[Federal Register Volume 79, Number 190 (Wednesday, October 1, 2014)]
[Rules and Regulations]
[Pages 59093-59096]
[FR Doc No: 2014-22978]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0424; Directorate Identifier 2014-NM-003-AD;
Amendment 39-17976; AD 2014-20-03]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model BD-700-1A10 and BD-700-1A11 airplanes. This AD
was prompted by reports of an incorrectly assembled check tee fitting
used in fire extinguishing (FIREEX) distribution lines. This AD
requires inspecting to determine the part number and for all affected
check tee fittings measuring for correct depth, and replacing if
necessary. We are issuing this AD to detect and correct faulty check
tee fittings, which will reduce fire extinguishing protection.

DATES: This AD becomes effective November 5, 2014.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 5,
2014.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0424 or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
    For service information identified in this AD, contact Bombardier,
Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9,
Canada; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; email
<EMAIL_ADDRESS>Internet http://www.bombardier.com. You
may view this referenced service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>.

FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Bombardier, Inc.
Model BD-700-1A10 and BD-700-1A11 airplanes. The NPRM published in the
Federal Register on July 1, 2014 (79 FR 37246).
    Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2013-41, dated December 30, 2013 (referred to

after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition on certain Bombardier,
Inc. Model BD-700-1A10 and BD-700-1A11 airplanes. The MCAI states:

    A check tee fitting used in the aeroplane fire extinguishing
(FIREEX) distribution lines, was discovered by another airframe
manufacturer as being incorrectly assembled. A properly assembled
check tee fitting normally contains one check ball, however the
affected fitting contained two check balls. The FIREEX manufacturer
advised Bombardier that this condition may be present on aeroplane
models BD-700-1A10 and BD-700-1A11.
    Testing has verified that incorrect installation of the
additional check ball in the fitting reduces the flow rate of the
extinguishing agent. There are three check tee fittings installed on
the BD-700-1A10 and BD-700-1A11 aeroplanes, one for each engine and
one for the auxiliary power unit. Faulty fittings will reduce fire
extinguishing protection at the affected locations.
    Bombardier has issued several Alert Service Bulletins (ASBs) to
identify, inspect and replace if required, all affected fittings.
This [Canadian] AD mandates incorporation of the applicable
Bombardier ASBs to rectify this problem.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0424-0002.

Comments

    We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 37246, July 1,
2014) or on the determination of the cost to the public.

``Contacting the Manufacturer'' Paragraph in This AD

    Since late 2006, we have included a standard paragraph titled
``Airworthy Product'' in all MCAI ADs in which the FAA develops an AD
based on a foreign authority's AD.
    We have become aware that some operators have misunderstood or
misinterpreted the Airworthy Product paragraph to allow the owner/
operator to use messages provided by the manufacturer as approval of
deviations during the accomplishment of an AD-mandated action. The
Airworthy Product paragraph does not approve messages or other
information provided by the manufacturer for deviations to the
requirements of the AD-mandated actions. The Airworthy Product
paragraph only addresses the requirement to contact the manufacturer
for corrective actions for the identified unsafe condition and does not
cover deviations from other AD requirements. However, deviations to AD-
required actions are addressed in 14 CFR 39.17, and anyone may request
the approval for an alternative method of compliance to the AD-required
actions using the procedures found in 14 CFR 39.19.
    To address this misunderstanding and misinterpretation of the
Airworthy Product paragraph, we have changed the paragraph and retitled
it ``Contacting the Manufacturer.'' This paragraph now clarifies that
for any requirement in this AD to obtain corrective actions from a
manufacturer, the actions must be accomplished using a method approved
by the FAA, TCCA, or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO).
    The Contacting the Manufacturer paragraph also clarifies that, if
approved by the DAO, the approval must include the DAO-authorized
signature. The DAO signature indicates that the data and information
contained in the document are TCCA-approved, which is also FAA-
approved. Messages and other information provided by the manufacturer
that do not contain the DAO-authorized signature approval are not TCCA-
approved, unless TCCA directly approves the manufacturer's message or
other information.
    This clarification does not remove flexibility previously afforded
by the Airworthy Product paragraph. Consistent with long-standing FAA
policy, such flexibility was never intended for required actions. This
is also consistent with the recommendation of the Airworthiness
Directive Implementation Aviation Rulemaking Committee to increase
flexibility in complying with ADs by identifying those actions in
manufacturers' service instructions that are ``Required for
Compliance'' with ADs. We continue to work with manufacturers to
implement this recommendation. But once we determine that an action is
required, any deviation from the requirement must be approved as an
alternative method of compliance.
    We also have decided not to include a generic reference to either
the ``delegated agent'' or ``design approval holder (DAH) with State of
Design Authority design organization approval,'' but instead we have
provided the specific delegation approval granted by the State of
Design Authority for the DAH.

Conclusion

    We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD with the changes described
previously and minor editorial changes. We have determined that these
minor changes:
     Are consistent with the intent that was proposed in the
NPRM (79 FR 37246, July 1, 2014) for correcting the unsafe condition;
and
     Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 37246, July 1, 2014).
    We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.

Costs of Compliance

    We estimate that this AD affects 57 airplanes of U.S. registry.
    We also estimate that it would take about 1 work-hour 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 $0 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $4,845, or $85 per product.
    In addition, we estimate that any necessary follow-on actions would
take about 1 work-hour, for a cost of $85 per tee fitting. We have no
way of determining the number of aircraft that might need this action.
    According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0424; 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 Operations office (telephone 800-647-
5527) is in the ADDRESSES section.

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):

2014-20-03 Bombardier, Inc.: Amendment 39-17976. Docket No. FAA-
2014-0424; Directorate Identifier 2014-NM-003-AD.

(a) Effective Date

    This AD becomes effective November 5, 2014.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bombardier, Inc. Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, serial numbers
9002 through 9500 inclusive, and 9998.

(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire
Protection.

(e) Reason

    This AD was prompted by reports of an incorrectly assembled
check tee fitting used in fire extinguishing (FIREEX) distribution
lines. We are issuing this AD to detect and correct faulty check tee
fittings, which will reduce fire extinguishing protection.

(f) Compliance

    Comply with this AD within the compliance times specified,
unless already done.

(g) Part Number Identification

    Within 100 flight hours or 180 days, whichever occurs first
after the effective date of this AD, inspect to determine the part
number (P/N) of the FIREEX check tee fitting, in accordance with the
Accomplishment Instructions of the applicable service bulletin
identified in paragraph (g)(1), (g)(2), (g)(3), or (g)(4) of this
AD.
    (1) Bombardier Alert Service Bulletin A700-1A11-26-003, dated
April 18, 2013 (for Model BD-700-1A11 (BD-700) airplanes having S/Ns
9127 through 9383 inclusive; 9389 through 9400 inclusive, 9404
through 9431 inclusive, and 9998).
    (2) Bombardier Alert Service Bulletin A700-26-010, dated April
18, 2013 (for Model BD-700-1A10 (BD-700) airplanes having S/Ns 9002
through 9312 inclusive, 9314 through 9380 inclusive, and 9384
through 9429 inclusive).
    (3) Bombardier Alert Service Bulletin A700-26-5002, dated April
18, 2013 (for Model BD-700-1A11 (BD-700) airplanes having S/Ns 9386,
9401, and 9445 through 9498 inclusive).
    (4) Bombardier Alert Service Bulletin A700-26-6002, dated April
18, 2013 (for Model BD-700-1A10 (BD-700) airplanes having S/Ns 9313,
9381, and 9432 through 9500 inclusive).

(h) Measurement and Replacement

    If any inspection specified in paragraph (g) of this AD reveals
any check tee fitting having P/N 446651 and S/N 062 through 070
inclusive, 117 through 133 inclusive, 3728 through 3731 inclusive,
3733 through 3760 inclusive, or 3762 through 3776 inclusive: Within
100 flight hours or 180 days, whichever occurs first after the
effective date of this AD, measure the depth of the inlet fitting of
the check tee, in accordance with the Accomplishment Instructions of
the applicable service bulletin identified in paragraph (g)(1),
(g)(2), (g)(3), or (g)(4) of this AD. If the check tee depth is less
than 1.70 inches (4.32 cm), before further flight, replace the check
tee in accordance with the Accomplishment Instructions of the
applicable service bulletin identified in paragraph (g)(1), (g)(2),
(g)(3), or (g)(4) of this AD.

(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the ACO, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office. The AMOC approval letter must specifically reference this
AD.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, Engine and Propeller Directorate, FAA; or Transport Canada
Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO). If approved by the DAO, the approval must
include the DAO-authorized signature.

(j) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directive CF-2013-41, dated December 30,
2013, for related information. This MCAI may be found in the AD
docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0424-0002.

(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
    (i) Bombardier Alert Service Bulletin A700-1A11-26-003, dated
April 18, 2013.
    (ii) Bombardier Alert Service Bulletin A700-26-010, dated April
18, 2013.
    (iii) Bombardier Alert Service Bulletin A700-26-5002, dated
April 18, 2013.
    (iv) Bombardier Alert Service Bulletin A700-26-6002, dated April
18, 2013.
    (3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone<PHONE_NUMBER>; fax 514-855-
7401; email<EMAIL_ADDRESS>Internet http://www.bombardier.com.
    (4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (5) You may view this service information that is incorporated
by reference at the

National Archives and Records Administration (NARA). For information
on the availability of this material at NARA, call<PHONE_NUMBER>, or
go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on September 19, 2014.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-22978 Filed 9-30-14; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 80, Number 179 (Wednesday, September 16, 2015)]
[Notices]
[Pages 55668-55669]
[FR Doc No: 2015-23241]

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SECURITIES AND EXCHANGE COMMISSION

[Release No. 75886]

Securities Exchange Act of 1934; In the Matter of the Options
Clearing Corporation; Order Discontinuing the Automatic Stay

September 10, 2015.
    This matter comes before the Commission on the Options Clearing
Corporation's (``OCC'') motion to lift the

