[Federal Register: September 8, 2008 (Volume 73, Number 174)]
[Rules and Regulations]
[Page 51903-51906]
[DOCID:fr08se08-2]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0356; Directorate Identifier 2008-NM-042-AD;
Amendment 39-15661; AD 2008-18-04]
RIN 2120-AA64

Airworthiness Directives; Bombardier Model DHC-8-400 Series
Airplanes

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

ACTION: Final rule.

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SUMMARY: The FAA is superseding an existing airworthiness directive
(AD), which applies to certain Bombardier Model DHC-8-400 series
airplanes. That AD currently requires inspecting all barrel nuts to
determine if the barrel nuts have a certain marking, inspecting
affected bolts to determine if the bolts are pre-loaded correctly, and
replacing all hardware if the pre-load is incorrect. For airplanes on
which the pre-load is correct, the existing AD requires doing
repetitive visual inspections for cracking of the barrel nuts and
cradles and replacing all hardware for all cracked barrel nuts. The
existing AD also requires replacing all hardware for certain affected
barrel nuts that do not have cracking, which would end the repetitive
inspections for those airplanes. The existing AD also provides an
optional replacement for all affected barrel nuts. This new AD requires
replacing all affected barrel nuts and applying a certain compound to
the affected barrel nuts and bolts. This AD results from reports of
cracking in the barrel nuts at the four primary front spar wing-to-
fuselage attachment joints. We are issuing this AD to detect and
correct cracking of the barrel nuts at the wing front spar wing-to-
fuselage joints, which could result in reduced structural integrity of
the wing-to-fuselage attachments and consequent detachment of the wing.

DATES: This AD becomes effective October 14, 2008.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of October 14,
2008.
    On February 13, 2008 (73 FR 8187, February 13, 2008), the Director
of the Federal Register approved the incorporation by reference of
Bombardier Alert Service Bulletin A84-57-19, Revision A, dated February
6, 2008.

ADDRESSES: For service information identified in this AD, contact
Bombardier, Inc., Bombardier Regional Aircraft Division, 123 Garratt
Boulevard, Downsview, Ontario M3K 1Y5, Canada.

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 AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (telephone<PHONE_NUMBER>) is the Document Management
Facility, U.S. Department of Transportation, Docket Operations, M-30,
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.

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

SUPPLEMENTARY INFORMATION:

Discussion

    The FAA issued a supplemental notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an AD that supersedes AD 2008-04-02,
amendment 39-15374 (73 FR 8187, February 13, 2008). The existing AD
applies to certain Bombardier Model DHC-8-400 series airplanes. That
supplemental NPRM was published in the Federal Register on June 26,
2008 (73 FR 36285). That supplemental NPRM proposed to continue to
require inspecting all barrel nuts to determine if the barrel nuts have
a certain marking, inspecting affected bolts to determine if the bolts
are pre-loaded correctly, and replacing all hardware if the pre-load is
incorrect. For airplanes on which the pre-load is correct, that
supplemental NPRM also proposed to continue to require doing repetitive
visual inspections for cracking of the barrel nuts and cradles and
replacing all hardware for all cracked barrel nuts. That supplemental
NPRM also proposed to continue to require replacing all hardware for
certain affected barrel nuts that do not have cracking, which would end
the repetitive inspections for those airplanes. In addition, that
supplemental NPRM also proposed to continue to provide an optional
replacement for all affected barrel nuts. Finally, that supplemental
NPRM also proposed to require replacing all affected barrel nuts and
applying a certain compound to the affected barrel nuts and bolts.

Comments

    We provided the public the opportunity to participate in the
development of this AD. No comments have been received on the NPRM or
on the determination of the cost to the public.

Conclusion

    We have carefully reviewed the available data and determined that
air

safety and the public interest require adopting the AD as proposed.

Costs of Compliance

    This AD affects about 48 airplanes of U.S. registry.
    The actions that are required by AD 2008-04-02 and retained in this
AD take about 3 work hours per airplane, at an average labor rate of
$80 per work hour. Based on these figures, the estimated cost of the
currently required actions is $11,520, or $240 per airplane, per
inspection cycle.
    Replacement of the hardware of a barrel nut, if required, takes
about 12 work hours per airplane, at an average labor rate of $80 per
work hour. Required parts cost about $800 per barrel nut. Based on
these figures, we estimate the cost of a replacement to be $1,760 per
barrel nut.
    Application of the compound, if required, takes about 4 work hours
per airplane, at an average labor rate of $80 per work hour. Based on
these figures, we estimate the cost of a replacement to be $320 per
application.

