[Federal Register: August 12, 2009 (Volume 74, Number 154)]
[Rules and Regulations]
[Page 40488-40494]
[DOCID:fr12au09-7]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 95

[Docket No. 30680; Amdt. No. 482]

IFR Altitudes; Miscellaneous Amendments

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: This amendment adopts miscellaneous amendments to the required
IFR (instrument flight rules) altitudes and changeover points for
certain Federal airways, jet routes, or direct routes for which a
minimum or maximum en route authorized IFR altitude is prescribed. This
regulatory action is needed because of changes occurring in the
National Airspace System. These changes are designed to provide for the
safe and efficient use of the navigable airspace under instrument
conditions in the affected areas.

DATES: Effective Date: 0901 UTC, August 27, 2009.

FOR FURTHER INFORMATION CONTACT: Harry Hodges, Flight Procedure
Standards Branch (AMCAFS-420), Flight Technologies and Programs
Division, Flight Standards Service, Federal Aviation Administration,
Mike Monroney Aeronautical Center, 6500 South MacArthur Blvd., Oklahoma
City, OK 73169 (Mail Address: P.O. Box 25082, Oklahoma City, OK 73125)
telephone:<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: This amendment to part 95 of the Federal
Aviation Regulations (14 CFR part 95) amends, suspends, or revokes IFR
altitudes governing the operation of all aircraft in flight over a
specified route or any portion of that route, as well as the changeover
points (COPs) for Federal airways, jet routes, or direct routes as
prescribed in part 95.

The Rule

    The specified IFR altitudes, when used in conjunction with the
prescribed changeover points for those routes, ensure navigation aid
coverage that is adequate for safe flight operations and free of
frequency interference. The reasons and circumstances that create the
need for this amendment involve matters of flight safety and
operational efficiency in the National Airspace System, are related to
published aeronautical charts that are essential to the user, and
provide for the safe and efficient use of the navigable airspace. In
addition, those various reasons or circumstances require making this
amendment effective before the next scheduled charting and publication
date of the flight information to assure its timely availability to the
user. The effective date of this amendment reflects those
considerations. In view of the close and immediate relationship between
these regulatory changes and safety in air commerce, I find that notice
and public procedure before adopting this amendment are impracticable
and contrary to the public interest and that good cause exists for
making the amendment effective in less than 30 days.

Conclusion

    The FAA has determined that this regulation only involves an
established body of technical regulations for which frequent and
routine amendments are necessary to keep them operationally current.
It, therefore--(1) is not a ``significant regulatory action'' under
Executive Order 12866; (2) is not a ``significant rule'' under DOT
Regulatory Policies and Procedures (44 FR 11034; February 26, 1979);
and (3) does not warrant preparation of a regulatory evaluation as the
anticipated impact is so minimal. For the same reason, the FAA
certifies that this amendment will not have a significant economic
impact on a substantial number of small entities under the criteria of
the Regulatory Flexibility Act.

    Issued in Washington, DC, on July 24, 2009.
John M. Allen,
Director, Flight Standards Service.

List of Subjects in 14 CFR Part 95

    Airspace, Navigation (air).

Adoption of the Amendment

0
Accordingly, pursuant to the authority delegated to me by the
Administrator, part 95 of the Federal Aviation Regulations (14 CFR part
95) is amended as follows effective at 0901 UTC, August 27, 2009.
0
1. The authority citation for part 95 continues to read as follows:

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

0
2. Part 95 is amended to read as follows:

                                 Revisions to IFR Altitudes & Changeover Points
                                 [Amendment 482 Effective Date August 27, 2009]
----------------------------------------------------------------------------------------------------------------
                     From                                         To                        MEA          MAA
----------------------------------------------------------------------------------------------------------------
                                    Sec.   95.4000 High Altitude RNAV Routes
----------------------------------------------------------------------------------------------------------------
                            Sec.   95.4016 RNAV Route Q16 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
KODIAK, AK VOR/DME GNSS MEA..........  MIDDLETON ISLAND, AK VOR/DME..........        18000        45000
----------------------------------------------------------------------------------------------------------------
                                              Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
MIDDLETON ISLAND, AK VOR/DME GNSS MEA  YAKUTAT, AK VOR/DME...................        18000        45000
----------------------------------------------------------------------------------------------------------------

                                 Sec.   95.4041 RNAV Route Q41 Is Added To Read
----------------------------------------------------------------------------------------------------------------
*CAWIN, AK FIX                                  DEADHORSE, AK VOR/DME.................        18000        45000
    *12000-MRA GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4042 RNAV Route Q42 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KIRKSVILLE, MO VORTAC.........................  DANVILLE, IL VORTAC...................  *3        45000
                                                                                4000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
DANVILLE, IL VORTAC...........................  MUNCIE, IN VOR/DME....................  *3        45000
                                                                                4000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
MUNCIE, IN VOR/DME............................  BRNAN, PA FIX.........................  *2        45000
                                                                                4000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
BRNAN, PA FIX.................................  MAALS, PA FIX.........................  *2        45000
                                                                                6000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
MAALS, PA FIX.................................  EAST TEXAS, PA VOR/DME................  *2        45000
                                                                                4000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
EAST TEXAS, PA VOR/DME........................  ELIOT, NJ FIX.........................  *2        45000
                                                                                4000
    *18000-GNSS MEA
    DME/DME/IRU RNAV MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4043 RNAV Route Q43 Is Added To Read
----------------------------------------------------------------------------------------------------------------
ANCHORAGE, AK VOR/DME.........................  FAIRBANKS, AK VORTAC..................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4044 RNAV Route Q44 Is Added To Read
----------------------------------------------------------------------------------------------------------------
NOME, AK VOR/DME..............................  ANCHORAGE, AK VOR/DME.................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4045 RNAV Route Q45 Is Added To Read
----------------------------------------------------------------------------------------------------------------
DILLINGHAM, AK VOR/DME........................  AMOTT, AK FIX.........................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4046 RNAV Route Q46 Is Added To Read
----------------------------------------------------------------------------------------------------------------
POINT HOPE, AK NDB............................  BARROW, AK VOR/DME....................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4047 RNAV Route Q47 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KING SALMON, AK VORTAC........................  AMOTT, AK FIX.........................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4048 RNAV Route Q48 Is Added To Read
----------------------------------------------------------------------------------------------------------------
BARROW, AK VOR/DME............................  DEADHORSE, AK VOR/DME.................  18        45000
                                                                                000
    GNSS MEA
DEADHORSE, AK VOR/DME.........................  ROCES, AK FIX.........................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4049 RNAV Route Q49 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KODIAK, AK VOR/DME............................  AMOTT, AK FIX.........................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4051 RNAV Route Q51 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KING SALMON, AK VORTAC........................  KOTZEBUE, AK VOR/DME..................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4053 RNAV Route Q53 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KODIAK, AK VOR/DME............................  ILIAMNA, AK NDB/DME...................  18        45000
                                                                                000

    GNSS MEA
----------------------------------------------------------------------------------------------------------------
ILIAMNA, AK NDB/DME...........................  KOTZEBUE, AK VOR/DME..................  18        45000
                                                                                000
    GNSS MEA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4055 RNAV Route Q55 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KODIAK, AK VOR/DME............................  NOME, AK VOR/DME......................  18        45000
                                                                                000
    GNSS MEA
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                                 Sec.   95.4057 RNAV Route Q57 Is Added To Read
----------------------------------------------------------------------------------------------------------------
KING SALMON, AK VORTAC........................  MC GRATH, AK VORTAC...................  18        45000
                                                                                000
    GNSS MEA
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                               Sec.   95.4059 RNAV Route Q59 Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
COLD BAY, AK VORTAC...........................  BETHEL, AK VORTAC.....................  18        45000
                                                                                000
    GNSS MEA
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                                 Sec.   95.4061 RNAV Route Q61 Is Added To Read
----------------------------------------------------------------------------------------------------------------
FAIRBANKS, AK VORTAC..........................  BARROW, AK VOR/DME....................  18        45000
                                                                                000
    GNSS MEA
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                            Sec.   95.4219 RNAV Route T219 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
NANWAK, AK NDB/DME............................  RUFVY, AK FIX.........................        *2300        17500
    *1700-MOCA
RUFVY, AK FIX.................................  ACATE, AK FIX.........................        *2000        17500
    *1300-MOCA
ACATE, AK FIX.................................  BROUS, AK FIX.........................        *6000        17500
    *5400-MOCA
BROUS, AK FIX.................................  DILLINGHAM, AK VOR/DME................        *6000        17500
    *5000-MOCA
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                            Sec.   95.4222 RNAV Route T222 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
MOUNT MOFFETT, AK, NDB/DME....................  BAERE, AK FIX.........................        *6000        17500
BAERE, AK FIX.................................  ST PAUL ISLAND, AK NDB/DME............        *3600        17500
ST PAUL ISLAND, AK NDB/DME....................  RUFVY, AK FIX.........................        *3000        17500
    *1800-MOCA
RUFVY, AK FIX.................................  BETHEL, AK VORTAC.....................        *3000        17500
    *1400-MOCA
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                            Sec.   95.4223 RNAV Route T223 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
CAPE NEWENHAM, AK NDB/DME.....................  DILLINGHAM, AK VOR/DME................         4400        17500
DILLINGHAM, AK VOR/DME........................  FAGIN, AK FIX.........................         4400        17500
FAGIN, AK FIX.................................  NONDA, AK FIX.........................         8400        17500
NONDA, AK FIX.................................  BLUGA, AK FIX.........................        12000        17500
BLUGA, AK FIX.................................  AMOTT, AK FIX.........................         3000        17500
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                                              Is Amended To Delete
----------------------------------------------------------------------------------------------------------------
AMOTT, AK FIX.................................  ANCHORAGE, AK VOR/DME.................         2000        17500
----------------------------------------------------------------------------------------------------------------
                            Sec.   95.4225 RNAV Route T225 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
HOOPER BAY, AK VOR/DME........................  AKELT, AK FIX.........................         4600        17500
AKELT, AK FIX.................................  ALMOT, AK FIX.........................         4400        17500
ALMOT, AK FIX.................................  UNALAKLEET, AK VOR/DME................         3700        17500
UNALAKLEET, AK VOR/DME........................  EDMON, AK FIX.........................         5000        17500
EDMON, AK FIX.................................  VENCE, AK FIX.........................         5900        17500
VENCE, AK FIX.................................  GALENA, AK VOR/DME....................         3400        17500
GALENA, AK VOR/DME............................  KUHZE, AK FIX.........................         3400        17500
KUHZE, AK FIX.................................  CHOKK, AK FIX.........................         6800        17500
CHOKK, AK FIX.................................  TANANA, AK VOR/DME....................         4000        17500
TANANA, AK VOR/DME............................  *REEBA, AK FIX........................         3600        17500
    *7000-MRA
REEBA, AK FIX.................................  FAIRBANKS, AK VORTAC..................         4500        17500
----------------------------------------------------------------------------------------------------------------