automatic stay of the approval, through delegated authority, of OCC's
plan for raising additional capital (``Capital Plan'') to support its
function as a systemically important financial market utility. On
January 26, 2015, the Commission issued a notice of filing of the
proposed rule change regarding the Capital Plan.\1\ After consideration
of the record in the proposed rule change, the Division of Trading and
Markets, for the Commission pursuant to delegated authority, issued an
order approving (``Approval Order'') the Capital Plan on March 6,
2015.\2\
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    \1\ Securities Exchange Act Release No. 74136 (January 26,
2015), 80 FR 5171 (January 30, 2015) (SR-OCC-2015-02).
    \2\ Order Approving Proposed Rule Change Concerning a Proposed
Capital Plan for Raising Additional Capital That Would Support the
Options Clearing Corporation's Function as a Systemically Important
Financial Market Utility, Securities Exchange Act Release No. 74452
(March 6, 2015), 80 FR 13058 (March 12, 2015) (SR-OCC-2015-02). The
Capital Plan was previously filed as an advance notice pursuant to
Section 806(e)(1) of the Payment, Clearing, and Settlement
Supervision Act of 2010. See 12 U.S.C. 5465(e)(1). The Commission
issued a notice of no objection to the advance notice on February
26, 2015. See Securities Exchange Act Release No. 74387 (February
26, 2015), 80 FR 12215 (March 6, 2015) (SR-OCC-2014-813).
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    BATS Global Markets, Inc. (``BATS''), BOX Options Exchange LLC
(``BOX''), KCG Holdings, Inc. (``KCG''), Miami International Securities
Exchange, LLC (``MIAX''), and Susquehanna International Group, LLP
(``SIG'') (collectively ``Petitioners'') each filed petitions for
review of the Approval Order, challenging the action taken by delegated
authority. The filing of the petitions automatically stayed the
Approval Order pursuant to Commission Rule of Practice 431(e).\3\ The
Commission has entered a separate Order Granting the Petitions for
Review and Scheduling Filing of Statements.\4\
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    \3\ 17 CFR 201.431(e).
    \4\ See Order Granting Petitions for Review and Scheduling
Filing of Statements, Securities Exchange Act Release No. 75885
(September 10, 2015).
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    In response to the automatic stay imposed by the filing of the
petitions to review the Approval Order, OCC filed a Motion to Lift the
Stay on April 2, 2015, citing the public policy reasons for
implementing the Capital Plan. The Petitioners responded, arguing that
continuing the automatic stay is appropriate in light of the important
policy and competition issues raised by the Approval Order.
    The Commission finds that it is in the public interest to lift the
stay during the pendency of the Commission's review. Under the
circumstances of this case, the Commission believes, on balance, that
strengthening the capitalization of a systemically important clearing
agency, such as OCC, is a compelling public interest. The Commission
also believes that the concerns raised by the Petitioners regarding
potential monetary and competitive harm do not currently justify
maintaining the stay during the pendency of the Commission's review.
Nor does the Commission believe that lifting the stay precludes
meaningful review of the Approval Order.
    For the reasons stated above, it is hereby:
    Ordered that the automatic stay of delegated action pursuant to
Commission Rule of Practice 431(e) \5\ is hereby discontinued, and that
OCC's Motion to Lift Stay of the staff's action in approving by
delegated authority File No. SR-OCC-2015-02 \6\ is granted.
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    \5\ See supra note 4.
    \6\ See supra note 2.
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    The order approving such proposed rule change shall remain in
effect.

    By the Commission.
Robert W. Errett,
Deputy Secretary.
[FR Doc. 2015-23241 Filed 9-15-15; 8:45 am]
 BILLING CODE 8011-01-P


[Federal Register Volume 87, Number 227 (Monday, November 28, 2022)]
[Rules and Regulations]
[Page 72869]
[FR Doc No: 2022-25820]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Docket No. FAA-2021-1152; Airspace Docket No. 19-AAL-72]
RIN 2120-AA66

Amendment of United States Area Navigation (RNAV) Route T-269;
Yakutat, AK

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: This action corrects a final rule published by the FAA in the
Federal Register on October 24, 2022, that amends United States Area
Navigation (RNAV) route T-269 in the vicinity of Yakutat, AK, in
support of a large and comprehensive T-route modernization project for
the state of Alaska. The final rule identified the MALAS, AK, route
point as a waypoint (WP), in error. This action makes an editorial
correction to the reference of the MALAS, AK, WP to change it to be
reflected as a Fix and match the FAA's National Airspace System
Resource (NASR) database information.

DATES: Effective date 0901 UTC, December 29, 2022. The Director of the
Federal Register approves this incorporation by reference action under
1 CFR part 51, subject to the annual revision of FAA Order 7400.11 and
publication of conforming amendments.

ADDRESSES: FAA Order 7400.11G, Airspace Designations and Reporting
Points, and subsequent amendments can be viewed online at www.faa.gov/air_traffic/publications/. For further information, you can contact the
Rules and Regulations Group, Federal Aviation Administration, 800
Independence Avenue SW, Washington, DC 20591; telephone: (202) 267-
8783.

FOR FURTHER INFORMATION CONTACT: Colby Abbott, Rules and Regulations
Group, Office of Policy, Federal Aviation Administration, 800
Independence Avenue SW, Washington, DC 20591; telephone: (202) 267-
8783.

