MCAI AD,
operators of this product, we find good environmental, and energy aspects of we are providing the following cost
cause that notice and opportunity for this AD. We will consider all comments estimates for an affected airplane that is
prior public comment are unnecessary. received by the closing date and may placed on the U.S. Register in the future:
ESTIMATED COSTS
Cost per
Action Labor cost Parts cost product
Inspection ......................................... 1 work-hour × $85 per hour = $85 ............................................................ $0 $85
Reporting ......................................... 1 work-hour × $85 per hour = $85 ............................................................ 0 85
We have received no definitive data period, the Executive Director has Adoption of the Amendment
that would enable us to provide cost delegated the authority to issue ADs Accordingly, under the authority
estimates for the on-condition actions applicable to transport category delegated to me by the Administrator,
specified in this AD. airplanes to the Director of the System the FAA amends 14 CFR part 39 as
Oversight Division. follows:
Authority for This Rulemaking
Title 49 of the United States Code Regulatory Findings
PART 39—AIRWORTHINESS
specifies the FAA’s authority to issue We determined that this AD will not DIRECTIVES
rules on aviation safety. Subtitle I, have federalism implications under
section 106, describes the authority of Executive Order 13132. This AD will ■ 1. The authority citation for part 39
the FAA Administrator. ‘‘Subtitle VII: not have a substantial direct effect on continues to read as follows:
Aviation Programs,’’ describes in more the States, on the relationship between Authority: 49 U.S.C. 106(g), 40113, 44701.
detail the scope of the Agency’s the national government and the States,
authority. § 39.13 [Amended]
or on the distribution of power and
We are issuing this rulemaking under responsibilities among the various ■ 2. The FAA amends § 39.13 by adding
the authority described in ‘‘Subtitle VII, levels of government. the following new airworthiness
Part A, Subpart III, Section 44701: directive (AD):
General requirements.’’ Under that For the reasons discussed above, I
certify that this AD: 2018–07–11 Fokker Services B.V.:
section, Congress charges the FAA with Amendment 39–19242; Docket No.
promoting safe flight of civil aircraft in 1. Is not a ‘‘significant regulatory FAA–2018–0268; Product Identifier
air commerce by prescribing regulations action’’ under Executive Order 12866; 2017–NM–096–AD.
for practices, methods, and procedures 2. Is not a ‘‘significant rule’’ under the (a) Effective Date
the Administrator finds necessary for DOT Regulatory Policies and Procedures
safety in air commerce. This regulation This AD becomes effective April 23, 2018.
(44 FR 11034, February 26, 1979);
is within the scope of that authority (b) Affected ADs
3. Will not affect intrastate aviation in
because it addresses an unsafe condition None.
Alaska; and
that is likely to exist or develop on
products identified in this rulemaking 4. Will not have a significant (c) Applicability
action. economic impact, positive or negative, This AD applies to Fokker Services B.V.
This AD is issued in accordance with on a substantial number of small entities Model F28 Mark 0100 airplanes, certificated
authority delegated by the Executive under the criteria of the Regulatory in any category, serial numbers 11359, 11361,
daltland on DSKBBV9HB2PROD with RULES
Director, Aircraft Certification Service, Flexibility Act. 11367, 11397, 11404, 11446, 11456, 11460,
as authorized by FAA Order 8000.51C. 11468, 11483, 11490, 11499, 11502, 11515
List of Subjects in 14 CFR Part 39 and 11520.
In accordance with that order, issuance
of ADs is normally a function of the Air transportation, Aircraft, Aviation (d) Subject
Compliance and Airworthiness safety, Incorporation by reference, Air Transport Association (ATA) of
Division, but during this transition Safety. America Code 25, Equipment/furnishings.
VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\06APR1.SGM 06APR1](https://thefederalregister.org/doc/83_FR_14810/page/2.svg)
![Federal Register / Vol. 83, No. 67 / Friday, April 6, 2018 / Rules and Regulations 14745
(e) Reason DEPARTMENT OF TRANSPORTATION Issued in College Park, Georgia, on March
This AD was prompted by a report of 29, 2018.
interference between certain passenger Federal Aviation Administration Geoff Lelliott,
service unit (PSU) panels, when in the Acting Manager, Operations Support Group,
deployed/open position, and the nearby 14 CFR Part 71 Eastern Service Center, Air Traffic
emergency exit door cover. We are issuing Organization.
this AD to detect and correct interference
[Docket No. FAA–2017–0953; Airspace [FR Doc. 2018–06997 Filed 4–5–18; 8:45 am]
between certain PSU panels and the nearby
emergency exit door cover, which could Docket No. 17–AEA–15] BILLING CODE 4910–13–P
prevent a complete opening of the overwing
emergency exit door, and possibly obstruct Amendment of Class E Airspace;
the evacuation of occupants in case of an Massena, NY DEPARTMENT OF THE TREASURY
emergency landing.