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 have 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 DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
    (3) 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. See the ADDRESSES
section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

0
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 Federal Aviation Administration (FAA) amends Sec.  39.13 by
removing amendment 39-15374 (73 FR 8187, February 13, 2008) and by
adding the following new airworthiness directive (AD):

2008-18-04 Bombardier, Inc. (Formerly de Havilland, Inc.): Amendment
39-15661. Docket No. FAA-2008-0356; Directorate Identifier 2008-NM-
042-AD.

Effective Date

    (a) This AD becomes effective October 14, 2008.

Affected ADs

    (b) This AD supersedes AD 2008-04-02.

Applicability

    (c) This AD applies to Bombardier Model DHC-8-400, DHC-8-401,
and DHC-8-402 airplanes, certificated in any category; serial
numbers 4001 and 4003 through 4176 inclusive.

Unsafe Condition

    (d) This AD results from reports of cracking in the barrel nuts
at the four primary front spar wing-to-fuselage attachment joints.
We are issuing this AD to detect and correct cracking of the barrel
nuts at the wing front spar wing-to-fuselage joints, which could
result in reduced structural integrity of the wing-to-fuselage
attachments and consequent detachment of the wing.

Compliance

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

Restatement of Requirements of AD 2008-04-02 With New Service
Information

Inspections and Corrective Actions

    (f) Within 50 flight hours after February 13, 2008 (the
effective date of AD 2008-04-02), inspect all barrel nuts, part
number DSC228-16, to determine if the barrel nuts are identified
with a marking of LH7940T SPS 01. Inspect in accordance with the
Accomplishment Instructions of Bombardier Alert Service Bulletin
A84-57-19, Revision A, dated February 6, 2008; or Revision B, dated
March 6, 2008. As of the effective date of this AD, Bombardier Alert
Service Bulletin A84-57-19, Revision B, dated March 6, 2008, must be
used.
    (1) If no barrel nuts are identified with a marking of LH7940T
SPS 01, no further actions are required by this paragraph.
    (2) If any barrel nut is found that is identified with a marking
of LH7940T SPS 01, before further flight, inspect the inboard and
outboard bolts to determine if the bolts are pre-loaded correctly.
Inspect in accordance with the Accomplishment Instructions of
Bombardier Alert Service Bulletin A84-57-19, Revision A, dated
February 6, 2008; or Revision B, dated March 6, 2008. As of the
effective date of this AD, Bombardier Alert Service Bulletin A84-57-
19, Revision B, dated March 6, 2008, must be used.
    (i) If the pre-load is incorrect (i.e., the ring can be
rotated), before further flight, replace all hardware at that
location in accordance with the Accomplishment Instructions of the
alert service bulletin.
    (ii) If the pre-load is correct, before further flight, do a
visual inspection for cracking of the barrel nuts and cradles in
accordance with the Accomplishment Instructions of the alert service
bulletin.
    (A) If no cracking of the barrel nut and cradle is found, do the
applicable action required by paragraph (g) of this AD.
    (B) If no cracking of the barrel nut is found and only cracking
of the cradle is found, no action is required by this paragraph
provided that the applicable corrective action specified in
paragraph (g) of this AD is done.
    (C) If any cracking of the barrel nut is found, before next
flight, replace all hardware only at that location in accordance
with the Accomplishment Instructions of the alert service bulletin.
    (g) For any barrel nuts on which no cracking of the barrel nut
was found during the inspection required by paragraph (f)(2)(ii) of
this AD, do the applicable corrective action specified in paragraph
(g)(1), (g)(2), (g)(3), (g)(4), or (g)(5) of this AD at the
compliance time specified in the applicable paragraph.
    (1) If four barrel nuts having no cracking are found, do the
actions specified in paragraphs (g)(1)(i), (g)(1)(ii), and
(g)(1)(iii) of this AD.
    (i) Within 50 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, repeat the inspection specified
in paragraph (f)(2) of this AD. Thereafter, repeat the inspection at
intervals not to exceed 50

flight hours until the replacement specified in paragraph (g)(1)(ii)
of this AD is done.
    (ii) Within 100 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, replace all hardware at the
left-hand outboard location and the right-hand outboard location in
accordance with the Accomplishment Instructions of Bombardier Alert
Service Bulletin A84-57-19, Revision A, dated February 6, 2008; or
Revision B, dated March 6, 2008. As of the effective date of this
AD, Bombardier Alert Service Bulletin A84-57-19, Revision B, dated
March 6, 2008, must be used. Replacing the barrel nuts on the
outboard locations terminates the requirement to do the repetitive
inspections specified in paragraph (g)(1)(i) of this AD.
    (iii) Within 100 flight hours after doing the replacement
required by paragraph (g)(1)(ii) of this AD, repeat the inspection
specified in paragraph (f)(2) of this AD for the remaining barrel
nuts identified with a marking of LH7940T SPS 01. Thereafter, repeat
the inspection at intervals not to exceed 100 flight hours until the
replacement of all hardware at those locations is done. Do the
inspection and replacement in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Revision B, dated March 6,
2008. As of the effective date of this AD, Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008, must be used.
    (2) If three barrel nuts having no cracking are found, do the
actions specified in paragraphs (g)(2)(i), (g)(2)(ii), and
(g)(2)(iii) of this AD.
    (i) Within 50 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, repeat the inspection specified
in paragraph (f)(2) of this AD. Thereafter, repeat the inspection at
intervals not to exceed 50 flight hours until the replacement
specified in paragraph (g)(2)(ii) of this AD is done.
    (ii) Within 100 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, replace all hardware for one
affected barrel nut at the outboard location, on the side with two
affected barrel nuts, in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Revision B, dated March 6,
2008. As of the effective date of this AD, Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008, must be used.
Replacing the barrel nut on the outboard location terminates the
requirement to do the repetitive inspections specified in paragraph
(g)(2)(i) of this AD.
    (iii) Within 100 flight hours after doing the replacement
required by paragraph (g)(2)(ii) of this AD, repeat the inspection
specified in paragraph (f)(2) of this AD for the remaining barrel
nuts identified with a marking of LH7940T SPS 01. Thereafter, repeat
the inspection at intervals not to exceed 100 flight hours until the
replacement of all hardware at those locations is done. Do the
inspection and replacement in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Revision B, dated March 6,
2008. As of the effective date of this AD, Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008, must be used.
    (3) If two barrel nuts having no cracking are found and both
nuts are on the same side, do the actions specified in paragraphs
(g)(3)(i), (g)(3)(ii), and (g)(3)(iii) of this AD.
    (i) Within 100 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, repeat the inspection specified
in paragraph (f)(2) of this AD. Thereafter, repeat the inspection at
intervals not to exceed 100 flight hours until the replacement
specified in paragraph (g)(3)(ii) of this AD is done.
    (ii) Within 500 flight hours after doing the inspection required
by paragraph (f)(2)(ii) of this AD, replace all hardware for one
affected barrel nut at the outboard location that has two affected
barrel nuts in accordance with the Accomplishment Instructions of
Bombardier Alert Service Bulletin A84-57-19, Revision A, dated
February 6, 2008; or Revision B, dated March 6, 2008. As of the
effective date of this AD, Bombardier Alert Service Bulletin A84-57-
19, Revision B, dated March 6, 2008, must be used. Replacing the
barrel nut on the outboard location terminates the requirement to do
the repetitive inspections specified in paragraph (g)(3)(i) of this
AD.
    (iii) Within 100 flight hours after doing the replacement
required by paragraph (g)(3)(ii) of this AD, repeat the inspection
specified in paragraph (f)(2) of this AD for the remaining barrel
nut identified with a marking of LH7940T SPS 01. Thereafter, repeat
the inspection at intervals not to exceed 100 flight hours until the
replacement of all hardware at that location is done. Do the
inspection and replacement in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Revision B, dated March 6,
2008. As of the effective date of this AD, Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008, must be used.
    (4) If two barrel nuts having no cracking are found and are on
opposite sides, within 100 flight hours after doing the inspection
required by paragraph (f)(2)(ii) of this AD, repeat the inspection
specified in paragraph (f)(2) of this AD. Thereafter, repeat the
inspection at intervals not to exceed 100 flight hours until the
replacement of all hardware at those locations is done. Do the
inspection and replacement in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Revision B, dated March 6,
2008. As of the effective date of this AD, Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008, must be used.
    (5) If one barrel nut having no cracking is found, within 100
flight hours after doing the inspection required by paragraph
(f)(2)(ii) of this AD, repeat the inspection specified in paragraph
(f)(2) of this AD. Thereafter, repeat the inspection at intervals
not to exceed 100 flight hours until the replacement of all hardware
at that location is done. Do the inspection and replacement in
accordance with the Accomplishment Instructions of Bombardier Alert
Service Bulletin A84-57-19, Revision A, dated February 6, 2008; or
Revision B, dated March 6, 2008. As of the effective date of this
AD, Bombardier Alert Service Bulletin A84-57-19, Revision B, dated
March 6, 2008, must be used.

Actions Accomplished According to Previous Issue of Alert Service
Bulletin

    (h) Actions accomplished before February 13, 2008, in accordance
with Bombardier Alert Service Bulletin A84-57-19, dated February 1,
2008, are acceptable for compliance with the corresponding actions
specified in this AD.

Actions Accomplished According to Bombardier Alert Service Bulletin
A84-57-18

    (i) For airplanes on which the actions specified in Bombardier
Alert Service Bulletin A84-57-18, dated January 16, 2008, were
accomplished before February 13, 2008, and on which no barrel nuts
were found that were identified with a marking of LH7940T SPS 01: No
further action is required by this AD.

Parts Installation

    (j) As of February 13, 2008, no person may install a barrel nut,
part number DSC228-16, identified with a marking of LH7940T SPS 01,
on any airplane.

New Requirement of This AD

Replacement of All Affected Barrel Nuts

    (k) For airplanes on which barrel nuts are inspected in
accordance with paragraph (g)(1)(iii), (g)(2)(iii), (g)(3)(iii),
(g)(4), or (g)(5) of this AD: Within 3,000 flight hours after the
effective date of this AD, replace all hardware for all remaining
barrel nuts, part number DSC228-16, identified with a marking of
LH7940T SPS 01. Do the replacement in accordance with the
Accomplishment Instructions of Bombardier Alert Service Bulletin
A84-57-19, Revision B, dated March 6, 2008. Replacement of all
hardware for all affected barrel nuts constitutes terminating action
for the repetitive inspections of this AD.
    (l) For airplanes on which hardware for the barrel nut was
replaced in accordance with Bombardier Alert Service Bulletin A84-
57-19, dated February 1, 2008; or Revision A, dated February 6,
2008: Within 3,000 flight hours after the effective date of this AD,
apply F13, Type 2 corrosion inhibiting compound to the affected
bolts and barrel nuts in accordance with the Accomplishment
Instructions of Bombardier Alert Service Bulletin A84-57-19,
Revision B, dated March 6, 2008; except if it can be conclusively
determined from a review of airplane maintenance records that F13,
Type 2 corrosion inhibiting compound was applied to the affected
bolts and barrel nuts, then no further action is required by this
paragraph.

Special Flight Permit

    (m) Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), may be issued to operate the airplane to a location
where the requirements of this AD can be accomplished, but
concurrence by the Manager, New York Aircraft Certification Office
(ACO), FAA, is

required prior to issuance of the special flight permit. Before
using any approved special flight permits, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO. Special flight permits may
be permitted provided that the conditions specified in paragraphs
(m)(1), (m)(2), (m)(3), (m)(4), and (m)(5) of this AD are met.
    (1) Both the right-hand side and left-hand side of the airplane
must have at least one barrel nut that is not within the suspect
batch (i.e., barrel nut is not identified with a marking of LH7940T
SPS 01). The barrel nuts that are not within the suspect batch must
be in good working condition (i.e., no cracking of the barrel nut).
    (2) No passengers and no cargo are onboard.
    (3) Airplane must operate in fair weather conditions with a low
risk of turbulence.
    (4) Airplane must operate with reduced airspeed. For further
information, contact Bombardier, Q Series 24 Hour Service Customer
Response Center, at: Telephone 1-416-375-4000; fax 1-416-375-4539;
E-mail<EMAIL_ADDRESS>    (5) All of the conditions specified in paragraphs (m)(1),
(m)(2), (m)(3), and (m)(4) of this AD are on a case-by-case basis.
Contact your appropriate principal inspector (PI) in the FAA Flight
Standards District Office (FSDO), or lacking a PI, your local FSDO,
for assistance.

Alternative Methods of Compliance (AMOCs)

    (n)(1) The Manager, New York ACO, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. Send information to ATTN: Pong Lee, Aerospace
Engineer, Airframe and Propulsion Branch, ANE-171, FAA, New York
ACO, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590;
telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>. Before using any
approved AMOC on any airplane to which the AMOC applies, notify your
appropriate principal inspector (PI) in the FAA Flight Standards
District Office (FSDO), or lacking a PI, your local FSDO.

Related Information

    (o) Canadian airworthiness directive CF-2008-11R1, dated May 9,
2008, also addresses the subject of the AD.

Material Incorporated by Reference

    (p) You must use Bombardier Alert Service Bulletin A84-57-19,
Revision A, dated February 6, 2008; or Bombardier Alert Service
Bulletin A84-57-19, Revision B, dated March 6, 2008; as applicable;
to perform the actions that are required by this AD, unless the AD
specifies otherwise.
    (1) The Director of the Federal Register approved the
incorporation by reference of Bombardier Alert Service Bulletin A84-
57-19, Revision B, dated March 6, 2008, in accordance with 5 U.S.C.
552(a) and 1 CFR part 51.
    (2) On February 13, 2008 (73 FR 8187, February 13, 2008), the
Director of the Federal Register approved the incorporation by
reference of Bombardier Alert Service Bulletin A84-57-19, Revision
A, dated February 6, 2008.
    (3) Contact Bombardier, Inc., Bombardier Regional Aircraft
Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada,
for a copy of this service information. You may review copies at the
FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-
register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on August 18, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
 [FR Doc. E8-19718 Filed 9-5-08; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register: October 9, 2007 (Volume 72, Number 194)]
[Notices]
[Page 57326-57327]
[DOCID:fr09oc07-73]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 12841-000]

Ute Water Conservancy District; Notice of Application Accepted
for Filing and Soliciting Motions To Intervene, Protests, and Comments

September 26, 2007.
    Take notice that the following hydroelectric application has been
filed with the Commission and is available for public inspection:
    a. Type of Application: Preliminary Permit.
    b. Project No.: 12841-000.
    c. Date filed: July 20, 2007.
    d. Applicant: Ute Water Conservancy District.
    e. Name of Project: Plateau Creek Project.
    f. Location: The project would be located on Plateau Creek, Jerry
Creek Reservoir 1, and Jerry Creek Reservoir 2, near
the town of Palisade, in Mesa County, Colorado.
    g. Filed Pursuant to: Federal Power Act, 16 U.S.C. 791(a)-825(r).
    h. Applicant Contact: Mr. Larry Clever, Ute Water Conservancy
District, P.O. Box 460, 25Rd, Grand Junction, CO 81502, phone (970)
242-7491.
    i. FERC Contact: Sonali Dohale,<PHONE_NUMBER>.
    j. Deadline for filing comments, protests, and motions to
intervene: 60 days from the issuance date of this notice.
    The Commission's Rules of Practice and Procedure require all
intervenors filing documents with the Commission to serve a copy of
that document on each person in the official service list for the
project. Further, if an intervenor files comments or documents with the
Commission relating to the merits of an issue that may affect the
responsibilities of a particular resource agency, they must also serve
a copy of the document on that resource agency.
    k. Description of Project: The project would consist of the
following. The Jerry Creek Dams and Reservoirs are owned by the Ute
Water Conservancy District. Jerry Creek Reservoir 1 is located
in Sections 9 and 16, Township T10S, Range 96W, Sixth Principal
Meridian. Jerry Creek Reservoir 2 is located in Sections 9, 10
and 16, Township T10S, Range 96W, Sixth Principal Meridian. From the
valve vault at Jerry Creek Reservoirs, water is transmitted through the
Plateau Creek Pipeline by gravity to the Rapid Creek Water Treatment
Plant (both facilities owned by the District) for a distance of about
15 miles in an alignment generally following Plateau Creek and
Interstate Highway 70. The pipeline, completed in 2001, consists of 48-
inch and 54-inch welded steel pipe. The total difference in elevation
between the inlet at Jerry Creek Reservoirs and the terminus of the
pipeline in a flow control vault at the water treatment plant (WTP) is
about 290 feet.
    The proposed generating unit would be located at the terminus of
the Plateau Creek Pipeline in the existing flow control vault at the
Rapid Creek WTP site with certain modifications to the vault and to
existing equipment, piping and fittings in the vault. The total power
production would be about 2.7 million kilowatt hours (kWh) in 2009.
    l. Locations of Applications: A copy of the application is
available for inspection and reproduction at the Commission in the
Public Reference Room, located at 888 First Street, NE., Room 2A,
Washington, DC 20426, or by calling<PHONE_NUMBER>. This filing may
also be viewed on the Commission's Web site at http://www.ferc.gov

using the ``eLibrary'' link. Enter the docket number excluding the last
three digits in the docket number field to access the document. For
assistance, call toll-free 1-866-208-3676 or e-mail
<EMAIL_ADDRESS>For TTY, call<PHONE_NUMBER>. A copy is

also available for inspection and reproduction at the address in item h
above.
    m. Individuals desiring to be included on the Commission's mailing
list should so indicate by writing to the Secretary of the Commission.
    n. Competing Preliminary Permit: Anyone desiring to file a
competing application for preliminary permit for a proposed project
must submit the competing application itself, or a notice of intent to
file such an application, to the Commission on or before the specified
comment date for the particular application (see 18 CFR 4.36).
Submission of a timely notice of intent allows an interested person to
file the competing preliminary permit application no later than 30 days
after the specified comment date for the particular application. A
competing preliminary permit application must conform with 18 CFR 4.30
and 4.36.
    o. Competing Development Application: Any qualified development
applicant desiring to file a competing development application must
submit to the Commission, on or before a specified comment date for the
particular application, either a competing development application or a
notice of intent to file such an application. Submission of a timely

notice of intent to file a development application allows an interested
person to file the competing application no later than 120 days after
the specified comment date for the particular application. A competing
license application must conform with 18 CFR 4.30 and 4.36.
    p. Notice of Intent: A notice of intent must specify the exact
name, business address, and telephone number of the prospective
applicant, and must include an unequivocal statement of intent to
submit, if such an application may be filed, either a preliminary
permit application or a development application (specify which type of
application). A notice of intent must be served on the applicant(s)
named in this public notice.
    q. Proposed Scope of Studies under Permit: A preliminary permit, if
issued, does not authorize construction. The term of the proposed
preliminary permit would be 36 months. The work proposed under the
preliminary permit would include economic analysis, preparation of
preliminary engineering plans, and a study of environmental impacts.
Based on the results of these studies, the Applicant would decide
whether to proceed with the preparation of a development application to
construct and operate the project.
    r. Comments, Protests, or Motions to Intervene: Anyone may submit
comments, a protest, or a motion to intervene in accordance with the
requirements of Rules of Practice and Procedure, 18 CFR 385.210, .211,
.214. In determining the appropriate action to take, the Commission
will consider all protests or other comments filed, but only those who
file a motion to intervene in accordance with the Commission's Rules
may become a party to the proceeding. Any comments, protests, or
motions to intervene must be received on or before the specified
comment date for the particular application.
    Comments, protests and interventions may be filed electronically
via the Internet in lieu of paper; See 18 CFR 385.2001(a)(1)(iii) and
the instructions on the Commission's Web site under ``e-filing'' link.
The Commission strongly encourages electronic filing.
    s. Filing and Service of Responsive Documents: Any filings must
bear in all capital letters the title ``COMMENTS'', ``RECOMMENDATIONS
FOR TERMS AND CONDITIONS'', ``PROTEST'', ``COMPETING APPLICATION'' or
``MOTION TO INTERVENE'', as applicable, and the Project Number of the
particular application to which the filing refers. Any of the above-
named documents must be filed by providing the original and the number
of copies provided by the Commission's regulations to: The Secretary,
Federal Energy Regulatory Commission, 888 First Street, NE.,
Washington, DC 20426. A copy of any motion to intervene must also be
served upon each representative of the Applicant specified in the
particular application.
    t. Agency Comments: Federal, State, and local agencies are invited
to file comments on the described application. A copy of the
application may be obtained by agencies directly from the Applicant. If
an agency does not file comments within the time specified for filing
comments, it will be presumed to have no comments. One copy of an
agency's comments must also be sent to the Applicant's representatives.

Kimberly D. Bose,
Secretary.
[FR Doc. E7-19777 Filed 10-5-07; 8:45 am]

BILLING CODE 6717-01-P


PAPERWORK REDUCTION ACT SUBMISSION Please read the instructions before completing this form. For additional forms or assistance in completing this form, contact your agency's Paperwork Clearance Officer. Send two copies of this form, the collection instrument to be reviewed, the Supporting Statement and any additional documentation to: Office of Information and Regulatory Affairs, Office of Management and Budget, Docket Library, Room 10102, 725 17th Street NW Washington, DC 20503.

1. Agency/ Subagency originating request EPA, Office of Transportation and Air Quality, OAR 2. OMB control number b. None a 2060 0275 3. Type of information collection ( check one) a. Q New collection b. Revision of a currently approved collection c. X Extension of a currently approved collection d. Q Reinstatement, without change, of a previously approved collection for which approval has expired e. Q Reinstatement, with change, of a previously approved collection for which approval has expired f. Q Existing collection in use without an OMB control number 4. Type of review requested ( check one) a. X Regular b. Q Emergency  Approval requested by: / / c. Q Delegated 5. Small entities Will this information collection have a significant economic impact on a substantial number of small entities? Q Yes X No For b f, note item A2 of Supporting Statement Instructions 6. Requested expiration date a. Three years from approval date b. Other Specify: / /___

7. Title Detergent Gasoline: Certification Requirements for Manufacturers of Detergent Additives; Requirements for Transferors and Transferees of Detergent Additives; Requirements for Blenders of Detergents Into Gasoline or Post refinery Component; Requirements for Manufacturers, Transferors, and Transferees of Gasoline or Post refinery Component ( 40 CFR 80  Subpart G)

8. Agency form number( s) ( If applicable) 1655.04 9. Keywords Gasoline, detergent additives, blenders 10. Abstract The Clean Air Act requires gasoline to contain detergent additives. Certification requirements for detergent manufacturers are at 40 CFR 80  Subpart There G, and require reporting certain information the Agency. There are recordkeeping requirements for blenders of detergents into gasoline to ensure that effective concentrations are used.

11. Affected public ( Mark primary with " P" and all others that apply with " X") a. Individuals or households d. Farms b. P Business or other for profit e. Federal Government c. Not for profit institutions f. State, Local or Tribal Government 12. Obligation to respond ( Mark primary with " P" and all others that apply with " X") a. Q Voluntary b. Q Required to obtain or retain benefits c. P Mandatory 13. Annual reporting and recordkeeping hour burden a. Number of respondents 1374 b. Total annual responses 69,558 1. Percentage of these responses collected electronically 0 % c. Total hours requested 223,008 d. Current OMB inventory 17,992 e. Difference 205,016 f. Explanation of difference 1. Program Change 2. Adjustment 205,016 14. Annual reporting and recordkeeping cost burden ( in thousands of dollars) a. Total annualized capital/ startup costs 0 b. Total annual costs ( O& M) 1 c. Total annualized cost requested 1 d. Current OMB inventory 3,742 e. Difference ( 3,741)

f. Explanation of difference 1. Program change 2. Adjustment ( 3,741)

15. Purpose of information collection ( Mark Primary With " P" and all others that apply with " X") a. __ Application for benefits e. __ Program planning or management b. __ Program evaluation f. __ Research c. __ General purpose statistics g. P Regulatory or compliance d. __ Audit 16. Frequency of recordkeeping or reporting ( check all that apply) a. X Recordkeeping b. Q Third party disclosure c. X Reporting 1. X On occasion 2. Q Weekly 3. X Monthly 4. Q Quarterly 5. Q Semi annually 6. Q Annually 7. Q Biennially 8. Q Other ( describe)

17. Statistical methods Does this information collection employ statistical methods?

Q Yes X No 18. Agency contact ( person who can best answer questions regarding the content of this submission) Name: James W. Caldwell Phone: 202 564 9303 OMB 83 I 10/ 95


[Federal Register Volume 88, Number 18 (Friday, January 27, 2023)]
[Notices]
[Page 5327]
[FR Doc No: 2023-01659]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. ID-4068-003]

Walker, Kevin E.; Notice of Filing

    Take notice that on January 20, 2023, Kevin E. Walker submitted for
filing, application for authority to hold interlocking positions,
pursuant to section 305(b) of the Federal Power Act, 16 U.S.C. 825d(b)
and part 45.8 of the Federal Energy Regulatory Commission's
(Commission) Rules of Practice and Procedure, 18 CFR part 45.8.
    Any person desiring to intervene or to protest this filing must
file in accordance with Rules 211 and 214 of the Commission's Rules of
Practice and Procedure (18 CFR 385.211, 385.214). Protests will be
considered by the Commission in determining the appropriate action to
be taken but will not serve to make protestants parties to the
proceeding. Any person wishing to become a party must file a notice of
intervention or motion to intervene, as appropriate. Such notices,
motions, or protests must be filed on or before the comment date. On or
before the comment date, it is not necessary to serve motions to
intervene or protests on persons other than the Applicant.
    In addition to publishing the full text of this document in the
Federal Register, the Commission provides all interested persons an
opportunity to view and/or print the contents of this document via the
internet through the Commission's Home Page (http://www.ferc.gov) using
the ``eLibrary'' link. Enter the docket number excluding the last three
digits in the docket number field to access the document. At this time,
the Commission has suspended access to the Commission's Public
Reference Room, due to the proclamation declaring a National Emergency
concerning the Novel Coronavirus Disease (COVID-19), issued by the
President on March 13, 2020. For assistance, contact the Federal Energy
Regulatory Commission at [email protected] or call toll-free,
(886) 208-3676 or TYY,<PHONE_NUMBER>.
    The Commission strongly encourages electronic filings of comments,
protests and interventions in lieu of paper using the ``eFiling'' link
at http://www.ferc.gov. Persons unable to file electronically may mail
similar pleadings to the Federal Energy Regulatory Commission, 888
First Street NE, Washington, DC 20426. Hand delivered submissions in
docketed proceedings should be delivered to Health and Human Services,
12225 Wilkins Avenue, Rockville, Maryland 20852.
    Comment Date: 5:00 p.m. Eastern Time on February 10, 2023.