                            Sec.   95.4227 RNAV Route T227 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
SHEMYA, AK NDB................................  JANNT, AK FIX.........................         3400        17500
JANNT, AK FIX.................................  BAERE, AK FIX.........................         2900        17500
BAERE, AK FIX.................................  ALEUT, AK FIX.........................         3300        17500
ALEUT, AK FIX.................................  MORDI, AK FIX.........................         2500        17500
MORDI, AK FIX.................................  BINAL, AK FIX.........................         4900        17500
BINAL, AK FIX.................................  PORT HEIDEN, AK NDB/DME...............         3800        17500
PORT HEIDEN, AK NDB/DME.......................  AMOTT, AK FIX.........................        13000        17500
AMOTT, AK FIX.................................  ANCHORAGE, AK VOR/DME.................         4000        17500
ANCHORAGE, AK VOR/DME.........................  FAIRBANKS, AK VORTAC..................         9700        17500
FAIRBANKS, AK VORTAC..........................  DEADHORSE, AK VOR/DME.................        11000        17500
----------------------------------------------------------------------------------------------------------------
                            Sec.   95.4228 RNAV Route T228 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
CAPE NEWENHAM, AK NDB/DME.....................  KUCYE, AK FIX.........................         4600        17500
KUCYE, AK FIX.................................  RUFVY, AK FIX.........................         2000        17500
RUFVY, AK FIX.................................  HOOPER BAY, AK VOR/DME................         3000        17500
----------------------------------------------------------------------------------------------------------------
                            Sec.   95.4231 RNAV Route T231 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
FAIRBANKS, AK VORTAC..........................  SELAWIK, AK VOR/DME...................         6300        17500
SELAWIK, AK VOR/DME...........................  KOTZEBUE, AK VOR/DME..................         3400        17500
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                           Sec.   95.4231 RNAV Route T232 Is Amended To Delete In Part
----------------------------------------------------------------------------------------------------------------
OLARU, AK FIX.................................  NORTHWAY, AK VORTAC...................         6000        17500
    5400-MOCA
----------------------------------------------------------------------------------------------------------------
                           Sec.   95.4240 RNAV Route T240 Is Amended To Delete In Part
----------------------------------------------------------------------------------------------------------------
EVANSVILLE, AK NDB............................  NAMRE, AK FIX.........................        10000        17500
----------------------------------------------------------------------------------------------------------------
                                           Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
BETTLES, AK VOR/DME...........................  TEGDE, AK FIX.........................         7800        17500
TEGDE, AK FIX.................................  DERIK, AK FIX.........................         9700        17500
DERIK, AK FIX.................................  SHELO, AK FIX.........................         3600        17500
SHELO, AK FIX.................................  DEADHORSE, AK VOR/DME.................         2000        17500
----------------------------------------------------------------------------------------------------------------
                               Sec.   95.4246 RNAV Route T246 Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
BARROW, AK VOR/DME............................  GALENA, AK VOR/DME....................         9200        17500
----------------------------------------------------------------------------------------------------------------
                                           Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
GALENA, AK VOR/DME............................  MC GRATH, AK VORTAC...................         5800        17500
MC GRATH, AK VORTAC...........................  ANCHORAGE, AK VOR/DME.................         8700        17500
----------------------------------------------------------------------------------------------------------------
                               Sec.   95.4248 RNAV Route T248 Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
GAMBELL, AK NDB/DME...........................  QAYAQ, AK FIX.........................         3600        17500
----------------------------------------------------------------------------------------------------------------
                                           Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
QAYAQ, AK FIX.................................  EMMONAK, AK VOR/DME...................         3000        17500
----------------------------------------------------------------------------------------------------------------
                            Sec.   95.4250 RNAV Route T250 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
BETHEL, AK VORTAC.............................  AKELT, AK FIX.........................         3800        17500
AKELT, AK FIX.................................  QAYAQ, AK FIX.........................         3000        17500
QAYAQ, AK FIX.................................  KUKULIAK, AK VOR/DME..................         3700        17500
----------------------------------------------------------------------------------------------------------------
                               Sec.   95.4252 RNAV Route T252 Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
NOME, AK VOR/DME..............................  KOTZEBUE, AK VOR/DME..................         5900        17500
----------------------------------------------------------------------------------------------------------------
                               Sec.   95.4260 RNAV Route T260 Is Amended By Adding
----------------------------------------------------------------------------------------------------------------
NOME, AK VOR/DME..............................  TIN CITY, AK NDB/DME..................         6900        17500
----------------------------------------------------------------------------------------------------------------

                                           Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
TIN CITY, AK NDB/DME..........................  COGNU, AK FIX.........................         5300        17500
COGNU, AK FIX.................................  POINT HOPE, AK NDB....................         3000        17500
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4269 RNAV Route T269 Is Added To Read
----------------------------------------------------------------------------------------------------------------
BETHEL, AK VORTAC.............................  SPARREVOHN, AK VOR/DME................         6800        17500
SPARREVOHN, AK VOR/DME........................  ANCHORAGE, AK VOR/DME.................        11300        17500
ANCHORAGE, AK VOR/DME.........................  JOHNSTONE POINT, AK VOR/DME...........         9000        17500
JOHNSTONE POINT, AK VOR/DME...................  YAKUTAT, AK VOR/DME...................         5900        17500
YAKUTAT, AK VOR/DME...........................  BIORKA ISLAND, AK VORTAC..............         6200        17500
BIORKA ISLAND, AK VORTAC......................  ANNETTE ISLAND, AK VOR/DME............         7100        17500
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                                 Sec.   95.4273 RNAV Route T273 Is Added To Read
----------------------------------------------------------------------------------------------------------------
FAIRBANKS, AK VORTAC..........................  ROCES, AK FIX.........................        12000        17500
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4275 RNAV Route T275 Is Added To Read
----------------------------------------------------------------------------------------------------------------
BETHEL, AK VORTAC.............................  UNALAKLEET, AK VOR/DME................         5900        17500
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4277 RNAV Route T277 Is Added To Read
----------------------------------------------------------------------------------------------------------------
BETTLES, AK VOR/DME...........................  POINT LAY, AK NDB.....................        10300        17500
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4278 RNAV Route T278 Is Added To Read
----------------------------------------------------------------------------------------------------------------
*HAPIT, AK FIX................................  SISTERS ISLAND, AK VORTAC.............         6100        17500
    *15000-MRA
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4279 RNAV Route T279 Is Added To Read
----------------------------------------------------------------------------------------------------------------
ALEUT, AK FIX.................................  BETHEL, AK VORTAC.....................         3200        17500
----------------------------------------------------------------------------------------------------------------
                                 Sec.   95.4280 RNAV Route T280 Is Added To Read
----------------------------------------------------------------------------------------------------------------
FLIPS, AK FIX.................................  LEVEL ISLAND, AK VOR/DME..............         7100        17500
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                                 Sec.   95.4282 RNAV Route T282 Is Added To Read
----------------------------------------------------------------------------------------------------------------
VENCE, AK FIX.................................  HORSI, AK FIX.........................         5000        17500
HORSI, AK FIX.................................  PERZO, AK FIX.........................         4700        17500
PERZO, AK FIX.................................  FAIRBANKS, AK VORTAC..................         4300        17500
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               From                           To                 MEA
------------------------------------------------------------------------
                    Sec.   95.6001 Victor Routes-U.S.
------------------------------------------------------------------------
     Sec.   95.6003 VOR Federal Airway V3 Is Amended To Read In Part
------------------------------------------------------------------------
HARVY, VA FIX....................  *NUTTS, VA FIX..........       **6000
    *9000-MRA
    **4000-GNSS MEA
*NUTTS, VA FIX...................  FLAT ROCK, VA         **6000
                                    VORTAC.
    *9000-MRA
    **4000-GNSS MEA
     R-220 UNUSABLE
------------------------------------------------------------------------
    Sec.   95.6020 VOR Federal Airway V20 Is Amended To Read In Part
------------------------------------------------------------------------
RESERVE, LA VOR/DME..............  *SLIDD, LA FIX..........         2000
    *5000-MCA SLIDD, LA FIX, NE
     BND
SLIDD, LA FIX....................  GULFPORT, MS VORTAC.....        *5000
    *2000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6029 VOR FederaL Airway V29 Is Amended To Read In Part
------------------------------------------------------------------------
DUPONT, DE VORTAC.......  MODENA, PA VORTAC.......        *6000
    *1800-MOCA
    *2000-GNSS MEA

     R-358 UNUSABLE
------------------------------------------------------------------------
    Sec.   95.6051 VOR Federal Airway V51 Is Amended To Read In Part
------------------------------------------------------------------------
CRAIG, FL VORTAC.................  ALMA, GA VORTAC        *5000
    *1700-MOCA
    *4000-GNSS MEA
     R-144 NA BELOW
     10000
------------------------------------------------------------------------
    Sec.   95.6086 VOR Federal Airway V86 Is Amended To Read In Part
------------------------------------------------------------------------
MISSOULA, MT VOR/DME.............  COPPERTOWN, MT VOR/DME..       *13000
    *11300-MOCA
    *12000-GNSS MEA
*PACTO, SD FIX...................  RAPID CITY, SD VORTAC...
    E BND........................  ........................       **8000
    W BND........................  ........................       **9700
    *9700-MRA
    **7100-MOCA
------------------------------------------------------------------------
    Sec.   95.6106 VOR Federal Airway V106 Is Amended To Read In Part
------------------------------------------------------------------------
JOHNSTOWN, PA VORTAC.............  HUDON, PA FIX...........        *5000
    *4500-MOCA
HUDON, PA FIX....................  RASHE, PA FIX...........        *7000
    *4000-MOCA
    *4000-GNSS MEA
RASHE, PA FIX....................  SELINSGROVE, PA VORTAC..       *14000
    *4000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6114 VOR Federal Airway V114 Is Amended To Read In Part
------------------------------------------------------------------------
RESERVE, LA VOR/DME..............  *SLIDD, LA FIX..........         2000
    *5000-MCA SLIDD, LA FIX, NE
     BND
SLIDD, LA FIX....................  GULFPORT, MS VORTAC.....        *5000
    *2000-GNSS MEA
GULFPORT, MS VORTAC..............  EATON, MS VORTAC........        *6000
    *2000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6168 VOR Federal Airway V168 Is Amended To Read In Part
------------------------------------------------------------------------
MILER, AL FIX....................  EFORD, AL FIX...........        *3000
    *2400-MOCA
    *3000-GNSS MEA
EFORD, AL FIX....................  WIREGRASS, AL           2400
                                    VORTAC.
    R-360 UNUSABLE
     BEYOND EFORD
------------------------------------------------------------------------
    Sec.   95.6170 VOR Federal Airway V170 Is Amended To Read In Part
------------------------------------------------------------------------
MODENA, PA VORTAC................  DUPONT, DE             *6000
                                    VORTAC.
    *1800-MOCA
    *2000-GNSS MEA
      R-358 UNUSABLE
------------------------------------------------------------------------
    Sec.   95.6259 VOR Federal Airway V259 Is Amended To Read In Part
------------------------------------------------------------------------
*KOOKE, SC FIX...................  **CLETA, SC FIX.........         2000
    *3000-MRA
    **3000-MRA
*CLETA, SC FIX...................  FLORENCE, SC VORTAC.....         2000
    *3000-MRA
------------------------------------------------------------------------
    Sec.   95.6269 VOR Federal Airway V269 Is Amended To Read In Part
------------------------------------------------------------------------
HOVEL, ID FIX....................  FONNA, OR FIX...........       *12000
    *8700-MOCA
    *9000-GNSS MEA
MANTE, OR FIX....................  MOBIL, OR FIX...........       *10000
    *7600-MOCA
    *8000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6292 VOR Federal Airway V292 Is Amended To Read In Part
------------------------------------------------------------------------
*WIGAN, NY FIX...................  BARNES, MA           **10000
                                    VORTAC.
    *4500-MRA

    **4900-MOCA
    **5000-GNSS MEA
     R-279 UNUSABLE.
------------------------------------------------------------------------
    Sec.   95.6514 VOR Federal Airway V514 Is Amended To Read In Part
------------------------------------------------------------------------
*TWENTYNINE PALMS, CA VORTAC.....  GOFFS, CA VORTAC........      **12000
    *10200-MCA TWENTYNINE PALMS,
     CA VORTAC, NE BND
    **7900-MOCA
    **8000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6528 VOR Federal Airway V528 Is Amended To Read In Part
------------------------------------------------------------------------
*PHOENIX, AZ VORTAC..............  EAGUL, AZ FIX...........      **14500
    *8000-MCA PHOENIX, AZ VORTAC,
     NE BND
    **9400-MOCA
    **10000-GNSS MEA
------------------------------------------------------------------------
    Sec.   95.6538 VOR Federal Airway V538 Is Amended To Read In Part
------------------------------------------------------------------------
*TWENTYNINE PALMS, CA VORTAC.....  GOFFS, CA VORTAC........      **12000
    *10200-MCA TWENTYNINE PALMS,
     CA VORTAC, NE BND
    **7900-MOCA
    **8000-GNSS MEA
------------------------------------------------------------------------
Sec.   95.6480 Alaska VOR Federal Airway V480 Is Amended To Read In Part
------------------------------------------------------------------------
MOUNT MOFFETT, AK NDB/DME........  ST PAUL ISLAND, AK NDB/          6000
                                    DME.                       MAA-17500
ZESKA, AK FIX....................  BETHEL, AK VORTAC.......
                                   SW BND..................       *10000
                                   NE BND..................        *2000
    *1400-MOCA
------------------------------------------------------------------------

                     From                                         To                        MEA          MAA
----------------------------------------------------------------------------------------------------------------
                                            Sec.   95.7001 Jet Routes
----------------------------------------------------------------------------------------------------------------
                             Sec.   95.7051 JET Route J51 Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
TUBAS, NC FIX.................................  FLAT ROCK, VA VORTAC.........       *26000        45000
    *18000-GNSS MEA
     R-218 UNUSABLE
----------------------------------------------------------------------------------------------------------------
                             Sec.   95.7091 Jet Route J9 1Is Amended To Read In Part
----------------------------------------------------------------------------------------------------------------
CROSS CITY, FL VORTAC.........................  ATLANTA, GA VORTAC...........        24000        45000
    R-169 DME UNUSABLE
----------------------------------------------------------------------------------------------------------------

                                                                        Changeover Points
               Airway Segment                ----------------------------------------------------------------------
                                                              From                       To        Distance   From
------------------------------------------------------------------------------------------------------------ ------
     Sec.   95.8003 VOR Federal Airway Changeover Points Is Amended To Add Changeover Point Alaska V480
----------------------------------------------------------------------------------------------------------------
ST PAUL ISLAND, AK NDB/DME..................  BETHEL, AK VORTAC...................          223     *ST PAUL
                                                                                ISLAND.
----------------------------------------------------------------------------------------------------------------
                                    Is Amended To Delete Changeover Point
----------------------------------------------------------------------------------------------------------------
ST PAUL ISLAND, AK NDB/DME..................  KIPNUKL, AK VORTAC..................          197      ST PAUL
                                                                                ISLAND.
----------------------------------------------------------------------------------------------------------------

[FR Doc. E9-18851 Filed 8-11-09; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register: February 18, 2009 (Volume 74, Number 31)]
[Rules and Regulations]
[Page 7557]
[DOCID:fr18fe09-5]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Docket No. FAA-2008-1105; Airspace Docket No. 08-AGL-10]

Amendment of Class E Airspace; Atlantic, IA

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: This action amends Class E airspace at Atlantic, IA.
Additional controlled airspace is necessary to accommodate Area
Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at
Atlantic Municipal Airport, Atlantic, IA. The FAA is taking this action
to enhance the safety and management of Instrument Flight Rule (IFR)
operations at Atlantic Municipal Airport.

DATES: Effective Date: 0901 UTC, May 7, 2009. The Director of the
Federal Register approves this incorporation by reference action under
1 CFR Part 51, subject to the annual revision of FAA Order 7400.9 and
publication of conforming amendments.

FOR FURTHER INFORMATION CONTACT: Scott Enander, Central Service Center,
Operations Support Group, Federal Aviation Administration, Southwest
Region, 2601 Meacham Blvd., Ft. Worth, TX 76193-0530; telephone (817)
321-7716.

SUPPLEMENTARY INFORMATION:

History

    On December 8, 2008, the FAA published in the Federal Register a
notice of proposed rulemaking to amend Class E airspace at Atlantic,
IA, adding additional controlled airspace at Atlantic Municipal
Airport, Atlantic, IA. (73 FR 74376, Docket No. FAA-2008-1105).
Interested parties were invited to participate in this rulemaking
effort by submitting written comments on the proposal to the FAA. No
comments were received. Class E airspace designations are published in
paragraph 6005 of FAA Order 7400.9S signed October 3, 2008, and
effective October 31, 2008, which is incorporated by reference in 14
CFR Part 71.1. The Class E airspace designations listed in this
document will be published subsequently in that Order.

The Rule

    This action amends Title 14 Code of Federal Regulations (14 CFR)
Part 71 by amending Class E airspace at Atlantic, IA, adding additional
controlled airspace at Atlantic Municipal Airport, Atlantic, IA.
    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.
Therefore, this regulation: (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. Since this is a routine matter
that will only affect air traffic procedures and air navigation, it is
certified that this rule, when promulgated, will not have a significant
economic impact on a substantial number of small entities under the
criteria of the Regulatory Flexibility Act.
    The FAA's authority to issue rules regarding aviation safety is
found in Title 49 of the U.S. Code. Subtitle 1, Section 106, describes
the authority of the FAA Administrator. Subtitle VII, Aviation
Programs, describes in more detail the scope of the agency's authority.
This rulemaking is promulgated under the authority described in
Subtitle VII, Part A, Subpart I, Section 40103. Under that section, the
FAA is charged with prescribing regulations to assign the use of
airspace necessary to ensure the safety of aircraft and the efficient
use of airspace. This regulation is within the scope of that authority
as it adds additional controlled airspace at Atlantic Municipal
Airport, Atlantic, IA.

List of Subjects in 14 CFR Part 71

    Airspace, Incorporation by reference, Navigation (air).

Adoption of the Amendment

0
In consideration of the foregoing, the Federal Aviation Administration
amends 14 CFR Part 71 as follows:

PART 71--DESIGNATION OF CLASS A, B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND REPORTING POINTS

0
1. The authority citation for 14 CFR Part 71 continues to read as
follows:

    Authority: 49 U.S.C. 106(g), 40103, 40113, 40120; E.O. 10854, 24
FR 9565, 3 CFR, 1959-1963 Comp., p. 389.

Sec.  71.1  [Amended]

0
2. The incorporation by reference in 14 CFR Part 71.1 of the Federal
Aviation Administration Order 7400.9S, Airspace Designations and
Reporting Points, signed October 3, 2008, and effective October 31,
2008, is amended as follows:

Paragraph 6005 Class E airspace areas extending upward from 700
feet or more above the surface.

* * * * *

ACE IA E5 Atlantic, IA [Amended]

Atlantic Municipal Airport, IA
    (Lat. 41[deg]24'26'' N., long. 95[deg]02'49'' W.)

    That airspace extending upward from 700 feet above the surface
within a 6.8-mile radius of Atlantic Municipal Airport and within
3.4 miles each side of the 022[deg] bearing from the airport
extending from the 6.8-mile radius to 9.9 miles northeast of the
airport.
* * * * *

    Issued in Fort Worth, TX, on February 5, 2009.
Anthony D. Roetzel,
Manager, Operations Support Group, ATO Central Service Center.
[FR Doc. E9-3007 Filed 2-17-09; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register Volume 80, Number 50 (Monday, March 16, 2015)]
[Rules and Regulations]
[Pages 13486-13491]
[FR Doc No: 2015-05035]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0561; Directorate Identifier 2007-NM-223-AD;
Amendment 39-18111; AD 2015-05-01]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all The
Boeing Company Model 757-200, -200PF, -200CB, and -300 series
airplanes; and Model 767-200, -300, -300F, and -400ER series airplanes.
This AD was prompted by reports indicating that the counterweights in
some hub assemblies of the ram air turbine (RAT) could be understrength
and fracture when the RAT is rotating, and that some RAT hub assemblies
were delivered with balance washer retention screws that were
incorrectly heat-treated, and therefore, susceptible to fracture and
cracking. This AD requires a part number and serial number inspection
to determine if certain RAT hub assemblies are installed; and, for
affected RAT hub assemblies, doing an inspection for missing and
fractured balance washer screws, and replacement or rework if
necessary. We are issuing this AD to prevent an inoperative RAT, which,
following a dual engine shutdown in flight, will cause loss of all
hydraulic power to the primary flight controls, resulting in subsequent
loss of control of the airplane.

DATES: This AD is effective April 20, 2015.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of April 20,
2015.

ADDRESSES: For Boeing service information identified in this AD,
contact Boeing Commercial Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone
206-544-5000, extension 1; fax<PHONE_NUMBER>; email
<EMAIL_ADDRESS>Internet https://www.myboeingfleet.com. For
Hamilton Sundstrand service information identified in this AD, contact
Hamilton Sundstrand, Technical Publications, Mail Stop 302-9, 4747
Harrison Avenue, P.O. Box 7002, Rockford, IL 61125-7002; phone: 860-
654-3575; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>
Internet: http://www.hamiltonsundstrand.com. You may view this
referenced service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>. It is also
available on the Internet at http://www.regulations.gov by searching
for and locating Docket No. FAA-2008-0561.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2008-
0561; 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 (phone: 800-647-
5527) is Docket Management Facility, U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE., Washington, DC 20590.

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

Discussion

    We issued a supplemental notice of proposed rulemaking (SNPRM) to
amend 14 CFR part 39 by adding an AD that would apply to all The Boeing
Company Model 757-200, -200PF, -200CB, and -300 series airplanes; and
Model 767-200, -300, -300F, and -400ER series airplanes. The SNPRM
published in the Federal Register on April 24, 2014 (79 FR 22777). We
preceded the SNPRM with a notice of proposed rulemaking (NPRM) that
published in the Federal Register on May 20, 2008 (73 FR 29087). The
NPRM proposed to require doing an inspection to determine the part
number and serial number of the RAT hub assembly, and replacing the RAT
hub assembly with a new, serviceable, or reworked and re-identified RAT
hub assembly if necessary. The NPRM was prompted by reports indicating
that the counterweights in some hub assemblies of the RATs could be
understrength and fracture when the RAT is rotating. The

SNPRM proposed to add airplanes to the applicability; add an additional
part number and serial number inspection to determine if certain RAT
hub assemblies are installed; and, for affected RAT hub assemblies,
doing an inspection for missing and fractured balance washer screws,
and replacement if necessary to address an additional defect identified
within the RAT hub assembly. We are issuing this AD to prevent an
inoperative RAT, which, following a dual engine shutdown in flight,
will cause loss of all hydraulic power to the primary flight controls,
resulting in subsequent loss of control of the airplane.

Comments

    We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the SNPRM (79
FR 22777, April 24, 2014) and the FAA's response to each comment.

Request To Perform a Records Review in Lieu of an Inspection

    FedEx requested an option to perform a records review in lieu of an
inspection to determine if any suspect RAT hub assemblies are
installed. FedEx stated that this is to prevent unnecessary inspections
on future Model 767 airplanes delivered from Boeing.
    We agree with the commenter's request. The serial number
applicability relates to a sub-assembly of the RAT (the turbine hub
assembly serial number, and not the RAT serial number). Consequently,
many operators might not have such detailed records. However, if an
operator has records indicating the serial number of the turbine hub
assembly that is currently installed on the RAT of a particular
airplane, there is no need to deploy the RAT for inspection to
determine if this AD is applicable. Therefore, a review of airplane
maintenance records is acceptable in lieu of this inspection if the
part number and serial number of the RAT hub assembly can be
conclusively determined from that review. We have revised paragraphs
(g) and (h) of this AD accordingly.

