[Federal Register: May 10, 2010 (Volume 75, Number 89)]
[Rules and Regulations]
[Page 25760-25763]
[DOCID:fr10my10-2]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 97

[Docket No. 30723; Amdt. No 3372]

Standard Instrument Approach Procedures, and Takeoff Minimums and
Obstacle Departure Procedures; Miscellaneous Amendments

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: This establishes, amends, suspends, or revokes Standard
Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums
and Obstacle Departure Procedures for operations at certain airports.
These regulatory actions are needed because of the adoption of new or
revised criteria, or because of changes occurring in the National
Airspace System, such as the commissioning of new navigational
facilities, adding new obstacles, or changing air traffic requirements.
These changes are designed to provide safe and efficient use of the
navigable airspace and to promote safe flight operations under
instrument flight rules at the affected airports.

DATES: This rule is effective May 10, 2010. The compliance date for
each SIAP, associated Takeoff Minimums, and ODP is specified in the
amendatory provisions.
    The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of May 10, 2010.

ADDRESSES: Availability of matters incorporated by reference in the
amendment is as follows:
    For Examination--
    1. FAA Rules Docket, FAA Headquarters Building, 800 Independence
Avenue, SW., Washington, DC 20591;
    2. The FAA Regional Office of the region in which the affected
airport is located;
    3. The National Flight Procedures Office, 6500 South MacArthur
Blvd., Oklahoma City, OK 73169 or
    4. The National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, call 202-741-
6030, or go to: http://www.archives.gov/federal_register/code_of_
federal_regulations/ibr_locations.html.
    Availability--All SIAPs and Takeoff Minimums and ODPs are available
online free of charge. Visit http://www.nfdc.faa.gov to register.
Additionally, individual SIAP and Takeoff Minimums and ODP copies may
be obtained from:
    1. FAA Public Inquiry Center (APA-200), FAA Headquarters Building,
800 Independence Avenue, SW., Washington, DC 20591; or
    2. The FAA Regional Office of the region in which the affected
airport is located.

FOR FURTHER INFORMATION CONTACT: Harry J. Hodges, Flight Procedure
Standards Branch (AFS-420), Flight Technologies and Programs Divisions,
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 rule amends Title 14 of the Code of
Federal Regulations, part 97 (14 CFR part 97), by establishing,
amending, suspending, or revoking SIAPS, Takeoff Minimums and/or ODPS.
The complete regulators description of each SIAP and its associated
Takeoff Minimums or ODP for an identified airport is listed on FAA form
documents which are incorporated by reference in this amendment under 5
U.S.C. 552(a), 1 CFR part 51, and 14 CFR 97.20. The applicable FAA
Forms are FAA Forms 8260-3, 8260-4, 8260-5, 8260-15A, and 8260-15B when
required by an entry on 8260-15A.
    The large number of SIAPs, Takeoff Minimums and ODPs, in addition
to their complex nature and the need for a special format make
publication in the Federal Register expensive and impractical.
Furthermore, airmen do not use the regulatory text of the SIAPs,
Takeoff Minimums or ODPs, but instead refer to their depiction on
charts printed by publishers of aeronautical materials. The advantages
of incorporation by reference are realized and publication of the
complete description of each SIAP, Takeoff Minimums and ODP listed on
FAA forms is unnecessary. This amendment provides the affected CFR
sections and specifies the types of SIAPs and the effective dates of
the, associated Takeoff Minimums and ODPs. This amendment also
identifies the airport and its location, the procedure, and the
amendment number.

The Rule

    This amendment to 14 CFR part 97 is effective upon publication of
each separate SIAP, Takeoff Minimums and ODP as contained in the
transmittal. Some SIAP and Takeoff Minimums and textual ODP amendments
may have been issued previously by the FAA in a Flight Data Center
(FDC) Notice to Airmen (NOTAM) as an emergency action of immediate
flight safety relating directly to published aeronautical charts. The
circumstances which created the need for some SIAP and Takeoff Minimums
and ODP amendments may require making them effective in less than 30
days. For the remaining SIAPS and Takeoff Minimums and ODPS, an
effective date at least 30 days after publication is provided.
    Further, the SIAPs and Takeoff Minimums and ODPS contained in this
amendment are based on the criteria contained in the U.S. Standard for
Terminal Instrument Procedures (TERPS). In developing these SIAPS and
Takeoff Minimums and ODPs, the TERPS criteria were applied to the
conditions existing or anticipated at the affected airports. Because of
the close and immediate relationship between these SIAPs, Takeoff
Minimums and ODPs, and safety in air commerce, I find that notice and
public procedures before adopting these SIAPS, Takeoff Minimums and
ODPs are impracticable and contrary to the public interest and, where
applicable, that good cause exists for making some SIAPs 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 97

    Air Traffic Control, Airports, Incorporation by reference, and
Navigation (Air).

    Issued in Washington, DC, on April 30, 2010.
John M. Allen,
Director, Flight Standards Service.

Adoption of the Amendment

0
Accordingly, pursuant to the authority delegated to me, Title 14, Code
of Federal Regulations, part 97 (14 CFR part 97) is amended by
establishing, amending, suspending, or revoking Standard Instrument
Approach Procedures and/or Takeoff Minimums and/or Obstacle Departure
Procedures effective at 0902 UTC on the dates specified, as follows:

PART 97--STANDARD INSTRUMENT APPROACH PROCEDURES

0
1. The authority citation for part 97 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40103, 40106, 40113, 40114, 40120,
44502, 44514, 44701, 44719, 44721-44722.

0
2. Part 97 is amended to read as follows:

* * * Effective 3 JUN 2010

Jacksson, AL, Takeoff Minimums and Obstacle DP, Orig
Tuscaloosa, AL, Tuscaloosa Rgnl, RNAV (GPS) RWY 22, Amdt 1
Phoenix, AZ, Phoenix, Deer Valley, RNAV (GPS) RWY 7R, Amdt 1
Willcox, AZ, Cochise County, GPS RWY 21, Orig, CANCELLED
Willcox, AZ, Cochise County, GPS-A, Orig, CANCELLED
Willcox, AZ, Cochise County, RNAV (GPS) RWY 3, Orig
Willcox, AZ, Cochise County, RNAV (GPS) RWY 21, Orig
Little River, CA, Little River, LITTLE RIVER ONE Graphic Obstacle DP
Little River, CA, Little River, Takeoff Minimums and Obstacle DP,
Orig
Windsor Locks, CT, Bradley, RNAV (RNP) Z RWY 15, Orig
Fort Lauderdale, FL, Fort Lauderdale/Hollywood Intl, RNAV (GPS) RWY
27L, Orig-A
Honolulu, HI, Honolulu Intl, ILS RWY 8L, Amdt 22
Honolulu, HI, Honolulu Intl, LOC RWY 8L, Orig
Lanai City, HI, Lanai, ILS OR LOC/DME RWY 3, Amdt 1
Forest City, IA, Forest City Muni, VOR/DME-A, Amdt 3
Fort Dodge, IA, Fort Dodge Rgnl, ILS or LOC RWY 6, Amdt 7A
Lewiston, ID, Lewiston-Nez Perce County, RNAV (GPS) Y RWY 8, Amdt 1A
Lewiston, ID, Lewiston-Nez Perce County, RNAV (GPS) Y RWY 12, Amdt
1A
Lewiston, ID, Lewiston-Nez Perce County, RNAV (GPS) Y RWY 26, Orig-A
Lewiston, ID, Lewiston-Nez Perce County, RNAV (RNP) RWY 30, Orig
Lewiston, ID, Lewiston-Nez Perce County, RNAV (RNP) Z RWY 8, Orig
Lewiston, ID, Lewiston-Nez Perce County, RNAV (RNP) Z RWY 12, Orig
Lewiston, ID, Lewiston-Nez Perce County, RNAV (RNP) Z RWY 26, Orig
Alton/St Louis, IL, St Louis Rgnl, RNAV (GPS) RWY 11, Amdt 1
Chicago/Romeoville, IL, Lewis University, LOC RWY 2, Amdt 1
Chicago/Romeoville, IL, Lewis University, RNAV (GPS) RWY 2, Amdt 1
Chicago/Romeoville, IL, Lewis University, RNAV (GPS) RWY 20, Amdt 1
Effingham, IL, Effingham County Memorial, RNAV (GPS) RWY 1, Orig
Effingham, IL, Effingham County Memorial, VOR RWY 1, Amdt 10
Joliet, IL, Joliet Rgnl, RNAV (GPS) RWY 13, Orig
Joliet, IL, Joliet Rgnl, VOR RWY 13, Amdt 12
Shelbyville, IL, Shelby County, NDB-A, Amdt 2

Shelbyville, IL, Shelby County, RNAV (GPS) RWY 36, Orig
Springfield, IL, Abraham Lincoln Capital, ILS OR LOC RWY 22, Amdt 9
Springfield, IL, Abraham Lincoln Capital, RNAV (GPS) RWY 13, Amdt 1
Springfield, IL, Abraham Lincoln Capital, VOR/DME RWY 4, Orig
Springfield, IL, Abraham Lincoln Capital, VOR/DME RWY 13, Orig
Springfield, IL, Abraham Lincoln Capital, VOR/DME RWY 31, Orig
Auburn, IN, De Kalb County, ILS OR LOC RWY 27, Amdt 1B
Crawfordsville, IN, Crawfordsville Muni, GPS RWY 4, Orig-A,
CANCELLED
Crawfordsville, IN, Crawfordsville Muni, RNAV (GPS) RWY 4, Orig
Crawfordsville, IN, Crawfordsville Muni, RNAV (GPS) RWY 22, Orig
Kendallville, IN, Kendallville Muni, GPS RWY 28, Orig-A, CANCELLED
Kendallville, IN, Kendallville Muni, RNAV (GPS) RWY 28, Orig
Augusta, KS, Augusta Muni, Takeoff Minimums and Obstacle DP, Orig
Coffeyville, KS, Coffeyville Muni, VOR/DME RNAV RWY 35, Amdt 3B,
CANCELLED
Elkhart, KS, Elkhart-Morton County, NDB RWY 35, Amdt 2
Elkhart, KS, Elkhart-Morton County, RNAV (GPS) RWY 4, Amdt 1
Elkhart, KS, Elkhart-Morton County, RNAV (GPS) RWY 17, Amdt 1
Elkhart, KS, Elkhart-Morton County, RNAV (GPS) RWY 22, Amdt 1
Elkhart, KS, Elkhart-Morton County, RNAV (GPS) RWY 35, Amdt 1
Elkhart, KS, Elkhart-Morton County, Takeoff Minimums and Obstacle
DP, Amdt 1
Great Bend, KS, Great Bend Muni, RNAV (GPS) RWY 17, Orig
Wichita, KS, Wichita Mid-Continent, RNAV (GPS) RWY 14, Amdt 1
Wichita, KS, Wichita Mid-Continent, RNAV (GPS) RWY 32, Amdt 1
Mayfield, KY, Mayfield Graves County, GPS RWY 36, Orig, CANCELLED
Mayfield, KY, Mayfield Graves County, RNAV (GPS) RWY 18, Orig
Mayfield, KY, Mayfield Graves County, RNAV (GPS) RWY 36, Orig
Mayfield, KY, Mayfield Graves County, Takeoff Minimums and Obstacle
DP, Amdt 2
Mayfield, KY, Mayfield Graves County, VOR/DME-A, Amdt 8
Mayfield, KY, Mayfield Graves County, VOR/DME RNAV OR GPS RWY 18,
Amdt 3, CANCELLED
Owensboro, KY, Owensboro-Daviess County, ILS OR LOC RWY 36, Amdt 12
Owensboro, KY, Owensboro-Daviess County, RNAV (GPS) RWY 18, Amdt 1
Owensboro, KY, Owensboro-Daviess County, RNAV (GPS) RWY 23, Amdt 1
Owensboro, KY, Owensboro-Daviess County, RNAV (GPS) RWY 36, Amdt 3
Owensboro, KY, Owensboro-Daviess County, VOR RWY 36, Amdt 18
Sturgis, KY, Sturgis Muni, NDB OR GPS RWY 36, Amdt 6, CANCELLED
Sturgis, KY, Sturgis Muni, RNAV (GPS) RWY 18, Orig
Sturgis, KY, Sturgis Muni, RNAV (GPS) RWY 36, Orig
Sturgis, KY, Sturgis Muni, Takeoff Minimums and Obstacle DP, Amdt 3
Galliano, LA, South Lafourche Leonard Miller Jr, LOC/DME RWY 36,
Orig
New Orleans, LA, Louis Armstrong New Orleans Intl, ILS OR LOC RWY
28, Amdt 7A
Worcester, MA, Worcester Rgnl, GPS RWY 33, Amdt 1B, CANCELLED
Worcester, MA, Worcester Rgnl, RNAV (GPS) RWY 33, Orig
Fort Mead (Odenton), MD, Tipton, RNAV (GPS) RWY 28, Amdt 1
Pittsfield, ME, Pittsfield Muni, GPS RWY 19, Orig, CANCELLED
Pittsfield, ME, Pittsfield Muni, NDB RWY 36, Amdt 4
Pittsfield, ME, Pittsfield Muni, RNAV (GPS) RWY 18, Orig
Pittsfield, ME, Pittsfield Muni, RNAV (GPS) RWY 36, Orig
Pittsfield, ME, Pittsfield Muni, Takeoff Minimums and Obstacle DP,
Amdt 2
Wiscasset, ME, Wiscasset, GPS RWY 7, Amdt 1A, CANCELLED
Wiscasset, ME, Wiscasset, GPS RWY 25, Amdt 1, CANCELLED
Wiscasset, ME, Wiscasset, RNAV (GPS) RWY 7, Orig
Wiscasset, ME, Wiscasset, RNAV (GPS) RWY 25, Orig
Wiscasset, ME, Wiscasset, Takeoff Minimums and Obstacle DP, Amdt 2
Alpena, MI, Alpena County Rgnl, RNAV (GPS) RWY 19, Orig
Alpena, MI, Alpena County Rgnl, VOR RWY 19, Amdt 15
Oscoda, MI, Oscoda-Wurtsmith, RNAV (GPS) RWY 6, Amdt 1
Baudette, MN, Baudette Intl, ILS OR LOC/DME RWY 30, Orig
Baudette, MN, Baudette Intl, RNAV (GPS) RWY 12, Amdt 1
Baudette, MN, Baudette Intl, RNAV (GPS) RWY 30, Amdt 2
Duluth, MN, Duluth Intl, COPTER ILS OR LOC RWY 27, Amdt 1
Duluth, MN, Duluth Intl, GPS RWY 21, Orig-A, CANCELLED
Duluth, MN, Duluth Intl, ILS OR LOC RWY 9, ILS RWY 9 (CAT II), Amdt
21
Duluth, MN, Duluth Intl, ILS OR LOC RWY 27, Amdt 9
Duluth, MN, Duluth Intl, RNAV (GPS) RWY 3, Orig
Duluth, MN, Duluth Intl, RNAV (GPS) RWY 21, Orig
Duluth, MN, Duluth Intl, VOR OR TACAN RWY 3, Amdt 20
Luverne, MN, Quentin Aanenson Field, RNAV (GPS) RWY 18, Orig
Luverne, MN, Quentin Aanenson Field, RNAV (GPS) RWY 36, Orig
Luverne, MN, Quentin Aanenson Field, Takeoff Minimums and Obstacle
DP, Orig
Minneapolis, MN, Airlake, Takeoff Minimums and Obstacle DP, Orig
Minneapolis, MN, Airlake, VOR RWY 12, Amdt 2
Red Wing, MN, Red Wing Rgnl, RNAV (GPS) RWY 27, Amdt 1
Monroe City, MO, Capt. Ben Smith Airfield-Monroe City Airport, VOR/
DME RNAV RWY 27, Amdt 1, CANCELLED
Columbus/W PT/Starkville, MS, Golden Triangle Rgnl, LOC/DME RWY 36,
Orig
Albemarle, NC, Stanly County, GPS RWY 4R, Orig-C, CANCELLED
Albemarle, NC, Stanly County, ILS OR LOC RWY 22L, Amdt 1
Albemarle, NC, Stanly County, NDB RWY 22L, Amdt 1
Albemarle, NC, Stanly County, RNAV (GPS) RWY 4R, Orig
Albemarle, NC, Stanly County, RNAV (GPS) RWY 22L, Orig
Rockingham, NC, Richmond County, GPS RWY 31, Orig-A, CANCELLED
Rockingham, NC, Richmond County, NDB RWY 32, Amdt 3B
Rockingham, NC, Richmond County, RNAV (GPS) RWY 32, Orig
Rockingham, NC, Richmond County, Takeoff Minimums and Obstacle DP,
Amdt 2
Bottineau, ND, Bottineau Muni, GPS RWY 31, Orig-A, CANCELLED
Bottineau, ND, Bottineau Muni, RNAV (GPS) RWY 31, Orig
Bottineau, ND, Bottineau Muni, Takeoff Minimums and Obstacle DP,
Amdt 1
Crosby, ND, Crosby Muni, GPS RWY 30, Orig, CANCELLED
Crosby, ND, Crosby Muni, RNAV (GPS) RWY 30, Orig
Crosby ND, Crosby Muni, Takeoff Minimums and Obstacle DP, Orig
Devils Lake, ND, Devils Lake Rgnl, RNAV (GPS) RWY 13, Orig-A
Devils Lake, ND, Devils Lake Rgnl, RNAV (GPS) RWY 21, Orig
Grand Forks, ND, Grand Forks Intl, LOC BC RWY 17R, Amdt 13
Hettinger, ND, Hettinger Muni, GPS RWY 30, Amdt 1, CANCELLED
Hettinger, ND, Hettinger Muni, RNAV (GPS) RWY 30, Orig
Kindred, ND, Hamry Field, RNAV (GPS) RWY 11, Orig
Kindred, ND, Hamry Field, RNAV (GPS) RWY 29, Orig
Langdon, ND, Robertson Field, RNAV (GPS) RWY 14, Orig
Langdon, ND, Robertson Field, RNAV (GPS) RWY 32, Orig
Langdon, ND, Robertson Field, Takeoff Minimums and Obstacle DP, Orig
Keene, NH, Dillant-Hopkins, ILS OR LOC RWY 2, Amdt 4
Keene, NH, Dillant-Hopkins, VOR RWY 2, Amdt 13
Gallup, NM, Gallup Muni, RNAV (GPS) RWY 6, Amdt 2
Fallon, NV, Fallon Muni, RNAV (GPS)-C, Orig
Fallon, NV, Fallon Muni, Takeoff Minimums and Obstacle DP, Amdt 1
Fallon, NV, Fallon Muni, VOR/DME-B, Amdt 4
Newburgh, NY, Steward Intl, ILS OR LOC RWY 27, Amdt 1
Newburgh, NY, Steward Intl, RNAV (GPS) RWY 9, Amdt 1
Newburgh, NY, Steward Intl, RNAV (GPS) RWY 27, Amdt 1
Newburgh, NY, Steward Intl, VOR RWY 27, Amdt 5
Rome, NY, Griffiss Intl, ILS RWY 15, Orig-A, CANCELLED
Rome, NY, Griffiss Intl, ILS OR LOC RWY 33, Amdt 1
Rome, NY, Griffiss Intl, RNAV (GPS) RWY 15, Amdt 1

Rome, NY, Griffiss Intl, RNAV (GPS) RWY 33, Amdt 1
Williamson/Sodus, NY, Williamson-Sodus, RNAV (GPS) RWY 28, Amdt 2
Bryan, OH, Williams County, GPS RWY 7, Orig, CANCELLED
Bryan, OH, Williams County, GPS RWY 25, Orig, CANCELLED
Bryan, OH, Williams County, NDB-A, Amdt 7
Bryan, OH, Williams County, RNAV (GPS) RWY 7, Orig
Bryan, OH, Williams County, RNAV (GPS) RWY 25, Orig
Bryan, OH, Williams County, Takeoff Minimums and Obstacle DP, Orig
East Liverpool, OH, Columbiana County, GPS RWY 25, Orig, CANCELLED
East Liverpool, OH, Columbiana County, RNAV (GPS) RWY 25, Orig
Millersburg, OH, Holmes County, Takeoff Minimums and Obstacle DP,
Amdt 1
Steubenville, OH, Jefferson County Airpark, GPS RWY 14, Orig,
CANCELLED
Steubenville, OH, Jefferson County Airpark, GPS RWY 32, Orig,
CANCELLED
Steubenville, OH, Jefferson County Airpark, RNAV (GPS) RWY 14, Orig
Steubenville, OH, Jefferson County Airpark, RNAV (GPS) RWY 32, Orig
Youngstown, OH, Youngstown Elser Metro, GPS RWY 10, Orig-B,
CANCELLED
Youngstown, OH, Youngstown Elser Metro, GPS RWY 28, Orig-B,
CANCELLED
Youngstown, OH, Youngstown Elser Metro, RNAV (GPS) RWY 10, Orig
Youngstown, OH, Youngstown Elser Metro, RNAV (GPS) RWY 28, Orig
Youngstown, OH, Youngstown Elser Metro, VOR-C, Amdt 2
Pauls Valley, OK, Pauls Valley, RNAV (GPS) RWY 35, Amdt 1
Pauls Valley, OK, Pauls Valley, Takeoff Minimums and Obstacle DP,
Orig
Woodward, OK, West Woodward, VOR/DME-A, Amdt 7
Gettysburg, PA, Gettysburg Rgnl, RNAV (GPS)-A, Orig
Gettysburg, PA, Gettysburg Rgnl, Takeoff Minimums and Obstacle DP,
Orig
Washington, PA, Washington County, VOR-B, Amdt 7, CANCELLED
Orangeburg, SC, Orangeburg Muni, NDB RWY 5, Amdt 1, CANCELLED
Orangeburg, SC, Orangeburg Muni, RNAV (GPS) RWY 5, Amdt 1
Orangeburg, SC, Orangeburg Muni, RNAV (GPS) RWY 23, Amdt 1
Orangeburg, SC, Orangeburg Muni, RNAV (GPS) RWY 35, Amdt 1
Athens, TN, McMinn County, NDB RWY 2, Amdt 6
Athens, TN, McMinn County, NDB RWY 20, Amdt 7
Athens, TN, McMinn County, RNAV (GPS) RWY 2, Orig
Athens, TN, McMinn County, RNAV (GPS) RWY 20, Amdt 1
Athens, TN, McMinn County, Takeoff Minimums and Obstacle DP, Amdt 1
Clarksville, TN, Outlaw Field, RNAV (GPS) RWY 17, Orig
Lafayette, TN, Lafayette Muni, RNAV (GPS) RWY 1, Orig
Lafayette, TN, Lafayette Muni, RNAV (GPS) RWY 19, Amdt 1
Follett, TX, Follet-Lipscomb County, RNAV (GPS) RWY 35, Orig,
Follett, TX, Follet-Lipscomb County, Takeoff Minimums and Obstacle
DP, Orig
Follett, TX, Follet-Lipscomb County, VOR/DME-A, Amdt 3
Grayford, TX, Possum Kingdom, Takeoff Minimums and Obstacle DP,
Orig-A
Lubbock, TX, Lubbock Preston Smith Inthl, RADAR-1, Amdt 7, CANCELLED
Farmville, VA, Farmville Rgnl, Takeoff Minimums and Obstacle DP,
Amdt 1
Wise, VA, Lonesome Pine, LOC/DME RWY 24, Orig-A
Barre/Montpelier, VT, Edward F. Knapp State, RNAV (GPS) RWY 17,
Orig-A
Richland, WA, Richland, Takeoff Minimums and Obstacle DP, Orig
Appleton, WI, Outagamie County Rgnl, ILS OR LOC RWY 30, Amdt 3
Appleton, WI, Outagamie County Rgnl, RNAV (GPS) RWY 12, Amdt 1
Appleton, WI, Outagamie County Rgnl, RNAV (GPS) RWY 21, Amdt 2
Appleton, WI, Outagamie County Rgnl, RNAV (GPS) RWY 30, Amdt 1
Appleton, WI, Outagamie County Rgnl, Takeoff Minimums and Obstacle
DP, Orig
Janesville, WI, Southern Wisconsin Rgnl, RNAV (GPS) RWY 4, Amdt 1
Janesville, WI, Southern Wisconsin Rgnl, RNAV (GPS) RWY 14, Amdt 1
Janesville, WI, Southern Wisconsin Rgnl, RNAV (GPS) RWY 22, Amdt 1
Manitowish Waters, WI, Manitowish Waters, GPS RWY 32, Orig-B,
CANCELLED
Manitowish Waters, WI, Manitowish Waters, NDB RWY 32, Orig-A,
CANCELLED
Manitowish Waters, WI, Manitowish Waters, RNAV (GPS) RWY 14, Orig
Manitowish Waters, WI, Manitowish Waters, RNAV (GPS) RWY 32, Orig
Superior, WI, Richard I Bong, NDB RWY 31, Amdt 4A, CANCELLED

    On April 15, 2010 (75 FR 19542) the FAA published an Amendment
in Docket No. 30716, Amdt 3366 to Part 97 of the Federal Aviation
Regulations under section 97.23 and 97.33. The following entries
effective 3 June 2010 are hereby rescinded:

Kutztown, PA, Kutztown, RNAV (GPS)-A, Orig, CANCELLED
Kutztown, PA, Kutztown, Takeoff Minimums and Obstacle DP, Orig,
CANCELLED
Kutztown, PA, Kutztown, VOR-B, Amdt 1B, CANCELLED

    On April 28, 2010 (75 FR 22217) the FAA published an Amendment
in Docket No. 30720, Amdt 3370 to Part 97 of the Federal Aviation
Regulations under section 97.23 and 97.33. The following entry
effective 3 June 2010 is hereby rescinded:

Fostoria, OH, Fostoria Metropolitan, RNAV (GPS) RWY 27, Amdt 1

[FR Doc. 2010-10708 Filed 5-7-10; 8:45 am]
BILLING CODE 4910-13-P


MEMORANDUM

DATE: 11/7/14

FROM: 		Ken Mitchell/EPA Region 4

TO:CLEAN POWER PLAN FOR EXISTING POWER PLANTS; DOCKET ID: OAR - 2013-0602

SUBJECT:DISCUSSION OF THE Southeastern Electric Exchange (SEE) Conference held on 06/26/2014

SUMMARY:

EPA Region 4 provided an overview of the Clean Power Plan to attendees at the Southeastern Electric Exchange Conference held on 06/26/2014 in Orlando, FL.  The Clean Power Plan for Existing Power Plants was proposed on June 2, 2014.

ATTENDEES:

EPA Beverly Banister/EPA R4

External Stakeholders Approximately 25.  Convened by the Southeastern Electric Exchange (S.E.E. Conference Coordinator: Amy Bekele)

ATTACHMENTS


of view and image size requirements of S5.5.1 and S5.5.2 after each
durability test specified in S14.3.1, S14.3.2, and S14.3.3.
    S6. Requirements for multipurpose passenger vehicles, low-speed
vehicles, trucks, buses, and school buses with GVWR of 4,536 kg or
less.
* * * * *
    S6.2 Rear visibility.
    (a) Phase-in period requirements. For multipurpose passenger
vehicles, low-speed vehicles, trucks, buses, and school buses with a
GVWR of 4,536 kg or less manufactured on or after May 1, 2016, but not
later than April 30, 2018, a percentage of each manufacturer's
production, as specified in S15, shall display a rearview image meeting
the requirements of S6.2.1.
    (b) Final requirements. Each multipurpose passenger vehicle, low-
speed vehicle, truck, bus, and school bus with a GVWR of 4,536 kg or
less manufactured on or after May 1, 2018, shall display a rearview
image meeting the requirements of S6.2.1 through S6.2.7.
    S6.2.1 Field of view. When tested in accordance with the procedures
in S14.1, the rearview image shall include:
    (a) A minimum of a 150-mm wide portion along the circumference of
each test object located at positions F and G specified in S14.1.4; and
    (b) The full width and height of each test object located at
positions A through E specified in S14.1.4.
    S6.2.2 Size. When the rearview image is measured in accordance with
the procedures in S14.1, the calculated visual angle subtended by the
horizontal width of
    (a) All three test objects located at positions A, B, and C
specified in S14.1.4 shall average not less than 5 minutes of arc; and
    (b) Each individual test object (A, B, and C) shall not be less
than 3 minutes of arc.
    S6.2.3 Response time. The rearview image meeting the requirements
of S6.2.1 and S6.2.2, when tested in accordance with S14.2, shall be
displayed within 2.0 seconds of the start of a backing event.
    S6.2.4 Linger time. The rearview image meeting the requirements of
S6.2.1 and S6.2.2 shall not be displayed after the backing event has
ended.
    S6.2.5 Deactivation. The rearview image meeting the requirements of
S6.2.1 and S6.2.2 shall remain visible during the backing event until
either, the driver modifies the view, or the vehicle direction selector
is removed from the reverse position.
    S6.2.6 Default view. The rear visibility system must default to the
rearview image meeting the requirements of S6.2.1 and S6.2.2 at the
beginning of each backing event regardless of any modifications to the
field of view the driver has previously selected.
    S6.2.7 Durability. The rear visibility system shall meet the field
of view and image size requirements of S6.2.1 and S6.2.2 after each
durability test specified in S14.3.1, S14.3.2, and S14.3.3.
* * * * *
    S14. Rear visibility test procedure.
    S14.1 Field of view and image size test procedure.
    S14.1.1 Lighting. The ambient illumination conditions in which
testing is conducted consists of light that is evenly distributed from
above and is at an intensity of between 7,000 lux and 10,000 lux, as
measured at the center of the exterior surface of the vehicle's roof.
    S14.1.2 Vehicle conditions.
    S<IP_ADDRESS> Tires. The vehicle's tires are set to the vehicle
manufacturer's recommended cold inflation pressure.
    S<IP_ADDRESS> Fuel tank loading. The fuel tank is full.
    S<IP_ADDRESS> Vehicle load. The vehicle is loaded to simulate the
weight of the driver and four passengers or the designated occupant
capacity, if less. The weight of each occupant is represented by 45 kg
resting on the seat pan and 23 kg resting on the vehicle floorboard
placed in the driver's designated seating position and any other
available designated seating position.
    S<IP_ADDRESS> Rear hatch and trunk lids. If the vehicle is equipped
with rear hatches or trunk lids, they are closed and latched in their
normal vehicle operating condition.
    S<IP_ADDRESS> Driver's seat positioning.
    S<IP_ADDRESS>.1 Adjust the driver's seat to the midpoint of the
longitudinal

adjustment range. If the seat cannot be adjusted to the midpoint of the
longitudinal adjustment range, the closest adjustment position to the
rear of the midpoint shall be used.
    S<IP_ADDRESS>.2 Adjust the driver's seat to the lowest point of all
vertical adjustment ranges present.
    S<IP_ADDRESS>.3 Using the three dimensional SAE Standard J826 JUL95
(incorporated by reference, see Sec.  571.5) manikin, adjust the
driver's seat back angle at the vertical portion of the H-point
machine's torso weight hanger to 25 degrees. If this adjustment setting
is not available, adjust the seat-back angle to the positional detent
setting closest to 25 degrees in the direction of the manufacturer's
nominal design riding position.
    S14.1.3 Test object. Each test object is a right circular cylinder
that is 0.8 m high and 0.3 m in external diameter. There are seven test
objects, designated A through G, and they are marked as follows.
    (a) Test objects A, B, C, D, and E are marked with a horizontal
band encompassing the uppermost 150 mm of the side of the cylinder.
    (b) Test objects F and G are marked on the side with a solid
vertical stripe of 150 mm width extending from the top to the bottom of
each cylinder.
    (c) Both the horizontal band and vertical stripe shall be of a
color that contrasts with both the rest of the cylinder and the test
surface.
    S14.1.4 Test object locations and orientation. Place the test
objects at locations specified in S14.1.4(a)-(f) and illustrated in
Figure 5. Measure the distances shown in Figure 5 from a test object to
another test object or other object from the cylindrical center (axis)
of the test object as viewed from above. Each test object is oriented
so that its axis is vertical.
    (a) Place test objects F and G so that their centers are in a
transverse vertical plane that is 0.3 m to the rear of a transverse
vertical plane tangent to the rearmost surface of the rear bumper.
    (b) Place test objects D and E so that their centers are in a
transverse vertical plane that is 3.05 m to the rear of a transverse
vertical plane tangent to the rearmost surface of the rear bumper.
    (c) Place test objects A, B and C so that their centers are in a
transverse vertical plane that is 6.1 m to the rear of a transverse
vertical plane tangent to the rearmost surface of the rear bumper.
    (d) Place test object B so that its center is in a longitudinal
vertical plane passing through the vehicle's longitudinal centerline.
    (e) Place test objects C, E, and G so that their centers are in a
longitudinal vertical plane located 1.52 m, measured laterally and
horizontally, to the right of the vehicle longitudinal center line.
    (f) Place test objects A, D, and F so that their centers are in a
longitudinal vertical plane located 1.52 m, measured laterally and
horizontally, to the left of the vehicle longitudinal center line.
    S14.1.5 Test reference point. Obtain the test reference point using
the following procedure.
    (a) Locate the center of the forward-looking eye midpoint
(Mf) illustrated in Figure 6 so that it is 635 mm vertically
above the H point (H) and 96 mm aft of the H point.
    (b) Locate the head/neck joint center (J) illustrated in Figure 6
so that it is 100 mm rearward of Mf and 588 mm vertically
above the H point.
    (c) Draw an imaginary horizontal line between Mf and a
point vertically above J, defined as J2.
    (d) Rotate the imaginary line about J2 in the direction
of the rearview image until the straight-line distance between
Mf and the center of the display used to present the
rearview image required in this standard reaches the shortest possible
value.
    (e) Define this new, rotated location of Mf to be
Mr (eye midpoint rotated).
    S14.1.6 Display adjustment. If the display is mounted with a
rotational adjustment mechanism, adjust the display such that the
surface of the display is normal to the imaginary line traveling
through Mr and J2 or as near to normal as the
display adjustment will allow.
    S14.1.7 Steering wheel adjustment. The steering wheel is adjusted
to the position where the longitudinal centerline of all vehicle tires
are parallel to the longitudinal centerline of the vehicle. If no such
position exists, adjust the steering wheel to the position where the
longitudinal centerline of all vehicle tires are closest to parallel to
the longitudinal centerline of the vehicle.
    S14.1.8 Measurement procedure.
    (a) Locate a 35 mm or larger format still camera, video camera, or
digital equivalent such that the center of the camera's image plane is
located at Mr and the camera lens is directed at the center
of the display's rearview image.
    (b) Affix a ruler at the base of the rearview image in an
orientation perpendicular with a test object cylinder centerline. If
the vehicle head restraints obstruct the camera's view of the display,
they may be adjusted or removed.
    (c) Photograph the image of the visual display with the ruler
included in the frame and the rearview image displayed.
    S<IP_ADDRESS> Extract photographic data.
    (a) Using the photograph, measure the apparent length, of a 50 mm
delineated section of the in-photo ruler, along the ruler's edge,
closest to the rearview image and at a point near the horizontal center
of the rearview image.
    (b) Using the photograph, measure the horizontal width of the
colored band at the upper portion of each of the three test objects
located at positions A, B, and C in Figure 5.
    (c) Define the measured horizontal widths of the colored bands of
the three test objects as da, db, and dc.
    S<IP_ADDRESS> Obtain scaling factor. Using the apparent length of the
50 mm portion of the ruler as it appears in the photograph, divide this
apparent length by 50 mm to obtain a scaling factor. Define this
scaling factor as sscale.
    S<IP_ADDRESS> Determine viewing distance. Determine the actual distance
from the rotated eye midpoint location (Mr) to the center of
the rearview image. Define this viewing distance as aeye.
    S<IP_ADDRESS> Calculate visual angle subtended by test objects. Use the
following equation to calculate the subtended visual angles:
[GRAPHIC] [TIFF OMITTED] TR07AP14.006

    where i can take on the value of either test object A, B, or C, and
arcsine is calculated in units of degrees.
    S14.2 Image response time test procedure. The temperature inside
the vehicle during this test is any temperature between 15[deg]C and
25[deg]C. Immediately prior to commencing the actions listed in
subparagraphs (a)-(c) of this paragraph, all components of the rear
visibility system are in a powered off state. Then:
    (a) Open the driver's door to any width,
    (b) Close the driver's door
    (c) Activate the starting system using the key, and
    (d) Select the vehicle's reverse direction at any time not less
than 4.0 seconds and not more than 6.0 seconds after the driver's door
is opened. The driver door is open when the edge of the driver's door
opposite of the door's hinge is no longer flush with the exterior body
panel.
    S14.3 Durability test procedures. For the durability tests
specified in S14.3.1, S14.3.2, and S14.3.3, the external components are
mounted on an environmental test fixture.
    S14.3.1 Corrosion test procedure. The external components are
subjected to two 24-hour corrosion test cycles. In each corrosion test
cycle, the external components are subjected to a salt spray (fog) test
in accordance with ASTM

B117-03 (incorporated by reference, see Sec.  571.5) for a period of 24
hours. Allow 1 hour to elapse without spray between the two test
cycles.
    S14.3.2 Humidity exposure test procedure. The external components
are subjected to 24 consecutive 3-hour humidity test cycles. In each
humidity test cycle, external components are subjected to a temperature
of 100[deg]+7[deg]-0[deg] F (38[deg]+4[deg]-0[deg] C) with a relative
humidity of not less than 90% for a period of 2 hours. After a period
not to exceed 5 minutes, the external components are subjected to a
temperature of 32[deg] +5[deg] -0[emsp14][deg]F (0[deg] +3[deg] -0[deg]
C) and a humidity of not more than 30%  10% for 1 hour.
Allow no more than 5 minutes to elapse between each test cycle.
    S14.3.3 Temperature exposure test procedure. The external
components are subjected to 4 consecutive 2-hour temperature test
cycles. In each temperature test cycle, the external components are
first subjected to a temperature of 176[deg]
5[emsp14][deg]F (80[deg]  3[deg] C) for a period of one
hour. After a period not to exceed 5 minutes, the external components
are subjected to a temperature of 32[deg] +5[deg] -0[emsp14][deg]F
(0[deg] +3[deg] -0[deg] C) for 1 hour. Allow no more than 5 minutes to
elapse between each test cycle.
BILLING CODE 4910-59-P

[GRAPHIC] [TIFF OMITTED] TR07AP14.002

[GRAPHIC] [TIFF OMITTED] TR07AP14.003

BILLING CODE 4910-59-C
    S15 Rear visibility phase-in schedule. For the purposes of the
requirements in S15.1 through S15.7, production year means the 12-month
period between May 1 of one year and April 30 of the following year,
inclusive.
    S15.1 Vehicles manufactured on or after May 1, 2016 and before May
1, 2018. At any time during or after the production years ending April
30, 2017 and April 30, 2018, each manufacturer shall, upon request from
the Office of Vehicle Safety Compliance, provide information
identifying the vehicles (by make, model and vehicle identification
number) that have been certified as complying with S5.5.1 or S6.2.1 of
this standard. The manufacturer's designation of a vehicle as a
certified vehicle is irrevocable.
    S15.2 Vehicles manufactured on or after May 1, 2016 and before May
1, 2017. Except as provided in S15.4, for passenger cars, multipurpose
passenger vehicles, trucks, buses, and low-speed vehicles with a GVWR
of 4,536 kg or less, manufactured by a manufacturer on or after May 1,
2016, and before May

1, 2017, the number of such vehicles complying with S5.5.1 or S6.2.1
shall be not less than 10 percent of the manufacturer's--
    (a) Production of such vehicles during that period; or
    (b) Average annual production of such vehicles manufactured in the
three previous production years.
    S15.3 Vehicles manufactured on or after May 1, 2017 and before May
1, 2018. Except as provided in S15.4, for passenger cars, multipurpose
passenger vehicles, trucks, buses, and low-speed vehicles with a GVWR
of 4,536 kg or less, manufactured by a manufacturer on or after May 1,
2017, and before May 1, 2018, the number of such vehicles complying
with S5.5.1 or S6.2.1 shall be not less than 40 percent of the
manufacturer's--
    (a) Production of such vehicles during that period; or
    (b) Average annual production of such vehicles manufactured in the
three previous production years.
    S15.4 Exclusions from phase-in. The following vehicles shall not be
subject to the requirements in S15.1 through S15.3 but shall achieve
full compliance with this standard at the end of the phase-in period in
accordance with S5.5(b) and S6.2(b):
    (a) Vehicles that are manufactured by small manufacturers or by
limited line manufacturers.
    (b) Vehicles that are altered (within the meaning of 49 CFR 567.7)
before May 1, 2017, after having been previously certified in
accordance with part 567 of this chapter, and vehicles manufactured in
two or more stages before May 1, 2018.
    S15.5 Vehicles produced by more than one manufacturer. For the
purpose of calculating average annual production of vehicles for each
manufacturer and the number of vehicles manufactured by each
manufacturer under S15.1 through S15.3, a vehicle produced by more than
one manufacturer shall be attributed to a single manufacturer as
follows, subject to S15.6--
    (a) A vehicle that is imported shall be attributed to the importer.
    (b) A vehicle manufactured in the United States by more than one
manufacturer, one of which also markets the vehicle, shall be
attributed to the manufacturer that markets the vehicle.
    S15.6 A vehicle produced by more than one manufacturer shall be
attributed to any one of the vehicle's manufacturers specified by an
express written contract, reported to the National Highway Traffic
Safety Administration under 49 CFR part 585, between the manufacturer
so specified and the manufacturer to which the vehicle would otherwise
be attributed under S15.5.
    S15.7 Calculation of complying vehicles.
    (a) For the purposes of calculating the vehicles complying with
S15.2, a manufacturer may count a vehicle if it is manufactured on or
after May 1, 2016 but before May 1, 2017.
    (b) For purposes of complying with S15.3, a manufacturer may count
a vehicle if it is manufactured on or after May 1, 2017 but before May
1, 2018 and,
    (c) For the purposes of calculating average annual production of
vehicles for each manufacturer and the number of vehicles manufactured
by each manufacturer, each vehicle that is excluded from having to meet
the applicable requirement is not counted.

0
4. Section 571.500 is amended by adding S5(b)(11) to read as follows:

Sec.  571.500  Standard No. 500; Low-speed vehicles.

* * * * *
    S5. * * *
    (b) * * *
    (11) Low-speed vehicles shall comply with the rear visibility
requirements specified in paragraphs S6.2 of FMVSS No. 111.

PART 585--PHASE-IN REPORTING REQUIREMENTS

0
5. The authority citation for part 585 is revised to read as follows:

    Authority:  49 U.S.C. 322, 30111, 30115, 30117, and 30166;
delegation of authority at 49 CFR 1.95.

0
6. Add Subpart M to Part 585 to read as follows:

Subpart M--Rear Visibility Improvements Reporting Requirements

Sec.
585.121 Scope.
585.122 Purpose.
585.123 Applicability.
585.124 Definitions.
585.125 Response to inquiries.
585.126 Reporting requirements.
585.127 Records.

Subpart M--Rear Visibility Improvements Reporting Requirements

Sec.  585.121  Scope.

    This part establishes requirements for manufacturers of passenger
cars, of trucks, buses, multipurpose passenger vehicles and low-speed
vehicles with a gross vehicle weight rating (GVWR) of 4,536 kilograms
(kg) (10,000 pounds (lb)) or less, to submit a report, and maintain
records related to the report, concerning the number of such vehicles
that meet the rear visibility requirements in paragraphs S5.5 and S6.2
of Standard No. 111, Rear visibility (49 CFR 571.111).

Sec.  585.122  Purpose.

    The purpose of these reporting requirements is to assist the
National Highway Traffic Safety Administration in determining whether a
manufacturer has complied with the rear visibility requirements in
paragraphs S5.5 and S6.2 of Standard No. 111, Rear visibility (49 CFR
571.111).

Sec.  585.123  Applicability.

    This part applies to manufacturers of passenger cars, of trucks,
buses, multipurpose passenger vehicles and low-speed vehicles with a
gross vehicle weight rating (GVWR) of 4,536 kilograms (kg) (10,000
pounds (lb)) or less.

Sec.  585.124  Definitions.

    (a) All terms defined in 49 U.S.C. 30102 are used in their
statutory meaning.
    (b) Bus, gross vehicle weight rating or GVWR, low-speed vehicle,
multipurpose passenger vehicle, passenger car, and truck are used as
defined in Sec.  571.3 of this chapter.
    (c) Production year means the 12-month period between May 1 of one
year and April 30 of the following year, inclusive.

Sec.  585.125  Response to inquiries.

    At anytime during the production years ending April 30, 2017, and
April 30, 2018, each manufacturer shall, upon request from the Office
of Vehicle Safety Compliance, provide information identifying the
vehicles (by make, model and vehicle identification number) that have
been certified as complying with the rear visibility requirements in
paragraphs S5.5 and S6.2 of Standard No. 111, Rear visibility (49 CFR
571.111). The manufacturer's designation of a vehicle as a certified
vehicle is irrevocable.

Sec.  585.126  Reporting requirements.

    (a) Phase-in reporting requirements. Within 60 days after the end
of each of the production years ending April 30, 2017 and April 30,
2018, each manufacturer shall submit a report to the National Highway
Traffic Safety Administration concerning its compliance with the rear
visibility requirements in paragraphs S5.5 and S6.2 of Standard No. 111
(49 CFR 571.111) for its vehicles produced in that year. Each report
shall provide the

information specified in paragraph (b) of this section and in Sec.
585.2 of this part.
    (b) Phase-in report content-- (1) Basis for phase-in production
goals. Each manufacturer shall provide the number of vehicles
manufactured in the current production year, or, at the manufacturer's
option, in each of the three previous production years. A new
manufacturer that is, for the first time, manufacturing vehicles for
sale in the United States must report the number of vehicles
manufactured during the current production year.
    (2) Production of complying vehicles. Each manufacturer shall
report, for the production year being reported on, information on the
number of vehicles that meet the rear visibility requirements in
paragraphs S5.5 and S6.2 of Standard No. 111 (49 CFR 571.111).

Sec.  585.127  Records.

    Each manufacturer shall maintain records of the Vehicle
Identification Number for each vehicle for which information is
reported under Sec.  585.126 until April 30, 2022.

    Issued in Washington DC, on March 31, 2014 under authority
delegated in 49 CFR part 1.95.
David J. Friedman,
Acting Administrator.
[FR Doc. 2014-07469 Filed 4-1-14; 4:15 pm]
BILLING CODE 4910-59-P


[Federal Register: October 7, 2009 (Volume 74, Number 193)]
[Notices]
[Page 51614]
[DOCID:fr07oc09-83]

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DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-2009-N-0294]

Regulation of Tobacco Products; Extension of Comment Period;
Correction

AGENCY: Food and Drug Administration, HHS.

ACTION: Notice; extension of comment period; correction.

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

SUMMARY: The Food and Drug Administration (FDA) is correcting a notice;
extension of comment period that appeared in the Federal Register of
October 1, 2009 (74 FR 50810). The notice; extension of comment period
announced that FDA is extending to December 28, 2009, the comment
period for a notice that originally published in the Federal Register
of July 1, 2009 (74 FR 31457). The notice; extension of comment period
published with an inadvertent error in the DATES section. This document
corrects that error.

FOR FURTHER INFORMATION CONTACT: Joyce Strong, Office of Policy (HF-
27), Food and Drug Administration, 5600 Fishers Lane, Rockville, MD
20857,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: In FR Doc. E9-23607, appearing on page
50810, in the Federal Register of Thursday, October 1, 2009, the
following correction is made:
    1. On page 50810, in the second column, the ``DATES'' section is
corrected to read ``Submit electronic or written comments by December
28, 2009.''.

    Dated: October 1, 2009.
David Horowitz,
Assistant Commissioner for Policy.
[FR Doc. E9-24214 Filed 10-6-09; 8:45 am]

BILLING CODE 4160-01-S


Spray Foam Formulators in the U. S.

Industry Association Spray Polyurethane Foam Alliance ( SPFA) 4400 Fair Lakes Court, Suite 105 Fairfax, VA 22033 ( 703) 253 0660 Companies EPA is aware of 1. BASF 3000 Continental Drive North Mount Olive, NJ 07828 ( 979) 426 2600 2. Demilec 2925 Galleria Drive Arlington, Texas 76011 ( 817) 640 4900 3. Dow Chemical Co. ( in the docket in support of ban  document # 26) Polyurethane Systems North American Headquarters 1881 West Oak Parkway Marietta, Georgia 30062 ( 770) 428 2684 4. Foam Enterprises ( recently purchased by BASF) 13630 Watertower Circle Minneapolis, MN 55441 ( 763) 559 3342 5. Foam Supplies Inc. ( in the docket in support of ban  document # 3) 4387 North Rider Trail Earth City, MO 63045 ( 314) 344 3330 6. Gaco Western Po Box 88698 Seattle, WA 98138 ( 206) 575 0450 7. General Coatings ( in the docket requesting use of inventoried HCFC 141b  document # 16) 1220 East North Ave. Fresno, CA 93725 ( 559) 495 4004 8. Hydroseal 12151 Madera Way Riverside, CA 92503 ( 909) 272 2344 9. IsoTech 109 Cambria St. Newark, OH 43055 ( 740) 344 9554 10. North Carolina Foam Industries ( in the docket in support of ban  document # 4) PO Box 1528 Mount Airy, NC 27030 ( 336) 789 9161 11. Polythane Systems Inc. ( in the docket questioning the ban document # 22) Po Box 1452 Spring, TX 77383 ( 281) 350 9000 12. Resin Technology Company ( in the docket in support of ban  document # 39) 2270 Castle Harbor Place Ontario, CA 91761 ( 909) 947 7224 13. Stepan 22 West Frontage Road Northfield, IL 60093 ( 847) 446 7500 14. SWD Urethanes PO Box 1422 Mesa, AZ 85211 ( 480) 969 8413 15. UCSC Urethanes 3010 W. Lincoln Phoenix, AZ 85009 ( 888) 289 8272 16. Utah Foam Products PO Box 70838 Salt Lake City, UT 84119 ( 801) 269 0600


[Federal Register: January 23, 2009 (Volume 74, Number 14)]
[Notices]
[Page 4245-4246]
[DOCID:fr23ja09-96]

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DEPARTMENT OF LABOR

Occupational Safety and Health Administration

[Docket No. OSHA-2006-0048]

NSF International; Expansion of Recognition

AGENCY: Occupational Safety and Health Administration (OSHA), Labor.

ACTION: Notice.

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SUMMARY: This notice announces the Occupational Safety and Health
Administration's final decision expanding the recognition of NSF
International (NSF) as a Nationally Recognized Testing Laboratory under
29 CFR 1910.7.

DATES: The expansion of recognition becomes effective on January 23,
2009.

FOR FURTHER INFORMATION CONTACT: MaryAnn Garrahan, Director, Office of
Technical Programs and Coordination Activities, NRTL Program,
Occupational Safety and Health Administration, U.S. Department of
Labor, 200 Constitution Avenue, NW., Room N-3655, Washington, DC 20210,
or phone<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Notice of Final Decision

    The Occupational Safety and Health Administration (OSHA) hereby
gives notice of the expansion of recognition of NSF International
(NSF), as a Nationally Recognized Testing Laboratory (NRTL). NSF's
expansion covers the use of additional test standards. OSHA's current
scope of recognition for NSF may be found in the following
informational Web page: http://www.osha.gov/dts/otpca/nrtl/nsf.html.
    OSHA recognition of an NRTL signifies that the organization has met
the legal requirements in Section 1910.7 of Title 29, Code of Federal
Regulations (29 CFR 1910.7). Recognition is an acknowledgment that the
organization can perform independent safety testing and certification
of the specific products covered within its scope of recognition and is
not a delegation or grant of government authority. As a result of
recognition, employers may use products approved by the NRTL to meet
OSHA standards that require testing and certification.
    The Agency processes applications by an NRTL for initial
recognition, or for expansion or renewal of this recognition, following
requirements in Appendix A to 29 CFR 1910.7. This appendix requires
that the Agency publish two notices in the Federal Register in
processing an application. In the first notice, OSHA announces the
application and provides its preliminary finding and, in the second
notice, the Agency provides its final decision on the application.
These notices set forth the NRTL's scope of recognition or
modifications of that scope. We maintain an informational Web page for
each NRTL that details its scope of recognition. These pages can be
accessed from our Web site at http://www.osha.gov/dts/otpca/nrtl/
index.html.
    In an earlier action involving NSF, OSHA issued a Federal Register
notice to grant NSF's previous application, which was for an expansion
of recognition (71 FR 70431, December 4, 2006).
    NSF submitted another application, dated October 23, 2007 (see
Exhibit 18-1, as cited in the preliminary notice), to expand its
recognition to include one additional test standard. The NRTL Program
staff determined that the standard was an ``appropriate test standard''
within the meaning of 29 CFR 1910.7(c). In connection with this
request, OSHA did not perform an on-site review of NSF's NRTL testing
facilities. However, NRTL Program assessment staff reviewed information
pertinent to the request and recommended that NSF's recognition be
expanded to include the additional test standard listed below (see
Exhibit 18-2, as cited in the preliminary notice). Therefore, OSHA is
approving this one test standard for the expansion.
    Based on this review, OSHA published a preliminary notice
announcing the expansion application in the Federal Register on August
29, 2008 (73 FR 51008). Comments were requested by September 15, 2008,
but no comments were received in response to this notice. OSHA is now
proceeding with this final notice to grant NSF's expansion application.
    You may obtain or review copies of all public documents pertaining
to the NSF application by accessing http://www.regulations.gov, which
is the Federal eRulemaking Portal, or by contacting the Docket Office,
Occupational Safety and Health Administration, U.S. Department of
Labor, 200 Constitution Avenue, NW., Room N-2625, Washington, DC 20210.
Docket No. OSHA-2006-0048 contains all materials in the record
concerning NSF's recognition.
    The current address of the NSF facility (site) already recognized
by OSHA is: NSF International, 789 Dixboro Road, Ann Arbor, MI 48105.

Final Decision and Order

    NRTL Program staff has examined the application, the assessor's
recommendation, and other pertinent information. Based on this
examination and the assessor's recommendation, OSHA finds that NSF
meets the requirements of 29 CFR 1910.7 for expansion of its
recognition, subject to the limitation and conditions listed below.
Pursuant to the authority in 29 CFR 1910.7, OSHA hereby expands the
recognition of NSF, subject to this limitation and these conditions.

Limitation

    OSHA limits the expansion of NSF's recognition to testing and
certification of products for demonstration of conformance to the
following test standard, OSHA determined is an appropriate test
standard within the meaning of 29 CFR 1910.7(c): UL 1285 Pipe and
Couplings, Polyvinyl Chloride (PVC), for Underground Fire Service.
    The designation and title of this test standard was current at the
time of the preparation of the preliminary notice.
    OSHA's recognition of NSF, or any NRTL, for a particular test
standard is limited to equipment or materials (i.e., products) for
which OSHA standards require third-party testing and certification
before use in the workplace. Consequently, if a test standard also
covers any product(s) for which OSHA does not require such testing and
certification, an NRTL's scope of recognition does not include that
product(s).
    The test standard listed above may be approved as an American
National Standard by the American National Standards Institute (ANSI).
However, for convenience, we use the designation of the standards-
developing organization for the standard, as opposed to the ANSI
designation. You may contact ANSI to find out whether a test standard
is currently ANSI approved.

Conditions

    NSF also must abide by the following conditions of the recognition,
in

addition to those conditions already required by 29 CFR 1910.7:
    1. NSF must allow OSHA access to its facilities and records to
ascertain continuing compliance with the terms of its recognition and
to perform investigations, as OSHA deems necessary;
    2. If NSF has reason to doubt the efficacy of any test standard it
is using under this program, it must promptly inform the test standard-
developing organization of this concern and provide that organization
with appropriate relevant information on which its concern is based;
    3. NSF must not engage in, or permit others to engage in, any
misrepresentation of the scope or conditions of its recognition. As
part of this condition, NSF agrees that it will allow no representation
that it is either a recognized or an accredited Nationally Recognized
Testing Laboratory (NRTL) without clearly indicating the specific
equipment or material to which this recognition applies, and also
clearly indicating that its recognition is limited to certain products;
    4. NSF must inform OSHA as soon as possible, in writing, of any
change of ownership, facilities, or key personnel, and of any major
changes in its operations as an NRTL, including details of these
changes;
    5. NSF will meet all the terms of its recognition and will comply
with all OSHA policies pertaining to this recognition; and
    6. NSF will continue to meet the requirements for recognition in
all areas where it has been recognized.

Authority and Signature

    Thomas M. Stohler, Acting Assistant Secretary of Labor for
Occupational Safety and Health, U.S. Department of Labor, 200
Constitution Avenue, NW., Washington, DC 20210, directed the
preparation of this notice. Accordingly, the Agency is issuing this
notice pursuant to Sections 6(b) and 8(g) of the Occupational Safety
and Health Act of 1970 (29 U.S.C. 655 and 657), Secretary of Labor's
Order 5-2007 (72 FR 31160), and 29 CFR 1911.

    Signed at Washington, DC, on January 15, 2009.
Thomas M. Stohler
Acting Assistant Secretary of Labor for Occupational Safety and Health.
 [FR Doc. E9-1290 Filed 1-22-09; 8:45 am]

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[Federal Register Volume 84, Number 216 (Thursday, November 7, 2019)]
[Proposed Rules]
[Pages 60001-60003]
[FR Doc No: 2019-24269]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0863; Product Identifier 2019-NM-157-AD]
RIN 2120-AA64

Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Airbus SAS Model A318-112, A319-111, A319-112, A319-113,
A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212,
A320-214, A320-216, A320-231, A320-232, A320-233, A320-251N, and A320-
271N airplanes. This proposed AD was prompted by a report of marginal
clearance between certain fuel sensor covers on both left-hand (LH) and
right-hand (RH) wings. This proposed AD would require the replacement
of certain fuel level sensor brackets, as specified in a European Union
Aviation Safety Agency (EASA) AD, which will be incorporated by
reference. The FAA is proposing this AD to address the unsafe condition
on these products.

DATES: The FAA must receive comments on this proposed AD by December
23, 2019.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to https://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 the material identified in this proposed AD that will be
incorporated by reference (IBR), contact the EASA, Konrad-Adenauer-Ufer
3, 50668 Cologne, Germany; telephone +49 221 89990 1000; email
<EMAIL_ADDRESS>internet www.easa.europa.eu. You may find this IBR
material on the EASA website at https://ad.easa.europa.eu. You may view
this IBR material at the FAA, Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>. It is also available in the AD
docket on the internet at http://www.regulations.gov by searching for
and locating Docket No. FAA-2019-0863.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0863; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this NPRM, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations is listed above.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites 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-2019-0863;
Product Identifier 2019-NM-157-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM based on those comments.
    The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this NPRM.

Discussion

    The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2019-0197, dated August 14, 2019
(``EASA AD 2019-0197'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Airbus SAS Model A318-112, A319-111, A319-112,
A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211,
A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233,
A320-251N, and A320-271N airplanes. Model A320-215 airplanes are not on
the U.S. Register; this AD therefore does not include those airplanes
in the applicability.
    This proposed AD was prompted by a report of marginal clearance
between certain fuel sensor covers on rib 24 and the crown of stringer
15 on both LH and RH wings. A possible contact between the shield and
the stringer, and/or possible motion between the stringer and the
shield, can make the gap more susceptible to sparking in case of
lightning strike. The FAA is proposing this AD to address this
condition, which could create a source of ignition in a fuel tank vapor
space, possibly resulting in a fire or explosion and consequent loss of
the airplane. See the MCAI for additional background information.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2019-0197 describes procedures for the replacement of
certain fuel level sensor brackets. This material is reasonably
available because the interested parties have access to it through
their normal course of business or by the means identified in the
ADDRESSES section.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to a bilateral agreement with the State of Design Authority, the FAA
has been notified of the unsafe condition described in the MCAI
referenced above. The FAA is proposing this AD because the agency
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 EASA AD 2019-0197 described previously, as incorporated by
reference, except for any differences identified as exceptions in the
regulatory text of this AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA initially worked with Airbus and EASA to develop a
process to use certain EASA ADs as the primary source of information
for compliance with requirements for corresponding FAA ADs. The FAA has
since coordinated with other manufacturers and civil aviation
authorities (CAAs) to use this process. As a result, EASA AD 2019-0197
will be incorporated by reference in the FAA final rule. This proposed
AD would, therefore, require compliance with EASA AD 2019-0197 in its
entirety, through that incorporation, except for any differences
identified as exceptions in the regulatory text of this proposed AD.
Using common terms that are the same as the heading of a particular
section in the EASA AD does not mean that operators need comply only
with that section. For example, where the AD requirement refers to
``all required actions and compliance times,'' compliance with this AD
requirement is not limited to the section titled ``Required Action(s)
and Compliance Time(s)'' in the EASA AD. Service information specified
in EASA AD 2019-0197 that is required for compliance with EASA AD 2019-
0197 will be available on the internet at https://www.regulations.gov
by searching for and locating Docket No. FAA-2019-0863 after the FAA
final rule is published.

Costs of Compliance

    The FAA estimates that this proposed AD affects 776 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
          Labor cost                    Parts cost               Cost per product        Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 7 work-hour x $85 per     Up to $609................  Up to $1,204.............  Up to $934,304.
 hour = Up to $595.
----------------------------------------------------------------------------------------------------------------

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.
    The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
    This proposed AD is issued in accordance with authority delegated
by the Executive Director, Aircraft Certification Service, as
authorized by FAA Order 8000.51C. In accordance with that order,
issuance of ADs is normally a function of the Compliance and
Airworthiness Division, but during this transition period, the
Executive Director has delegated the authority to issue ADs applicable
to transport category airplanes and associated

appliances to the Director of the System Oversight Division.

Regulatory Findings

    The FAA 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) Will not affect intrastate aviation in Alaska, 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.

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

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive (AD):

Airbus SAS: Docket No. FAA-2019-0863; Product Identifier 2019-NM-
157-AD.

(a) Comments Due Date

    The FAA must receive comments by December 23, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus SAS Model A318-112, A319-111, A319-
112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133,
A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320-
233, A320-251N, and A320-271N airplanes, certificated in any
category, as identified in European Union Aviation Safety Agency
(EASA) AD 2019-0197, dated August 14, 2019 (``EASA AD 2019-0197'').

(d) Subject

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) Reason

    This AD was prompted by a report of marginal clearance between
certain fuel sensor covers on rib 24 and the crown of stringer 15 on
both left-hand (LH) and right-hand (RH) wings. A possible contact
between the shield and the stringer, and/or possible motion between
the stringer and the shield, can make the gap more susceptible to
sparking in case of lightning strike. The FAA is issuing this AD to
address this condition, which could create a source of ignition in a
fuel tank vapor space, possibly resulting in a fire or explosion and
consequent loss of the airplane.

(f) Compliance

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

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2019-0197.

(h) Exceptions to EASA AD 2019-0197

    (1) Where EASA AD 2019-0197 refers to its effective date, this
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2019-0197 does not apply
to this AD.

(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (j)(2) of this AD. Information
may be emailed to<EMAIL_ADDRESS>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.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS's
EASA Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
    (3) Required for Compliance (RC): For any service information
referenced in EASA AD 2019-0197 that contains RC procedures and
tests: Except as required by paragraph (i)(2) of this AD, RC
procedures and tests must be done to comply with this AD; any
procedures or tests that are not identified as RC are recommended.
Those procedures and tests that are not identified as RC may be
deviated from using accepted methods in accordance with the
operator's maintenance or inspection program without obtaining
approval of an AMOC, provided the procedures and tests identified as
RC can be done and the airplane can be put back in an airworthy
condition. Any substitutions or changes to procedures or tests
identified as RC require approval of an AMOC.

(j) Related Information

    (1) For information about EASA AD 2019-0197, contact the EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
89990 6017; email<EMAIL_ADDRESS>internet www.easa.europa.eu.
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu. You may view this material at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195. This material may be found in the AD docket on the
internet at https://www.regulations.gov by searching for and
locating Docket No. FAA-2019-0863.
    (2) For more information about this AD, contact Sanjay Ralhan,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax<PHONE_NUMBER>.

    Issued in Des Moines, Washington, on November 1, 2019.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-24269 Filed 11-6-19; 8:45 am]
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