    Dated: January 23, 2023.
Kimberly D. Bose,
Secretary.
[FR Doc. 2023-01659 Filed 1-26-23; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 76, Number 78 (Friday, April 22, 2011)]
[Rules and Regulations]
[Pages 22610-22611]
[FR Doc No: 2011-9765]

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

DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

21 CFR Part 522

[Docket No. FDA-2011-N-0003]

Implantation or Injectable Dosage Form New Animal Drugs;
Enrofloxacin

AGENCY: Food and Drug Administration, HHS.

ACTION: Final rule.

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SUMMARY: The Food and Drug Administration (FDA) is amending the animal
drug regulations to reflect approval of a supplemental new animal drug
application (NADA) filed by Bayer HealthCare LLC. The supplemental NADA
provides for the addition of a pathogen to the indications for use of
enrofloxacin solution in cattle, as a single injection, for the
treatment of respiratory disease.

DATES: This rule is effective April 22, 2011.

FOR FURTHER INFORMATION CONTACT: Cindy L. Burnsteel, Center for
Veterinary Medicine (HFV-130), Food and Drug Administration, 7500
Standish Pl., Rockville, MD 20855,<PHONE_NUMBER>, e-mail:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION: Bayer HealthCare LLC, Animal Health
Division, P.O. Box 390, Shawnee Mission, KS 66201, filed a supplement
to NADA 141-068 for BAYTRIL 100 (enrofloxacin), an injectable solution.
The supplemental NADA provides for the addition of Mycoplasma bovis to
the pathogens in the indication for use of enrofloxacin solution in
cattle, as a single injection, for the treatment of bovine respiratory
disease (BRD). The supplemental NADA is approved as of March 10, 2011,
and the regulation in 21 CFR 522.812 is amended to reflect the
approval.
    In accordance with the freedom of information provisions of 21 CFR
part 20 and Sec.  514.11(e)(2)(ii), a summary of safety and
effectiveness data and information submitted to support approval of
this application may be seen in the Division of Dockets Management
(HFA-305), Food and Drug Administration, 5630 Fishers Lane, rm. 1061,
Rockville, MD 20852, between 9 a.m. and 4 p.m., Monday through Friday.
    Under section 512(c)(2)(F)(iii) of the Federal Food, Drug, and
Cosmetic Act (21 U.S.C. 360b(c)(2)(F)(iii)), this supplemental approval
qualifies for 3

years of marketing exclusivity beginning on the date of approval.
    The Agency has determined under 21 CFR 25.33 that this action is of
a type that does not individually or cumulatively have a significant
effect on the human environment. Therefore, neither an environmental
assessment nor an environmental impact statement is required.
    This rule does not meet the definition of ``rule'' in 5 U.S.C.
804(3)(A) because it is a rule of ``particular applicability.''
Therefore, it is not subject to the congressional review requirements
in 5 U.S.C. 801-808.

List of Subjects in 21 CFR Part 522

    Animal drugs.

    Therefore, under the Federal Food, Drug, and Cosmetic Act and under
authority delegated to the Commissioner of Food and Drugs and
redelegated to the Center for Veterinary Medicine, 21 CFR part 522 is
amended as follows:

PART 522--IMPLANTATION OR INJECTABLE DOSAGE FORM NEW ANIMAL DRUGS

0
1. The authority citation for 21 CFR part 522 continues to read as
follows:

    Authority:  21 U.S.C. 360b.

0
2. In Sec.  522.812, revise paragraph (e)(2)(ii) to read as follows:

Sec.  522.812  Enrofloxacin.

* * * * *
    (e) * * *
    (2) * * *
    (ii) Indications for use--(A) Single-dose therapy: For the
treatment of bovine respiratory disease (BRD) associated with
Mannheimia haemolytica, Pasteurella multocida, Histophilus somni, and
Mycoplasma bovis in beef and non-lactating dairy cattle.
    (B) Multiple-day therapy: For the treatment of bovine respiratory
disease (BRD) associated with Mannheimia haemolytica, Pasteurella
multocida, and Histophilus somni in beef and non-lactating dairy
cattle.
* * * * *

    Dated: April 15, 2011.
Steven D. Vaughn,
Director, Office of New Animal Drug Evaluation, Center for Veterinary
Medicine.
[FR Doc. 2011-9765 Filed 4-21-11; 8:45 am]
BILLING CODE 4160-01-P