SUPPLEMENTARY INFORMATION:

History

    The FAA published a final rule in the Federal Register (87 FR
64159; October 24, 2022), amending T-269 in support of a large and
comprehensive T-route modernization project for the state of Alaska.
Additionally, the FAA published a final rule correction in the Federal
Register (87 FR 65680; November 1, 2022), correcting T-269 to reflect
the KATAT, AK, route point as a Fix. Subsequent to publication of the
final rule correction, the FAA determined that the MALAS, AK, route
point was also inadvertently identified as a WP, in error. This rule
corrects that error by changing the reference of the MALAS, AK, WP to
the MALAS, AK, Fix. This is an editorial change only to match the FAA's
NASR database information and does not alter the alignment of the
affected T-269 route.
    United States Area Navigation Routes are published in paragraph
6011 of FAA Order JO 7400.11G, dated August 19, 2022, and effective
September 15, 2022, which is incorporated by reference in 14 CFR 71.1.
The RNAV T-route listed in this document will be published subsequently
in FAA Order JO 7400.11.

Correction to Final Rule

    Accordingly, pursuant to the authority delegated to me, reference
to the MALAS, AK, WP that is reflected in Docket No. FAA-2021-1152, as
published in the Federal Register of October 24, 2022 (87 FR 64159), FR
Doc. 2022-22496, and as published in the Federal Register of November
1, 2022 (87 FR 65680), FR Doc. 2022-23536, is corrected as follows:

0
1. On page 64160 for FR Doc. 2022-22496 and pages 65680 and 65681 for
FR Doc. 2022-23536, correct the table for T-269 Annette Island, AK
(ANN) to MKLUK, AK [Amended] to read:

                T-269 Annette Island, AK (ANN) to MKLUK, AK [Amended]

Annette Island,   VOR/DME                                    (Lat. 55[deg]03'37.47''
 AK (ANN)                                                     N, long.
                                                              131[deg]34'42.24'' W)
Biorka Island,    VORTAC                                     (Lat. 56[deg]51'33.87''
 AK (BKA)                                                     N, long.
                                                              135[deg]33'04.72'' W)
Yakutat, AK       VOR/DME                                    (Lat. 59[deg]30'38.99''
    (YAK)                                                     N, long.
                                                              139[deg]38'53.26'' W)
MALAS, AK         FIX                                        (Lat. 59[deg]39'58.52''
                                                              N, long.
                                                              140[deg]34'57.61'' W)
OXIDS, AK         WP                                         (Lat. 59[deg]41'51.68''
                                                              N, long.
                                                              141[deg]03'17.73'' W)
FOGNU, AK         WP                                         (Lat. 59[deg]53'31.88''
                                                              N, long.
                                                              141[deg]49'02.83'' W)
HORGI, AK         WP                                         (Lat. 60[deg]00'04.68''
                                                              N, long.
                                                              142[deg]35'23.34'' W)
ZIXIM, AK         WP                                         (Lat. 60[deg]03'48.75''
                                                              N, long.
                                                              143[deg]13'27.77'' W)
JOVOM, AK         WP                                         (Lat. 60[deg]07'40.55''
                                                              N, long.
                                                              143[deg]42'56.99'' W)
OXUGE, AK         WP                                         (Lat. 60[deg]06'15.81''
                                                              N, long.
                                                              144[deg]13'28.54'' W)
KATAT, AK         FIX                                        (Lat. 60[deg]15'29.17''
                                                              N, long.
                                                              144[deg]42'18.77'' W)
Johnstone Point,  VOR/DME                                    (Lat. 60[deg]28'51.43''
 AK (JOH)                                                     N, long.
                                                              146[deg]35'57.61'' W)
Anchorage, AK     VOR/DME                                    (Lat. 61[deg]10'04.32''
    (TED)                                                     N, long.
                                                              149[deg]57'36.51'' W)
MKLUK, AK         WP                                         (Lat. 60[deg]26'40.04''
                                                              N, long.
                                                              165[deg]55'17.28'' W)

* * * * *

    Issued in Washington, DC, on November 21, 2022.
Scott M. Rosenbloom,
Manager, Airspace Rules and Regulations.
[FR Doc. 2022-25820 Filed 11-25-22; 8:45 am]
BILLING CODE 4910-13-P