IFR Altitudes; Miscellaneous Amendments, 15612-15615 [2017-06294]
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15612
Federal Register / Vol. 82, No. 60 / Thursday, March 30, 2017 / Rules and Regulations
unusual design features: Composite fan
blades. These fan blades will have
significant differences in material
property characteristics as compared to
conventionally designed fan blades
using non-composite metallic materials.
Composite material designs can
incorporate multiple load paths and/or
crack arresting features that prevent
delamination or crack propagation that
could result in blade failure during the
blade service life. These blades require
additional airworthiness standards for
type certification of the GE9X engine
models.
Discussion
As discussed in the summary section,
the GE9X engine models incorporate
composite fan blades instead of
conventional, single load path, metallic
fan blades, which is a novel or unusual
design feature for aircraft engines. The
applicable airworthiness regulations do
not contain adequate or appropriate
safety standards for this design feature.
Applicability
As discussed above, these special
conditions are applicable to the GE9X
engine models. Should GE apply at a
later date for a change to the type
certificate to include another model on
the same type certificate incorporating
the same novel or unusual design
features, the special conditions would
apply to that model as well.
Conclusion
This action affects only certain novel
or unusual design features on GE9X
engine models. It is not a rule of general
applicability and applies only to GE,
who requested FAA approval of this
engine feature.
List of Subjects in 14 CFR Part 33
Aircraft, Engines, Aviation safety,
Reporting and recordkeeping
requirements.
The authority citation for these
special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
jstallworth on DSK7TPTVN1PROD with RULES
The Special Conditions
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the following special
conditions are issued as part of the type
certification basis for GE9X engine
models.
1. Special Conditions: General
Electric Company, GE9X Engine
Models; Incorporation of Composite Fan
Blades. In lieu of the fan blade
containment test with the fan blade
failing at the outermost retention groove
VerDate Sep<11>2014
14:26 Mar 29, 2017
Jkt 241001
as specified in § 33.94(a)(1), complete
the following requirements:
(a) Conduct an engine fan blade
containment test with the fan blade
failing at the inner annulus flow path
line instead of at the outermost
retention groove.
(b) Substantiate by test and analysis,
or other methods acceptable to the FAA,
that a fan disk and fan blade retention
system with minimum material
properties can withstand, without
failure, a centrifugal load equal to two
times the maximum load the retention
system could experience within
approved engine operating limitations.
The fan blade retention system includes
the portion of the fan blade from the
inner annulus flow path line inward to
the blade dovetail, the blade retention
components, and the fan disk and fan
blade attachment features.
(c) Using a procedure approved by the
FAA, establish an operating limitation
that specifies the maximum allowable
number of start-stop stress cycles for the
fan blade retention system. The life
evaluation must include the combined
effects of high-cycle and low-cycle
fatigue. If the operating limitation is less
than 100,000 cycles, that limitation
must be specified in Chapter 5 of the
Engine Manual Airworthiness
Limitation Section. The procedure used
to establish the maximum allowable
number of start-stop stress cycles for the
fan blade retention system will
incorporate the integrity requirements
specified in paragraphs (c)(1), (c)(2), and
(c)(3) of these special conditions for the
fan blade retention system.
(1) An engineering plan which
establishes and maintains that the
combinations of loads, material
properties, environmental influences,
and operating conditions, including the
effects of parts influencing these
parameters, are well known or
predictable through validated analysis,
test, or service experience.
(2) A manufacturing plan that
identifies the specific manufacturing
constraints necessary to consistently
produce the fan blade retention system
with the attributes required by the
engineering plan.
(3) A service management plan that
defines in-service processes for
maintenance and repair of the fan blade
retention system, which will maintain
attributes consistent with those required
by the engineering plan.
(d) Substantiate by test and analysis,
or other methods acceptable to the FAA,
that the blade design below the inner
annulus flow path line provides
multiple load paths and/or crack
arresting features that prevent
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
delamination or crack propagation to
blade failure during the life of the blade.
(e) Substantiate that, during the
service life of the engine, the total
probability of the occurrence of a
hazardous engine effect defined in
§ 33.75 due to an individual blade
retention system failure resulting from
all possible causes will be extremely
improbable, with (a cumulative
calculated probability of failure of less
than 10¥9) per engine flight hour.
(f) Substantiate by test or analysis that
not only will the engine continue to
meet the requirements of § 33.75
following a lightning strike on the
composite fan blade structure, but that
the lightning strike will not cause
damage to the fan blades that would
prevent continued safe operation of the
affected engine.
(g) Account for the effects of inservice deterioration, manufacturing
variations, minimum material
properties, and environmental effects
during the tests and analyses required
by paragraphs (b), (c), (d), (e), and (f) of
these special conditions.
(h) Propose fleet leader monitoring
and field sampling programs that will
monitor the effects of engine fan blade
usage on fan blade retention system
integrity. The programs must be
approved by the FAA prior to
certification of the GE9X engine models.
(i) Mark each fan blade legibly and
permanently with a part number and a
serial number.
Issued in Burlington, Massachusetts, on
March 23, 2017.
Robert J. Ganley,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 2017–06277 Filed 3–29–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 95
[Docket No. 31129; Amdt. No. 532]
IFR Altitudes; Miscellaneous
Amendments
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule
AGENCY:
This amendment adopts
miscellaneous amendments to the
required IFR (instrument flight rules)
altitudes and changeover points for
certain Federal airways, jet routes, or
direct routes for which a minimum or
maximum en route authorized IFR
altitude is prescribed. This regulatory
SUMMARY:
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30MRR1
Federal Register / Vol. 82, No. 60 / Thursday, March 30, 2017 / Rules and Regulations
action is needed because of changes
occurring in the National Airspace
System. These changes are designed to
provide for the safe and efficient use of
the navigable airspace under instrument
conditions in the affected areas.
DATES: Effective 0901 UTC, April 27,
2017.
FOR FURTHER INFORMATION CONTACT:
Thomas J Nichols, Flight Procedure
Standards Branch (AMCAFS–420),
Flight Technologies and Programs
Division, Flight Standards Service,
Federal Aviation Administration, Mike
Monroney Aeronautical Center, 6500
South MacArthur Blvd., Oklahoma City,
OK 73169 (Mail Address: P.O. Box
25082, Oklahoma City, OK 73125)
telephone: (405) 954–4164.
SUPPLEMENTARY INFORMATION: This
amendment to part 95 of the Federal
Aviation Regulations (14 CFR part 95)
amends, suspends, or revokes IFR
altitudes governing the operation of all
aircraft in flight over a specified route
or any portion of that route, as well as
the changeover points (COPs) for
Federal airways, jet routes, or direct
routes as prescribed in part 95.
The Rule
The specified IFR altitudes, when
used in conjunction with the prescribed
changeover points for those routes,
ensure navigation aid coverage that is
adequate for safe flight operations and
free of frequency interference. The
reasons and circumstances that create
the need for this amendment involve
matters of flight safety and operational
efficiency in the National Airspace
System, are related to published
aeronautical charts that are essential to
the user, and provide for the safe and
efficient use of the navigable airspace.
In addition, those various reasons or
circumstances require making this
amendment effective before the next
scheduled charting and publication date
of the flight information to assure its
timely availability to the user. The
effective date of this amendment reflects
those considerations. In view of the
close and immediate relationship
between these regulatory changes and
safety in air commerce, I find that notice
and public procedure before adopting
this amendment are impracticable and
contrary to the public interest and that
good cause exists for making the
amendment effective in less than 30
days.
Conclusion
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
current. It, therefore—(1) is not a
‘‘significant regulatory action’’ under
15613
Executive Order 12866; (2) is not a
‘‘significant rule’’ under DOT
Regulatory Policies and Procedures (44
FR 11034; February 26, 1979); and (3)
does not warrant preparation of a
regulatory evaluation as the anticipated
impact is so minimal. For the same
reason, the FAA certifies that this
amendment will not have a significant
economic impact on a substantial
number of small entities under the
criteria of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 95
Airspace, Navigation (air).
Issued in Washington, DC, on March 24,
2017.
John Duncan,
Director, Flight Standards Service.
Adoption of the Amendment
Accordingly, pursuant to the
authority delegated to me by the
Administrator, part 95 of the Federal
Aviation Regulations (14 CFR part 95) is
amended as follows effective at 0901
UTC, April 27,2017.
1. The authority citation for part 95
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40103, 40106,
40113, 40114, 40120, 44502, 44514, 44719,
44721.
2. Part 95 is amended to read as
follows:
■
REVISIONS TO IFR ALTITUDES AND CHANGEOVER POINT
[Amendment 532 effective date April 27, 2017]
From
To
§ 95.6012
§ 95.6001 Victor Routes—U.S.
VOR Federal Airway V12 Is Amended To Read in Part
PANHANDLE, TX VORTAC .........................................................
§ 95.6014
jstallworth on DSK7TPTVN1PROD with RULES
14:26 Mar 29, 2017
Jkt 241001
CARFF, OK FIX ...........................................................................
*DATTA, OK FIX ..........................................................................
3700
3000
WILL ROGERS, OK VORTAC ....................................................
3000
MITBEE, OK VORTAC.
......................................................................................................
......................................................................................................
4300
4900
VOR Federal Airway V96 Is Amended To Read in Part
FORT WAYNE, IN VORTAC ........................................................
*16000—MCA ILLIE, OH FIX, NE BND.
**2300—MOCA.
ILLIE, OH FIX ................................................................................
*16000—MCA ANNTS, OH FIX, SW BND.
**2100—MOCA.
ANNTS, OH FIX ............................................................................
*2100—MOCA.
VerDate Sep<11>2014
5500
VOR Federal Airway V17 Is Amended To Read in Part
CAMAR, OK FIX ...........................................................................
W BND ...................................................................................
E BND ....................................................................................
§ 95.6096
MITBEE, OK VORTAC ................................................................
VOR Federal Airway V14 Is Amended To Read in Part
HOBART, OK VORTAC ................................................................
CARFF, OK FIX ............................................................................
*3500—MRA.
*DATTA, OK FIX ...........................................................................
*3500—MRA.
§ 95.6017
MEA
PO 00000
Frm 00005
*ILLIE, OH FIX .............................................................................
**5000
*ANNTS, OH FIX .........................................................................
**16000
DETROIT, MI VOR/DME .............................................................
*3000
Fmt 4700
Sfmt 4700
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30MRR1
15614
Federal Register / Vol. 82, No. 60 / Thursday, March 30, 2017 / Rules and Regulations
REVISIONS TO IFR ALTITUDES AND CHANGEOVER POINT—Continued
[Amendment 532 effective date April 27, 2017]
From
To
§ 95.6140
MEA
VOR Federal Airway V140 Is Amended By Adding
PANHANDLE, TX VORTAC .........................................................
BURNS FLAT, OK VORTAC ........................................................
*4000—MRA.
*HISLA, OK FIX .....................................................................
*4000—MRA.
**3000—MOCA.
BURNS FLAT, OK VORTAC .......................................................
*HISLA, OK FIX ...........................................................................
5300
3600
KINGFISHER, OK VORTAC .......................................................
**3600
Is Amended To Delete
PANHANDLE, TX VORTAC .........................................................
*3000—MOCA.
ZESUS, TX FIX .............................................................................
SAYRE, OK VORTAC ...................................................................
ODINS, OK FIX .............................................................................
*3100—MOCA.
§ 95.6272
ZESUS, TX FIX ...........................................................................
5800
SAYRE, OK VORTAC
W BND ..................................................................................
E BND ...................................................................................
ODINS, OK FIX ...........................................................................
KINGFISHER, OK VORTAC .......................................................
*5000
*5800
4000
*3500
VOR Federal Airway V272 Is Amended To Read in Part
BORGER, TX VORTAC ................................................................
BRISC, TX FIX ............................................................................
5000
Is Amended By Adding
BRISC, TX FIX ..............................................................................
*4500—MOCA.
BURNS FLAT, OK VORTAC ........................................................
BURNS FLAT, OK VORTAC .......................................................
*5000
WILL ROGERS, OK VORTAC ....................................................
4500
Is Amended To Delete
BRISC, TX FIX ..............................................................................
*4500—MOCA.
SAYRE, OK VORTAC ...................................................................
SERTS, OK FIX ............................................................................
*3100—MOCA.
*3700—GNSS MEA.
LIONS, OK FIX .............................................................................
§ 95.6280
SAYRE, OK VORTAC .................................................................
*5500
SERTS, OK FIX ...........................................................................
LIONS, OK FIX ............................................................................
3900
*4500
WILL ROGERS, OK VORTAC ....................................................
3300
VOR Federal Airway V280 Is Amended To Read in Part
PANHANDLE, TX VORTAC .........................................................
§ 95.6440
MITBEE, OK VORTAC ................................................................
5500
VOR Federal Airway V440 Is Amended By Adding
BRISC, TX FIX ..............................................................................
*4500—MOCA.
BURNS FLAT, OK VORTAC ........................................................
BURNS FLAT, OK VORTAC .......................................................
*5000
CARFF, OK FIX ...........................................................................
3600
Is Amended To Delete
BRISC, TX FIX ..............................................................................
*4500—MOCA.
SAYRE, OK VORTAC ...................................................................
SAYRE, OK VORTAC .................................................................
*5500
CARFF, OK FIX ...........................................................................
4000
Airway segment
Changeover points
jstallworth on DSK7TPTVN1PROD with RULES
From
To
Distance
From
§ 95.8003 VOR Federal Airway Changeover Point
V140 Is Amended To Modify Changeover Point
PANHANDLE, TX VORTAC ...........................................
V272
14:26 Mar 29, 2017
Jkt 241001
PO 00000
56
PANHANDLE.
51
BORGER.
Is Amended To Add Changeover Point
BORGER, TX VORTAC .................................................
VerDate Sep<11>2014
BURNS FLAT, OK VORTAC ........................................
BURNS FLAT, OK VORTAC ........................................
Frm 00006
Fmt 4700
Sfmt 4700
E:\FR\FM\30MRR1.SGM
30MRR1
Federal Register / Vol. 82, No. 60 / Thursday, March 30, 2017 / Rules and Regulations
Airway segment
15615
Changeover points
From
To
Distance
From
Is Amended To Delete Changeover Point
SAYRE, OK VORTAC ....................................................
[FR Doc. 2017–06294 Filed 3–29–17; 8:45 am]
BILLING CODE 4910–13–P
CONSUMER PRODUCT SAFETY
COMMISSION
16 CFR Parts 1112 and 1234
[Docket No. CPSC–2015–0019
Safety Standard for Infant Bath Tubs
Consumer Product Safety
Commission.
ACTION: Final rule.
AGENCY:
The Danny Keysar Child
Product Safety Notification Act, section
104 of the Consumer Product Safety
Improvement Act of 2008 (CPSIA),
requires the United States Consumer
Product Safety Commission
(Commission or CPSC) to promulgate
consumer product safety standards for
durable infant or toddler products.
These standards are to be ‘‘substantially
the same as’’ applicable voluntary
standards, or more stringent than the
voluntary standard if the Commission
concludes that more stringent
requirements would further reduce the
risk of injury associated with the
product. The Commission is issuing a
safety standard for infant bath tubs in
response to the direction of section
104(b) of the CPSIA. In addition, the
Commission is amending its regulations
regarding third party conformity
assessment bodies to include the
mandatory standard for infant bath tubs
in the list of notices of requirements
(NORs) issued by the Commission.
DATES: This rule will become effective
October 2, 2017. The incorporation by
reference of the publication listed in
this rule is approved by the Director of
the Federal Register as of October 2,
2017.
SUMMARY:
jstallworth on DSK7TPTVN1PROD with RULES
FOR FURTHER INFORMATION CONTACT:
Keysha Walker, Compliance Officer,
U.S. Consumer Product Safety
Commission, 4330 East West Highway,
Bethesda, MD 20814; telephone: 301–
504–6820; email: kwalker@cpsc.gov.
SUPPLEMENTARY INFORMATION:
I. Background and Statutory Authority
The CPSIA was enacted on August 14,
2008. Section 104(b) of the CPSIA, part
VerDate Sep<11>2014
14:26 Mar 29, 2017
Jkt 241001
WILL ROGERS, OK VORTAC ......................................
40
SAYRE.
of the Danny Keysar Child Product
Safety Notification Act, requires the
Commission to: (1) Examine and assess
the effectiveness of voluntary consumer
product safety standards for durable
infant or toddler products, in
consultation with representatives of
consumer groups, juvenile product
manufacturers, and independent child
product engineers and experts; and (2)
promulgate consumer product safety
standards for durable infant and toddler
products. Standards issued under
section 104 are to be ‘‘substantially the
same as’’ the applicable voluntary
standard or more stringent than the
voluntary standard if the Commission
concludes that more stringent
requirements would further reduce the
risk of injury associated with the
product.
The term ‘‘durable infant or toddler
product’’ is defined in section 104(f)(1)
of the CPSIA as ‘‘a durable product
intended for use, or that may be
reasonably expected to be used, by
children under the age of 5 years.’’
Section 104(f)(2) of the CPSIA lists
examples of durable infant or toddler
products, including products such as
‘‘bath seats’’ and ‘‘infant carriers.’’
Although section 104(f)(2) does not
specifically identify infant bath tubs, the
Commission has defined an infant bath
tub as a ‘‘durable infant or toddler
product’’ in the Commission’s product
registration card rule under CPSIA
section 104(d).1
On August 14, 2015, the Commission
issued a notice of proposed rulemaking
(NPR) for infant bath tubs. 80 FR 48769.
The NPR proposed to incorporate by
reference the voluntary standard, ASTM
F2670–13, Standard Consumer Safety
Specification for Infant Bath Tubs, with
several modifications to strengthen the
standard, as a mandatory consumer
product safety rule. In this document,
the Commission is issuing a mandatory
consumer product safety standard for
infant bath tubs. As required by section
104(b)(1)(A), the Commission consulted
with manufacturers, retailers, trade
organizations, laboratories, consumer
advocacy groups, consultants, and the
public to develop this proposed
standard, largely through the ASTM
process. Based on modifications to the
voluntary standard since the NPR
published, the final rule incorporates by
reference the most recent voluntary
standard, developed by ASTM
International, ASTM F2670–17, without
modification.
Additionally, the final rule amends
the list of NORs issued by the
Commission in 16 CFR part 1112 to
include the standard for infant bath
tubs. Under section 14 of the CPSA, the
Commission promulgated 16 CFR part
1112 to establish requirements for
accreditation of third party conformity
assessment bodies (or testing
laboratories) to test for conformity with
a children’s product safety rule.
Amending part 1112 adds an NOR for
the infant bath tub standard to the list
of children’s product safety rules.
1 Requirements for Consumer Registration of
Durable Infant or Toddler Products; Final Rule, 74
FR 68668, 68669 (Dec. 29, 2009); 16 CFR
1130.2(a)(16).
B. Market Description
Typically, infant bath tubs are
produced and/or marketed by juvenile
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
II. Product Description
A. Definition of Infant Bath Tub
Paragraph 3.1.2 of ASTM F2670–17
defines an ‘‘infant bath tub’’ as a ‘‘tub,
enclosure, or other similar product
intended to hold water and be placed
into an adult bath tub, sink, or on top
of other surfaces to provide support or
containment, or both, for an infant in a
reclining, sitting, or standing position
during bathing by a caregiver.’’
Paragraph 1.1 of the voluntary standard
specifically excludes ‘‘products
commonly known as bath slings,
typically made of fabric or mesh’’ from
the scope of the standard.
Infant bath tubs within the scope of
the final rule include products of
various designs, such as ‘‘bucket style’’
tubs that support a child sitting upright,
tubs with an inclined seat for infants too
young to sit unsupported, inflatable
tubs, folding tubs, and tubs with spa
features, such as handheld shower
attachments and even whirlpool
settings. Paragraph 6.1 of ASTM F2670–
17 permits infant bath tubs to have ‘‘a
permanent or removable passive crotch
restraint as part of their design,’’ but
does not permit ‘‘any additional
restraint system(s) which requires action
on the part of the caregiver to secure or
release.’’
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Agencies
[Federal Register Volume 82, Number 60 (Thursday, March 30, 2017)]
[Rules and Regulations]
[Pages 15612-15615]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-06294]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 95
[Docket No. 31129; Amdt. No. 532]
IFR Altitudes; Miscellaneous Amendments
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule
-----------------------------------------------------------------------
SUMMARY: This amendment adopts miscellaneous amendments to the required
IFR (instrument flight rules) altitudes and changeover points for
certain Federal airways, jet routes, or direct routes for which a
minimum or maximum en route authorized IFR altitude is prescribed. This
regulatory
[[Page 15613]]
action is needed because of changes occurring in the National Airspace
System. These changes are designed to provide for the safe and
efficient use of the navigable airspace under instrument conditions in
the affected areas.
DATES: Effective 0901 UTC, April 27, 2017.
FOR FURTHER INFORMATION CONTACT: Thomas J Nichols, Flight Procedure
Standards Branch (AMCAFS-420), Flight Technologies and Programs
Division, Flight Standards Service, Federal Aviation Administration,
Mike Monroney Aeronautical Center, 6500 South MacArthur Blvd., Oklahoma
City, OK 73169 (Mail Address: P.O. Box 25082, Oklahoma City, OK 73125)
telephone: (405) 954-4164.
SUPPLEMENTARY INFORMATION: This amendment to part 95 of the Federal
Aviation Regulations (14 CFR part 95) amends, suspends, or revokes IFR
altitudes governing the operation of all aircraft in flight over a
specified route or any portion of that route, as well as the changeover
points (COPs) for Federal airways, jet routes, or direct routes as
prescribed in part 95.
The Rule
The specified IFR altitudes, when used in conjunction with the
prescribed changeover points for those routes, ensure navigation aid
coverage that is adequate for safe flight operations and free of
frequency interference. The reasons and circumstances that create the
need for this amendment involve matters of flight safety and
operational efficiency in the National Airspace System, are related to
published aeronautical charts that are essential to the user, and
provide for the safe and efficient use of the navigable airspace. In
addition, those various reasons or circumstances require making this
amendment effective before the next scheduled charting and publication
date of the flight information to assure its timely availability to the
user. The effective date of this amendment reflects those
considerations. In view of the close and immediate relationship between
these regulatory changes and safety in air commerce, I find that notice
and public procedure before adopting this amendment are impracticable
and contrary to the public interest and that good cause exists for
making the amendment effective in less than 30 days.
Conclusion
The FAA has determined that this regulation only involves an
established body of technical regulations for which frequent and
routine amendments are necessary to keep them operationally current.
It, therefore--(1) is not a ``significant regulatory action'' under
Executive Order 12866; (2) is not a ``significant rule'' under DOT
Regulatory Policies and Procedures (44 FR 11034; February 26, 1979);
and (3) does not warrant preparation of a regulatory evaluation as the
anticipated impact is so minimal. For the same reason, the FAA
certifies that this amendment will not have a significant economic
impact on a substantial number of small entities under the criteria of
the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 95
Airspace, Navigation (air).
Issued in Washington, DC, on March 24, 2017.
John Duncan,
Director, Flight Standards Service.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, part 95 of the Federal Aviation Regulations (14 CFR part
95) is amended as follows effective at 0901 UTC, April 27,2017.
0
1. The authority citation for part 95 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40103, 40106, 40113, 40114, 40120,
44502, 44514, 44719, 44721.
0
2. Part 95 is amended to read as follows:
Revisions to IFR Altitudes and Changeover Point
[Amendment 532 effective date April 27, 2017]
------------------------------------------------------------------------
From To MEA
------------------------------------------------------------------------
Sec. 95.6001 Victor Routes--U.S.
Sec. 95.6012 VOR Federal Airway V12 Is Amended To Read in Part
------------------------------------------------------------------------
PANHANDLE, TX VORTAC............. MITBEE, OK VORTAC....... 5500
------------------------------------------------------------------------
Sec. 95.6014 VOR Federal Airway V14 Is Amended To Read in Part
------------------------------------------------------------------------
HOBART, OK VORTAC................ CARFF, OK FIX........... 3700
CARFF, OK FIX.................... *DATTA, OK FIX.......... 3000
*3500--MRA...................
*DATTA, OK FIX................... WILL ROGERS, OK VORTAC.. 3000
*3500--MRA...................
------------------------------------------------------------------------
Sec. 95.6017 VOR Federal Airway V17 Is Amended To Read in Part
------------------------------------------------------------------------
CAMAR, OK FIX.................... MITBEE, OK VORTAC.......
W BND........................ ........................ 4300
E BND........................ ........................ 4900
------------------------------------------------------------------------
Sec. 95.6096 VOR Federal Airway V96 Is Amended To Read in Part
------------------------------------------------------------------------
FORT WAYNE, IN VORTAC............ *ILLIE, OH FIX.......... **5000
*16000--MCA ILLIE, OH FIX, NE
BND.
**2300--MOCA.................
ILLIE, OH FIX.................... *ANNTS, OH FIX.......... **16000
*16000--MCA ANNTS, OH FIX, SW
BND.
**2100--MOCA.................
ANNTS, OH FIX.................... DETROIT, MI VOR/DME..... *3000
*2100--MOCA..................
------------------------------------------------------------------------
[[Page 15614]]
Sec. 95.6140 VOR Federal Airway V140 Is Amended By Adding
------------------------------------------------------------------------
PANHANDLE, TX VORTAC............. BURNS FLAT, OK VORTAC... 5300
BURNS FLAT, OK VORTAC............ *HISLA, OK FIX.......... 3600
*4000--MRA...................
*HISLA, OK FIX............... KINGFISHER, OK VORTAC... **3600
*4000--MRA...................
**3000--MOCA.................
------------------------------------------------------------------------
Is Amended To Delete
------------------------------------------------------------------------
PANHANDLE, TX VORTAC............. ZESUS, TX FIX........... 5800
*3000--MOCA..................
ZESUS, TX FIX.................... SAYRE, OK VORTAC
W BND................ *5000
E BND................ *5800
SAYRE, OK VORTAC................. ODINS, OK FIX........... 4000
ODINS, OK FIX.................... KINGFISHER, OK VORTAC... *3500
*3100--MOCA..................
------------------------------------------------------------------------
Sec. 95.6272 VOR Federal Airway V272 Is Amended To Read in Part
------------------------------------------------------------------------
BORGER, TX VORTAC................ BRISC, TX FIX........... 5000
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Is Amended By Adding
------------------------------------------------------------------------
BRISC, TX FIX.................... BURNS FLAT, OK VORTAC... *5000
*4500--MOCA..................
BURNS FLAT, OK VORTAC............ WILL ROGERS, OK VORTAC.. 4500
------------------------------------------------------------------------
Is Amended To Delete
------------------------------------------------------------------------
BRISC, TX FIX.................... SAYRE, OK VORTAC........ *5500
*4500--MOCA..................
SAYRE, OK VORTAC................. SERTS, OK FIX........... 3900
SERTS, OK FIX.................... LIONS, OK FIX........... *4500
*3100--MOCA..................
*3700--GNSS MEA..............
LIONS, OK FIX.................... WILL ROGERS, OK VORTAC.. 3300
------------------------------------------------------------------------
Sec. 95.6280 VOR Federal Airway V280 Is Amended To Read in Part
------------------------------------------------------------------------
PANHANDLE, TX VORTAC............. MITBEE, OK VORTAC....... 5500
------------------------------------------------------------------------
Sec. 95.6440 VOR Federal Airway V440 Is Amended By Adding
------------------------------------------------------------------------
BRISC, TX FIX.................... BURNS FLAT, OK VORTAC... *5000
*4500--MOCA..................
BURNS FLAT, OK VORTAC............ CARFF, OK FIX........... 3600
------------------------------------------------------------------------
Is Amended To Delete
------------------------------------------------------------------------
BRISC, TX FIX.................... SAYRE, OK VORTAC........ *5500
*4500--MOCA..................
SAYRE, OK VORTAC................. CARFF, OK FIX........... 4000
------------------------------------------------------------------------
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Airway segment Changeover points
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From To Distance From
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Sec. 95.8003 VOR Federal Airway Changeover Point
V140 Is Amended To Modify Changeover Point
----------------------------------------------------------------------------------------------------------------
PANHANDLE, TX VORTAC.................. BURNS FLAT, OK VORTAC......... 56 PANHANDLE.
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V272 Is Amended To Add Changeover Point
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BORGER, TX VORTAC..................... BURNS FLAT, OK VORTAC......... 51 BORGER.
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[[Page 15615]]
Is Amended To Delete Changeover Point
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SAYRE, OK VORTAC...................... WILL ROGERS, OK VORTAC........ 40 SAYRE.
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[FR Doc. 2017-06294 Filed 3-29-17; 8:45 am]
BILLING CODE 4910-13-P