(f) Compliance AGENCY:Federal Aviation Alcohol and Tobacco Tax and Trade
Administration (FAA), DOT. Bureau
Comply with this AD within the
compliance times specified, unless already ACTION: Final rule, withdrawal.
done. 27 CFR Part 9
(g) Required Actions SUMMARY: This action withdraws the [Docket No. TTB–2016–0007; T.D. TTB–150;
Within 30 days after the effective date of final rule published in the Federal Ref: Notice No. 161]
this AD, request instructions from the Register on March 15, 2018. In that RIN 1513–AC26
Manager, International Section, Transport action, the FAA amended Class E
Standards Branch, FAA, to address the surface airspace and Class E airspace Establishment of the Cape May
unsafe condition specified in paragraph (e) of extending upward from 700 feet above
this AD; and accomplish the actions at the Peninsula Viticultural Area
the surface at Massena, NY. The FAA
times specified in, and in accordance with, AGENCY: Alcohol and Tobacco Tax and
those instructions. Guidance can be found in has determined that withdrawal of the
Mandatory Continuing Airworthiness final rule is warranted since there has Trade Bureau, Treasury.
Information (MCAI) European Aviation been a change in the date for the ACTION: Final rule; Treasury decision.
Safety Agency (EASA) AD 2017–0113, dated decommissioning of the Massena
June 28, 2017. collocated VHF omnidirectional range SUMMARY: The Alcohol and Tobacco Tax
tactical air navigation (VORTAC). and Trade Bureau (TTB) establishes the
(h) Alternative Methods of Compliance
(AMOCs)
approximately 126,635-acre ‘‘Cape May
DATES: Effective 0901 UTC, April 6, Peninsula’’ viticultural area in Cape
The Manager, International Section, 2018. May and Cumberland Counties, New
Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if Jersey. The viticultural area lies entirely
FOR FURTHER INFORMATION CONTACT: John
requested using the procedures found in 14 within the established Outer Coastal
Fornito, Operations Support Group,
CFR 39.19. In accordance with 14 CFR 39.19, Plain viticultural area. TTB designates
Eastern Service Center, Federal Aviation
send your request to your principal inspector viticultural areas to allow vintners to
or local Flight Standards District Office, as
Administration, 1701 Columbia Avenue,
better describe the origin of their wines
appropriate. If sending information directly College Park, Georgia 30337; telephone
and to allow consumers to better
to the International Section, send it to the (404) 305–6364.
identify wines they may purchase.
attention of the person identified in
SUPPLEMENTARY INFORMATION: DATES: This final rule is effective May 7,
paragraph (i)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOC- History 2018.
REQUESTS@faa.gov. Before using any FOR FURTHER INFORMATION CONTACT: Kate
approved AMOC, notify your appropriate The FAA published a final rule in the M. Bresnahan, Regulations and Rulings
principal inspector, or lacking a principal Federal Register for Docket No. FAA–
inspector, the manager of the local flight Division, Alcohol and Tobacco Tax and
2017–0953 (83 FR 11407, March 15, Trade Bureau, 1310 G Street NW, Box
standards district office/certificate holding
district office. 2018) amending Title 14 Code of 12, Washington, DC 20005; phone (202)
Federal Regulations (14 CFR) part 71 453–1039, ext. 151.
(i) Related Information amending Class E Airspace at Massena SUPPLEMENTARY INFORMATION:
(1) Refer to MCAI EASA AD 2017–0113, International-Richards Field Airport,
dated June 28, 2017, for related information. Massena, NY. The FAA found that the Background on Viticultural Areas
You may examine the MCAI on the internet Massena collocated VORTAC navigation
at http://www.regulations.gov by searching TTB Authority
for and locating Docket No. FAA–2018–0268.
aid will not be decommissioned at this
time. As a result, the final rule is being Section 105(e) of the Federal Alcohol
(2) For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer, withdrawn. Administration Act (FAA Act), 27
International Section, Transport Standards U.S.C. 205(e), authorizes the Secretary
Lists of Subjects in 14 CFR Part 71 of the Treasury to prescribe regulations
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax: 206– Airspace, Incorporation by reference, for the labeling of wine, distilled spirits,
231–3226.
Navigation (air). and malt beverages. The FAA Act
(j) Material Incorporated by Reference provides that these regulations should,
The Withdrawal among other things, prohibit consumer
None.
deception and the use of misleading
Issued in Des Moines, Washington, on ■ In consideration of the foregoing, the statements on labels and ensure that
daltland on DSKBBV9HB2PROD with RULES
March 22, 2018. final rule for Docket No. FAA–2017– labels provide the consumer with
Michael Kaszicki, 0953 (83 FR 11407, March 15, 2018), FR adequate information as to the identity
Acting Director, System Oversight Division, Doc. 2018–05045, is hereby withdrawn. and quality of the product. The Alcohol
Aircraft Certification Service. Authority: 49 U.S.C. 106(f), 106(g); 40103, and Tobacco Tax and Trade Bureau
[FR Doc. 2018–06822 Filed 4–5–18; 8:45 am] 40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR, (TTB) administers the FAA Act
BILLING CODE 4910–13–P 1959–1963 Comp., p. 389. pursuant to section 1111(d) of the
VerDate Sep<11>2014 20:57 Apr 05, 2018 Jkt 244001 PO 00000 Frm 00013 Fmt 4700 Sfmt 4700 E:\FR\FM\06APR1.SGM 06APR1](https://thefederalregister.org/doc/83_FR_14810/page/3.svg)
Document Created: 2018-11-01 09:16:09
Document Modified: 2018-11-01 09:16:09
| 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 April 23, 2018. | |
| Contact | Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3226. | |
| FR Citation | 83 FR 14743 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR