[Federal Register: January 18, 2011 (Volume 76, Number 11)]
[Proposed Rules]
[Page 2846-2848]
[DOCID:fr18ja11-18]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1312; Directorate Identifier 2010-NM-220-AD]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Model 777-200, -
200LR, -300, and -300ER Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of Proposed Rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD would require installing
foreign object debris (FOD) rubber shields over the primary and
secondary external power connectors for certain airplanes, and wrapping
fire-resistant silicone tape around the hydraulic tube for certain
other airplanes. This proposed AD was prompted by a report of a fire in
the main equipment center due to failure of an external power
connector, which caused high-temperature arcing and subsequent splatter
of molten copper on an adjacent hydraulic tube, creating a hole in the
tube and spraying hydraulic fluid into the power connector, resulting
in a fire. In addition there were several reports of overheating or
arcing of external power connectors, and one report of a fire due to
arcing caused by FOD. We are proposing this AD to prevent FOD from
entering the primary and secondary external power connectors, which
could result in overheating or arcing and consequent fire in the main
equipment center.

DATES: We must receive comments on this proposed AD by March 4, 2011.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://
www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management, P.
O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-
544-5000, extension 1; fax<PHONE_NUMBER>; e-mail<EMAIL_ADDRESS>
Internet https://www.myboeingfleet.com. You may review copies of the
referenced service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; 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 proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Office (phone:<PHONE_NUMBER>) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.

FOR FURTHER INFORMATION CONTACT: Georgios Roussos, Aerospace Engineer,
Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98057-
3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; e-mail:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2010-1312;
Directorate Identifier 2010-NM-220-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of 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 proposed AD.

Discussion

    We received a report of a fire in the main equipment center due to
failure of an external power connector, which caused high-temperature
arcing and subsequent splatter of molten copper on an adjacent
hydraulic tube, creating a hole in the tube and spraying hydraulic
fluid into the power connector, resulting in a fire. In addition there
were several reports of overheating or arcing of external power
connectors, and one report of a fire due to arcing caused by FOD.
During one incident a fire occurred on an airplane in the factory at
the secondary external power connector location. Investigation revealed
that the overheating and arcing events were caused by FOD; during a
maintenance check a washer was found inside the external power
connector. FOD in the primary and secondary external power connectors
could result in overheating or arcing and consequent fire in the main
equipment center.

Relevant Service Information

    We reviewed Boeing Special Attention Service Bulletin 777-29-0032,
dated August 9, 2007 (for Model 777-200, -200LR, -300, and -300ER
airplanes); and Boeing Service Bulletin 777-24-0102, Revision 1, dated
June 17, 2010 (for Model 777-200, -200LR, -300, and -300ER airplanes
that require rubber FOD shields).
    Boeing Special Attention Service Bulletin 777-29-0032, dated August
9, 2007, describes procedures for wrapping self-fusing fire-resistant
silicone tape around the alternate extension hydraulic tube section of
the nose landing gear adjacent to the P30 panel.
    Boeing Service Bulletin 777-24-0102, Revision 1, dated June 17,
2010, describes procedures for installing new FOD rubber shields over
the primary and secondary external power connectors at approximately
station 350 in the main equipment center.

FAA's Determination

    We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

Proposed AD Requirements

    This proposed AD would require accomplishing the actions specified
in the service information described previously, except as discussed
under ``Difference Between the Proposed AD and the Service
Information.''

Difference Between the Proposed AD and the Service Information

    Boeing Service Bulletin 777-24-0102, Revision 1, dated June 17,
2010, does not provide a compliance time for installing new FOD rubber
shields; however, this proposed AD requires that installation be done
within 36 months after the effective date of this AD. We considered the
manufacturer's

recommendation that the compliance time coincide with the compliance
time specified in Boeing Special Attention Service Bulletin 777-29-
0032, dated August 9, 2007.

Costs of Compliance

    We estimate that this proposed AD will affect 126 airplanes of U.S.
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Number of
               Action                       Labor cost         Parts cost    Cost per    airplanes    Fleet cost
                                                                             product      affected
----------------------------------------------------------------------------------------------------------------
Install FOD rubber shields..........  6 work-hour x $85 per          $134         $644          124      $79,856
                                       hour = $510.
Wrap silicone tape..................  2 work-hour x $85 per            $0         $170          126      $21,420
                                       hour = $170.
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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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
    (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.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

    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]

    2. The FAA amends Sec.  39.13 by adding the following new
airworthiness directive (AD):

The Boeing Company: Docket No. FAA-2010-1312; Directorate Identifier
2010-NM-220-AD.

Comments Due Date

    (a) We must receive comments by March 4, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all The Boeing Company Model 777-200, -
200LR, -300, and -300ER series airplanes; certificated in any
category.

Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport
Association (ATA) of America Codes 29: Hydraulic power; and 24:
Electrical power.

Unsafe Condition

    (e) This AD was prompted by a report of a fire in the main
equipment center due to failure of an external power connector,
which caused high-temperature arcing and subsequent splatter of
molten copper on an adjacent hydraulic tube, creating a hole in the
tube and spraying hydraulic fluid into the power connector,
resulting in a fire. In addition there were several reports of
overheating or arcing of external power connectors, and one report
of a fire due to arcing caused by foreign object damage (FOD). We
are issuing this AD to prevent FOD from entering the primary and
secondary external power connectors, which could result in
overheating or arcing, and consequent fire in the main equipment
center.

Compliance

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

Modification

    (g) Within 36 months after the effective date of this AD, do the
actions required by paragraphs (g)(1) and (g)(2) of this AD.
    (1) For airplanes identified in Boeing Service Bulletin 777-24-
0102, Revision 1, dated June 17, 2010: Install FOD rubber shields
over the primary and secondary external power connectors, in
accordance with the Accomplishment Instructions of Boeing Service
Bulletin 777-24-0102, Revision 1, dated June 17, 2010.
    (2) For airplanes identified in Boeing Special Attention Service
Bulletin 777-29-0032, dated August 9, 2007: Wrap fire-resistant
silicone tape around the hydraulic tube, in accordance with the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 777-29-0032, dated August 9, 2007.

Exception to Service Information

    (h) Figure 1 of the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 777-29-0032, dated August 9,
2007, does not identify the dimensions of the electrical tape which
is installed on the hydraulic tube; those dimensions should be
measured in inches.

Credit for Actions Accomplished in Accordance With Previous Service
Information

    (i) Actions done before the effective date of this AD in
accordance with Boeing Service Bulletin 777-24-0102, dated July 12,
2007, are acceptable for compliance with the corresponding
requirements of this paragraph (g)(1) of this AD.

Alternative Methods of Compliance (AMOCs)

    (j)(1) The Manager, Seattle Aircraft Certification Office (ACO),
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 manager of the ACO, send it to the attention of the
person identified in the Related Information section of this AD.
Information may be e-mailed to: 9-ANM-Seattle-ACO-AMOC-
<EMAIL_ADDRESS>    (2) Before using any approved AMOC, notify your Principal
Maintenance Inspector or Principal Avionics Inspector, as
appropriate, or lacking a principal inspector, your local Flight
Standards District Office.

Related Information

    (k) For more information about this AD, contact Georgios
Roussos, Aerospace Engineer, Systems and Equipment Branch, ANM-130S,
FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone<PHONE_NUMBER>; fax (425)
917-6590; e-mail<EMAIL_ADDRESS>    (l) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone
206-544-5000, extension 1; fax<PHONE_NUMBER>; e-mail
<EMAIL_ADDRESS>Internet https://www.myboeingfleet.com. You
may review copies of the referenced service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.

    Issued in Renton, Washington on January 10, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-876 Filed 1-14-11; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 77, Number 79 (Tuesday, April 24, 2012)]
[Rules and Regulations]
[Pages 24364-24366]
[FR Doc No: 2012-9194]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-1228; Directorate Identifier 2011-NM-176-AD;
Amendment 39-17022; AD 2012-08-05]
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 CL-600-2C10 (Regional Jet Series 700, 701, &
702), CL-600-2D15 (Regional Jet Series 705), CL-600-2D24 (Regional Jet
Series 900), and CL-600-2E25 (Regional Jet Series 1000) airplanes. This
AD was prompted by reports of the air driven generator (ADG) failing to
power essential buses during functional tests, due to the low threshold
setting of the circuit protection on the ADG's generator control unit
(GCU) preventing the ADG from supplying power to the essential buses.
This AD requires installing a new

or serviceable ADG GCU. We are issuing this AD to prevent loss of power
from the ADG to the essential buses which, in the event of an
emergency, could prevent continued safe flight.

DATES: This AD becomes effective May 29, 2012.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 29,
2012.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Assata Dessaline, Aerospace Engineer,
Avionics and Flight Test Branch, ANE-172, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
New York 11590; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on November 8, 2011 (76
FR 69166). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:

    There have been several occurrences of the air driven generator
(ADG) failure to power essential buses during functional tests of
the ADG on aeroplane models CL-600-2B16 and CL-600-2B19. The
aeroplane models CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-
2E25 use the same ADG generator control unit (GCU) as models CL-600-
2B16 and CL-600-2B19. However the aeroplane models CL-600-2C10, CL-
600-2D15, CL-600-2D24, and CL-600-2E25 are installed with a
different hydraulic pump and do not experience the same failure due
to the low threshold setting of the circuit protection.
    However, it was found that the same ADG GCU transformer primary
winding can break due to thermal fatigue. Broken transformer primary
winding can prevent the supply of power from the ADG to the
essential buses. In the event of an emergency, failure for the
essential buses to remain powered can prevent continued safe flight.
    This [TCCA] directive mandates the replacement of the ADG GCU.

You may obtain further information by examining the MCAI in the AD
docket.

Comments

    We gave the public the opportunity to participate in developing
this AD. We have considered the comments received.

Request To Shorten the Compliance Time

    The Air Line Pilots Association, International (ALPA) requested the
compliance time of ``10,000 flight hours or 60 months after the
effective date of the AD'' be reduced, because ALPA believes that the
compliance time is too long to comply with the proposed AD (76 FR
69166, November 8, 2011) based on the importance of replacement.
    We do not agree to shorten the compliance time. In developing the
compliance time, we determined that the compliance time of 10,000
flight hours or 60 months after the effective date of the AD (whichever
is first), is appropriate when considering the safety implications, the
average utilization rate of the affected fleet, the practical aspects
of an orderly inspection of the fleet during regular maintenance
periods, and the availability of required replacement parts. In
addition, our compliance time corresponds with the 10,000-flight-hour
or 60-month compliance time of the parallel AD issued by Transport
Canada Civil Aviation (TCCA). We have not changed the AD in this
regard.

Request To Reference Hamilton Sundstrand's Part Number

    Comair, Inc. requested that we revise paragraphs (g) and (h) of the
NPRM (76 FR 69166, November 8, 2011) to reference Hamilton Sundstrand's
part number, in addition to the Bombardier part numbers for the ADG
GCU, because by doing so, Comair believes the proposed AD will make
certain all suspect ADG GCUs are removed and replaced and will be
congruent with the manufacturer's manual.
    We agree with the request to reference the Hamilton Sundstrand part
number for the ADG GCU unit that is affected and not higher assembly
part numbers. Bombardier Service Bulletin 670BA-24-031, dated May 30,
2011, refers to Hamilton Sundstrand Service Bulletin ERPS10G-24-1,
dated February 9, 2011, as an additional source of guidance for
modifying and testing the ADG GCU with new printed wiring assemblies
and re-identifying the GCU with a new part number. We have updated
paragraphs (g) and (h) of this AD to include the Hamilton Sundstrand
part number.

Explanation of Change to Costs of Compliance Section

    The Costs of Compliance section in this AD has been updated to show
a more accurate cost to operators. The work-hours quoted in Bombardier
Service Bulletin 670BA-24-031, dated May 30, 2011, include only the
labor time required for replacement, while Hamilton Sundstrand Service
Bulletin ERPS10G-24-1, dated February 9, 2011, estimates 4 work-hours
for replacement of the printed wiring assemblies from the GCU and
functional testing of the ADG. Because it may be necessary to do a non-
destructive test (NDT) inspection on some airplanes, we have added an
additional work-hour, resulting in a total labor time estimate of 6
work-hours in the Costs of Compliance section of this AD.

Conclusion

    We reviewed the available data, including the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously. We determined that these
changes will not increase the economic burden on any operator or
increase the scope of the AD.

Costs of Compliance

    Based on the service information, we estimate that this AD affects
402 products of U.S. registry. We also estimate that it takes 6 work-
hours per product to comply with the basic requirements of this AD. The
average labor rate is $85 per work-hour. Required parts cost $0 per
product. Where the service information lists required parts costs that
are covered under warranty, we have assumed that there will be no
charge for these parts. As we do not control warranty coverage for
affected parties, some parties may incur costs higher than estimated
here. Based on these figures, we estimate the cost of this AD on U.S.
operators to be $205,020, or $510 per product.

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.
    We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; 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 the NPRM (76 FR 69166, November 8,
2011), the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone<PHONE_NUMBER>) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

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 AD:

2012-08-05 Bombardier, Inc.: Amendment 39-17022. Docket No. FAA-
2011-1228; Directorate Identifier 2011-NM-176-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective May 29,
2012.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the airplanes, certificated in any category,
identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD.
    (1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700,
701, & 702) airplanes, serial numbers 10003 through 10319 inclusive.
    (2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705)
and CL-600-2D24 (Regional Jet Series 900) airplanes, serial numbers
15001 through 15260 inclusive.
    (3) Bombardier, Inc. Model CL-600-2E25 (Regional Jet Series
1000) airplanes, serial numbers 19001 through 19012 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 24: Electrical
Power.

(e) Reason

    This AD was prompted by reports of the air driven generator
(ADG) failing to power essential buses during functional tests, due
to the low threshold setting of the circuit protection on the ADG's
generator control unit (GCU) preventing the ADG from supplying power
to the essential buses. We are issuing this AD to prevent loss of
power from the ADG to the essential buses which, in the event of an
emergency, could prevent continued safe flight.

(f) Compliance

    You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.

(g) Actions

    Within 10,000 flight hours or 60 months after the effective date
of this AD, whichever occurs first, remove the ADG GCU, Bombardier
part number (P/N) 604-90800-7 (Hamilton Sundstrand P/N 761341A) and
install a new or serviceable ADG GCU, Bombardier P/N 604-90800-27
(Hamilton Sundstrand P/N 761341B), in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 670BA-24-
031, dated May 30, 2011.

(h) Parts Installation

    As of the effective date of this AD, no person may install an
ADG GCU, Bombardier P/N 604-90800-7 (Hamilton Sundstrand P/N
761341A) on any airplane.

(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, New York 11590; telephone<PHONE_NUMBER>; fax 516-794-
5531. 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) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.

(j) Related Information

    Refer to MCAI Canadian Airworthiness Directive CF-2011-27, dated
July 25, 2011; and Bombardier Service Bulletin 670BA-24-031, dated
May 30, 2011; for related information.

(k) Material Incorporated by Reference

    (1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) of the following service information under 5 U.S.C.
552(a) and 1 CFR part 51:
    (i) Bombardier Service Bulletin 670BA-24-031, dated May 30,
2011.
    (2) 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.
    (3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.
    (4) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at an NARA facility, call<PHONE_NUMBER>, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on April 6, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-9194 Filed 4-23-12; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 81, Number 102 (Thursday, May 26, 2016)]
[Notices]
[Pages 33526-33527]
[FR Doc No: 2016-12421]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. AD16-17-000]

Reactive Supply Compensation in Markets Operated by Regional
Transmission Organizations and Independent System Operators;
Supplemental Notice of Workshop

    As announced in the Notice of Workshop issued on March 17, 2016, in
the above-captioned proceeding,\1\ Federal Energy Regulatory Commission
(Commission) staff will convene a workshop on June 30, 2016, from 12:00
p.m. (EDT) to 4:00 p.m. (EDT) in the Commission Meeting Room at 888
First Street NE., Washington, DC 20426. The workshop will be open to
the public, and all interested parties are invited to attend and
participate. The workshop will be led by Commission staff, and may be
attended by one or more Commissioners.
---------------------------------------------------------------------------

    \1\ Reactive Supply Compensation in Markets Operated by Regional
Transmission Organizations and Independent System Operators, Docket
No. AD16-17-000 (Mar. 17, 2016) (Notice of Workshop).
---------------------------------------------------------------------------

    The purpose of the workshop is to discuss compensation for Reactive
Supply and Voltage Control (Reactive Supply) within the Regional
Transmission Organizations (RTOs) and Independent System Operators
(ISOs). Specifically, the workshop will explore the types of costs
incurred by generators for providing Reactive Supply capability and
service; whether those costs are being recovered solely as compensation
for Reactive Supply or whether recovery is also through compensation
for other services; and different methods by which generators receive
compensation for Reactive Supply (e.g., Commission-approved revenue
requirements, market-wide rates, etc.). The workshop will also explore
potential adjustments in compensation methods based on changes in
Reactive Supply capability and potential mechanisms to prevent
overcompensation for Reactive Supply.
    Attached to this supplemental notice is an agenda for the workshop,
including Reactive Supply compensation topics to be considered for
discussion at the workshop. Questions that speakers should be prepared
to discuss are grouped by topic.
    Discussions at the workshop may involve issues raised in
proceedings that are pending before the Commission. These proceedings
include, but are not limited to:

------------------------------------------------------------------------

------------------------------------------------------------------------
ISO New England Inc....................  Docket No. ER16-946-001.
Garrison Energy Center, LLC............  Docket No. ER15-2735-000.
Newark Energy Center, LLC..............  Docket Nos. ER15-1706-001, EL15-
                                          97-000.
Scrubgrass Generating Company, L.P.....  Docket No. ER15-2254-000.
CPV Shore, LLC.........................  Docket Nos. ER15-2589-000, EL16-
                                          4-000.
C.P. Crane LLC.........................  Docket Nos. ER16-259-000, ER16-
                                          332-000, EL16-21-000.
GenOn Energy Management, LLC...........  Docket Nos. ER15-2571-000, ER15-
                                          2572-000, ER15-2573-000.
NRG Wholesale Generation LP............  Docket Nos. ER16-413-000, ER04-
                                          1164-001, EL16-28-000.
Talen Energy Marketing, LLC............  Docket Nos. ER16-277-000, ER16-
                                          277-001, ER16-277-002, ER16-
                                          277-003, EL16-44-000, EL16-44-
                                          001, ER08-1462-001, EL16-32-
                                          000, ER16-1456-000.
Constellation Power Source Generation,   Docket Nos. ER16-746-000, ER16-
 LLC.                                     746-001.
New Covert Generating Company, LLC.....  Docket No. ER16-1226-000.
Panda Liberty LLC......................  Docket No. ER16-1256-001.
Roundtop Energy LLC....................  Docket No. ER16-1004-000.
Beaver Dam Energy LLC..................  Docket Nos. ER16-1032-000, EL16-
                                          51-000.
FirstEnergy Solutions Corp.............  Docket Nos. ER15-1510-000, ER15-
                                          1510-001.
Duke Energy Indiana, Inc...............  Docket Nos. ER16-200-000, ER16-
                                          201-000, ER16-200-002.
Wabash Valley Power Association, Inc...  Docket Nos. ER16-435-001, ER16-
                                          444-001.
Consumers Energy Company...............  Docket No. ER16-1058-000.
MidAmerican Energy Company.............  Docket No. ER16-1062-000.
Indiana Municipal Power Agency.........  Docket No. EL16-14-000.
BIF III Holtwood LLC...................  Docket No. ER16-1530-000.
Seward Generation, LLC.................  Docket No. ER16-1344-000.
Northampton Generating Company, L.P....  Docket No. ER13-1431-001.
------------------------------------------------------------------------

    This workshop will be transcribed and webcast. Transcripts of the
workshop will be available for a fee from Ace-Federal Reporters, Inc.
at<PHONE_NUMBER>. A free webcast of this event will be available
through www.ferc.gov. Anyone with internet access who wants to view
this event can do so by navigating to the Calendar of Events at
www.ferc.gov and locating this event in the Calendar. The event will
contain a link to its webcast. The Capitol

Connection provides technical support for webcasts and offers the
option of listening to the workshop via phone-bridge for a fee. If you
have any questions, visit www.CapitolConnection.org or call (703) 993-
3100. Those interested in attending the workshop or viewing the webcast
are encouraged to register at https://www.ferc.gov/whats-new/registration/06-30-16-form.asp.
    Commission workshops are accessible under section 508 of the
Rehabilitation Act of 1973. For accessibility accommodations, please
send an email to<EMAIL_ADDRESS>call<PHONE_NUMBER> (toll
free) or<PHONE_NUMBER> (TTY), or send a FAX to<PHONE_NUMBER> with the
required accommodations.
    Those who wish to file written comments may do so by July 28, 2016.
The Commission strongly encourages electronic filing. Please file
comments using the Commission's eFiling system at http://www.ferc.gov/docs-filing/efiling.asp. For assistance, please contact FERC Online
Support at<EMAIL_ADDRESS>(866) 208-3676 (toll free), or
(202) 502-8659 (TTY). In lieu of electronic filing, please send a paper
copy to: Secretary, Federal Energy Regulatory Commission, 888 First
Street NE., Washington, DC 20426. The first page of any filing should
include docket number AD16-17-000.
    All comments will be placed in the Commission's public files and
will be available for review at the Commission in the Public Reference
Room or may be viewed on the Commission's Web site at www.ferc.gov
using the eLibrary link. Enter AD16-17-000 in the docket number field
to access documents. For assistance, please contact FERC Online
Support.
    For more information about this workshop, please contact:

Sam Wellborn (Technical Information), Office of Energy Market
Regulation--East, Federal Energy Regulatory Commission, 888 First
Street NE., Washington, DC 20426,<PHONE_NUMBER>,
<EMAIL_ADDRESS>Gretchen Kershaw (Legal Information), Office of the General Counsel,
Federal Energy Regulatory Commission, 888 First Street NE., Washington,
DC 20426,<PHONE_NUMBER><EMAIL_ADDRESS>Sarah McKinley (Logistical Information), Office of External Affairs,
Federal Energy Regulatory Commission, 888 First Street NE., Washington,
DC 20426,<PHONE_NUMBER><EMAIL_ADDRESS>
    Dated: May 19, 2016.
Kimberly D. Bose,
Secretary.
[FR Doc. 2016-12421 Filed 5-25-16; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 79, Number 168 (Friday, August 29, 2014)]
[Rules and Regulations]
[Pages 51471-51475]
[FR Doc No: 2014-20707]

=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 95

[Docket No. 30976; Amdt. No. 515]

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 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 Date: 0901 UTC, September 18, 2014.

FOR FURTHER INFORMATION CONTACT: Harry Hodges, 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:<PHONE_NUMBER>.

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 14 August 2014.
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, June 03, 2010.

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 515 Effective Date September 18, 2014]
------------------------------------------------------------------------
              From                          To                  MEA
------------------------------------------------------------------------
                    Sec.   95.6001 Victor Routes--U.S
     Sec.   95.6003 VOR Federal Airway V3 Is Amended To Read in Part
------------------------------------------------------------------------
Fort Lauderdale, FL VOR/DME....  Palm Beach, FL VORTAC..            2000
------------------------------------------------------------------------
     Sec.   95.6005 VOR Federal Airway V5 Is Amended To Read in Part
------------------------------------------------------------------------
Athens, GA VORTAC..............  Irmos, GA FIX..........            3100
------------------------------------------------------------------------
    Sec.   95.6034 VOR Federal Airway V34 Is Amended To Read in Part
------------------------------------------------------------------------
Hancock, NY VOR/DME............  Rimba, NY FIX..........            6400
------------------------------------------------------------------------
    Sec.   95.6051 VOR Federal Airway V51 Is Amended To Read in Part
------------------------------------------------------------------------
Athens, GA VORTAC..............  Irmos, GA FIX..........            3100
------------------------------------------------------------------------
    Sec.   95.6068 VOR Federal Airway V68 Is Amended To Read in Part
------------------------------------------------------------------------
Crays, TX FIX..................  Industry, TX VORTAC....            2600
------------------------------------------------------------------------
    Sec.   95.6123 VOR Federal Airway V123 Is Amended To Read in Part
------------------------------------------------------------------------
Mitch, MD FIX..................  Swann, MD FIX..........           *7000
    *3000--GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6144 VOR Federal Airway V144 Is Amended To Read in Part
------------------------------------------------------------------------
Kessel, WV VOR/DME.............  Linden, VA VORTAC......            5500
------------------------------------------------------------------------
    Sec.   95.6154 VOR Federal Airway V154 Is Amended To Read in Part
------------------------------------------------------------------------
Macon, GA VORTAC...............  Dublin, GA VORTAC......   2300
    Macon R-099
     Unusable use Dublin R-286
------------------------------------------------------------------------
    Sec.   95.6198 VOR Federal Airway V198 Is Amended To Read in Part
------------------------------------------------------------------------
San Antonio, TX VORTAC.........  Seeds, TX FIX..........            2900
Seeds, TX FIX..................  Wemar, TX FIX..........           *2500
    *2000--MOCA
------------------------------------------------------------------------
    Sec.   95.6199 VOR Federal Airway V199 Is Amended To Read in Part
------------------------------------------------------------------------
Mendocino, CA VORTAC...........  *Henle, CA FIX.........            9000
    *5800--MCA Henle, CA FIX, S
     BND
------------------------------------------------------------------------
    Sec.   95.6210 VOR Federal Airway V210 Is Amended To Read in Part
------------------------------------------------------------------------
Aples, CA FIX..................  Hector, CA VORTAC......            7900
------------------------------------------------------------------------
    Sec.   95.6212 VOR Federal Airway V212 Is Amended To Read in Part
------------------------------------------------------------------------
Seeds, TX FIX..................  Wemar, TX FIX..........           *2500
    *2000--MOCA
------------------------------------------------------------------------
    Sec.   95.6222 VOR Federal Airway V222 Is Amended To Read in Part
------------------------------------------------------------------------
Stonewall, TX VORTAC...........  Marcs, TX FIX..........            4500
Crays, TX FIX..................  Industry, TX VORTAC....            2600
------------------------------------------------------------------------
    Sec.   95.6248 VOR Federal Airway V248 Is Amended To Read in Part
------------------------------------------------------------------------
Salinas, CA VORTAC.............  *Sardo, CA FIX.........          **6000
    *5500--MRA
    *6000--MCA Sardo, CA FIX,
     NW BND
    **5500--MOCA
------------------------------------------------------------------------
    Sec.   95.6259 VOR Federal Airway V259 Is Amended To Read in Part
------------------------------------------------------------------------
Barretts Mountain, NC VOR/DME..  Gowbe, NC FIX
                                 SE BND.................            5000
                                 NW BND.................            7500
Gowbe, NC FIX..................  *Holston Mountain, TN              7500
                                  VORTAC.

    *6600--MCA Holston
     Mountain, TN VORTAC, SE
     BND
------------------------------------------------------------------------
    Sec.   95.6266 VOR Federal Airway V266 Is Amended To Read in Part
------------------------------------------------------------------------
Greensboro, NC VORTAC..........  South Boston, VA VORTAC            2700
------------------------------------------------------------------------
    Sec.   95.6267 VOR Federal Airway V267 Is Amended To Read in Part
------------------------------------------------------------------------
Athens, GA VORTAC..............  Irmos, GA FIX..........            3100
------------------------------------------------------------------------
    Sec.   95.6286 VOR Federal Airway V286 Is Amended To Read in Part
------------------------------------------------------------------------
Elkins, WV VORTAC..............  Derin, WV FIX..........
                                 W BND..................            5700
                                 E BND..................            6200
Derin, WV FIX..................  Teakk, VA FIX..........            6900
Teakk, VA FIX..................  Casanova, VA VORTAC
                                 W BND..................           *6900
                                 E BND..................           *6500
    *5800--MOCA
------------------------------------------------------------------------
    Sec.   95.6292 VOR Federal Airway V292 Is Amended To Read in Part
------------------------------------------------------------------------
Hancock, NY VOR/DME............  Sages, NY FIX..........            6400
Sages, NY FIX..................  Wigan, NY FIX..........    000
    Unusable
Wigan, NY FIX..................  Barnes, MA VORTAC......  *1000
                                                                       0
    *4900--MOCA
    Barnes R-279
     Unusable BYD 50 NM
------------------------------------------------------------------------
    Sec.   95.6310 VOR Federal Airway V310 Is Amended To Read in Part
------------------------------------------------------------------------
Rosar, KY FIX..................  *Holston Mountain, TN              6400
                                  VORTAC.
    *6600--MCA Holston
     Mountain, TN VORTAC, E BND
Holston Mountain, TN VORTAC....  *Stain, TN FIX.........            6700
    *7000--MCA Stain, TN FIX, E
     BND
Stain, TN FIX..................  *Mulbe, NC FIX.........            7800
    *7100--MCA Mulbe, NC FIX, W
     BND
------------------------------------------------------------------------
    Sec.   95.6394 VOR Federal Airway V394 Is Amended To Read in Part
------------------------------------------------------------------------
Aples, CA FIX..................  Basal, CA FIX..........            7900
Basal, CA FIX..................  Daggett, CA VORTAC.....            7500
------------------------------------------------------------------------
    Sec.   95.6402 VOR Federal Airway V402 Is Amended To Read in Part
------------------------------------------------------------------------
Panhandle, TX VORTAC...........  *Brisc, TX FIX.........          **7000
    *7000--MRA
    **5000--MOCA
------------------------------------------------------------------------
    Sec.   95.6417 VOR Federal Airway V417 Is Amended To Read in Part
------------------------------------------------------------------------
Irmos, GA FIX..................  Athens, GA VORTAC......            3100
------------------------------------------------------------------------
    Sec.   95.6440 VOR Federal Airway V440 Is Amended To Read in Part
------------------------------------------------------------------------
Panhandle, TX VORTAC...........  *Brisc, TX FIX.........          **7000
    *7000--MRA
    **5000--MOCA
------------------------------------------------------------------------
    Sec.   95.6445 VOR Federal Airway V445 Is Amended To Read in Part
------------------------------------------------------------------------
Mitch, MD FIX..................  Swann, MD FIX..........           *7000
    *3000--GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6475 VOR Federal Airway V475 Is Amended To Read in Part
------------------------------------------------------------------------
Madison, CT VOR/DME............  Norwich, CT VOR/DME....   2600
    Madison R-078
     Unusable BYD 16 NM Use
     Norwich R-259
------------------------------------------------------------------------

    Sec.   95.6556 VOR Federal Airway V556 Is Amended To Read in Part
------------------------------------------------------------------------
Stonewall, TX VORTAC...........  Marcs, TX FIX..........            4500
Seeds, TX FIX..................  Wemar, TX FIX..........           *2500
    *2000--MOCA
------------------------------------------------------------------------
    Sec.   95.6605 VOR Federal Airway V605 Is Amended To Read in Part
------------------------------------------------------------------------
Spartanburg, SC VORTAC.........  *Genod, NC FIX.........         **15000
    *15000--MRA
    **4500--MOCA
    **5000--GNSS MEA
*Genod, NC FIX.................  **Holston Mountain, TN             8500
                                  VORTAZ.
    *15000--MRA
    **6000--MCA Holston
     Mountain, TN VORTAC, S BND
------------------------------------------------------------------------

                    From                                      To                        MEA             MAA
----------------------------------------------------------------------------------------------------------------
                                            Sec.   95.7001 Jet Routes
                                Sec.   95.7064 Jet Route J64 Is Amended To Delete
----------------------------------------------------------------------------------------------------------------
Ravine, PA VORTAC..........................  Robbinsville, NJ VORTAC............           18000           45000
----------------------------------------------------------------------------------------------------------------
                                           Is Amended To Read in Part
----------------------------------------------------------------------------------------------------------------
Ravine, PA VORTAC..........................  Saraa, PA FIX......................           18000           45000
----------------------------------------------------------------------------------------------------------------
                                Sec.   95.7077 Jet Route J77 Is Amended To Delete
----------------------------------------------------------------------------------------------------------------
Boston, MA VOR/DME.........................  Barnes, MA VORTAC..................           18000           45000
Barnes, MA VORTAC..........................  Sparta, NJ VORTAC..................           18000           31000
Sparta, NJ VORTAC..........................  Broadway, NJ VOR/DME...............           18000           45000
Broadway, NJ VOR/DME.......................  Pottstown, PA VORTAC...............           18000           45000
Pottstown, PA VORTAC.......................  Westminster, MD VORTAC.............           18000           45000
----------------------------------------------------------------------------------------------------------------
                                Sec.   95.7080 Jet Route J80 Is Amended To Delete
----------------------------------------------------------------------------------------------------------------
Bellaire, OH VOR/DME.......................  Vinse, PA FIX......................           18000           45000
Vinse, PA FIX..............................  Kippi, PA FIX......................           26000           45000
Kippi, PA FIX..............................  East Texas, PA VOR/DME.............           18000           38000
East Texas, PA VOR/DME.....................  Sparta, NJ VORTAC..................           18000           32000
Sparta, NJ VORTAC..........................  Barnes, MA VORTAC..................           18000           31000
Barnes, MA VORTAC..........................  Bangor, ME VORTAC..................           18000           45000
----------------------------------------------------------------------------------------------------------------
                                            Sec.   95.7001 Jet Routes
                            Sec.   95.7502 Jet Route J502 Is Amended To Read in Part
----------------------------------------------------------------------------------------------------------------
U.S. Canadian Border.......................  Annette Island, AK VOR/DME.........           22000           45000
----------------------------------------------------------------------------------------------------------------

                            Airway segment                                             Changeover
----------------------------------------------------------------------------------------------------------------
                 From                                 To                  Distance                From
----------------------------------------------------------------------------------------------------------------
                               Sec.   95.8003 VOR Federal Airway Changeover Point
                                     V198 Is Amended To Add Changeover Point
----------------------------------------------------------------------------------------------------------------
San Antonio, TX VORTAC................  Eagle Lake, TX VOR/DME.......              63  San Antonio.
----------------------------------------------------------------------------------------------------------------
                                     V212 Is Amended To Add Changeover Point
----------------------------------------------------------------------------------------------------------------
San Antonio, TX VORTAC................  Eagle Lake, TX VOR/DME.......              63  San Antonio.
----------------------------------------------------------------------------------------------------------------
                                     V286 Is Amended To Add Changeover Point
----------------------------------------------------------------------------------------------------------------
Elkins, WV VORTAC.....................  Casanova, VA VORTAC..........              43  Elkins.
----------------------------------------------------------------------------------------------------------------
                                     V475 Is Amended To Add Changeover Point
----------------------------------------------------------------------------------------------------------------
Madison, CT VOR/DME...................  Norwich, CT VOR/DME..........              16  Madison.
----------------------------------------------------------------------------------------------------------------

                                   Sec.   95.8005 Jet Routes Changeover Points
                                    J80 Is Amended To Delete Changeover Point
----------------------------------------------------------------------------------------------------------------
Bellaire, OH VOR/DME..................  East Texas, PA VOR/DME.......             132  Bellaire.
----------------------------------------------------------------------------------------------------------------

[FR Doc. 2014-20707 Filed 8-28-14; 8:45 am]
BILLING CODE 4910-13-P