Request for Additional Removal Options (Screw Replacement Information)

    United Airlines (UAL) requested that the SNPRM (79 FR 22777, April
24, 2014) be updated to include an additional scenario in which an
operator finds all balance washers in place, but one or more screws
fractured. UAL stated that paragraph 2.B.(5)(d) of Hamilton Sundstrand
Service Bulletin 730814-29-15, dated February 10, 2010 (for Model 757
airplanes); and paragraph 2.B.(5)(d) of Hamilton Sundstrand Service
Bulletin 729548-29-18, dated February 10, 2010 (for Model 767
airplanes); provide on-wing (or off-wing) procedures for the situation
where all balance washers are present, but one or more screws are
fractured. UAL stated that the operator has the option to remove the
screw shank still in the hole with vice grips or a screw extractor in
lieu of RAT or RAT hub replacement.
    We disagree with the commenter's request to not replace the RAT or
RAT hub assembly if all washers are in place, but one or more screws
are found fractured during the inspection required by paragraph (h)(1)
of this AD. In this scenario, since any fractured screw is found, the
RAT or RAT hub assembly needs to be replaced with a new, serviceable,
reworked, and re-identified RAT or RAT hub assembly.
    Multiple balance washers (of different weights) could be installed
in a location; therefore, depending on how the screw fractures, it may
be possible to lose one, but not all, balance washers. However, it is
most likely that the screw head and all balance washer(s) for that
location will be missing.
    However, it is also possible that a screw could fracture during its
removal (i.e., the screw was not found fractured during the inspection
required by paragraph (h)(1) of this AD). This scenario has been
reported on numerous occasions. In this case, it is not necessary to
remove the RAT hub assembly (or RAT) if removal of the fractured screw
is successful (i.e., successful removal of a screw that fractures
during its removal).
    The preamble of the SNPRM (79 FR 22777, April 24, 2014) included
the paragraph, ``Screw Replacement Information,'' to provide additional
clarification that if a screw fractures during any screw replacement
and the weight is still available, the balance weight can be installed
with the replacement screw. We further emphasize that screws should
only be replaced one at a time to prevent any potential for a removed
balance washer to be installed in a different location.
    We also provide the following additional information. The attempted
removal of a fractured screw can be done without replacement of the RAT
or RAT hub assembly only if the screw fractures during removal, and if
all balance washers originally installed at that location can be
positively accounted for and can be assembled back into that location.
We also note that there could be more than one washer installed at each
location. We have not changed this final rule in this regard.

Request To Not Require Returning Screws to Hamilton Sundstrand

    UAL requested the procedure to return all screws or remnants of
fractured screws to Hamilton Sundstrand for further investigation, as
specified in paragraph 2.E., ``Return Balance Washer Screws to Hamilton
Sundstrand,'' of Hamilton Sundstrand Service Bulletin 730814-29-15,
dated February 10, 2010 (for Model 757 airplanes); and in Hamilton
Sundstrand Service Bulletin 729548-29-18, dated February 10, 2010 (for
Model 767 airplanes); not be required. UAL stated that this is an
unnecessary requirement and will only burden the maintenance personnel
with additional logistical procedures that do not add value. UAL also
stated that the balance screw failure issue and root cause are well
understood by Hamilton Sundstrand and that returning failed screws will
not provide additional information.
    We agree with the commenter's request. Returning the screws or
fractured screws is not required since the issue is now well
understood. We have added new paragraph (h)(2)(iii) to this AD to
specifically exclude this requirement.

Request To Add New Paragraph To Clarify Compliance for Airplanes in
Production

    Boeing requested that a new paragraph be added to paragraph (i) of
the proposed AD (79 FR 22777, April 24, 2014), to read, ``New OEM RAT
hub assemblies not listed in (i)(1) or (i)(2) installed prior to
airplane delivery meet the requirements of paragraph (i). After
delivery, airline operators are responsible for maintaining paragraph
(i) compliance.'' Boeing stated that this language clarifies compliance
for Model 767 airplanes in production.
    We partially agree. We do not agree with the commenter's request to
add a new paragraph. However, we agree that clarification is necessary.
For airplanes on which new OEM RAT hub assemblies not listed in
paragraphs (i)(1) and (i)(2) of this AD are installed during
production, it is possible for suspect hub assemblies to be installed,
i.e., a suspect hub assembly might be removed from one airplane and
installed on another airplane. Therefore, an airplane delivered with
conforming parts may no longer have conforming parts due to the
interchangeability of parts in service. All airplanes must comply with
the requirements of paragraph (i) of this AD. We have not changed this
AD in this regard.

Request To Revise Paragraph (i) of the Proposed AD (79 FR 22777, April
24, 2014)

    Boeing requested that paragraph (i)(3) of the proposed AD (79 FR
22777, April 24, 2014) be revised to read as follows: ``As of the
effective date of this AD, no person may install a balance washer screw
having part number (P/N) MS24667-14, on the RAT hub assembly of any
airplane unless a records review can positively determine that the
screws did not come from Northeast Fasteners, lots 24057 and 30533.''
Boeing stated that this language would clarify that the P/N MS24667-14
screw is prohibited only for installation on RAT hub assemblies.
    We agree with the commenter's request. Screws having P/N MS24667-14
should not be installed on the RAT hub assembly unless operators can
guarantee the screws did not come from Northeast Fasteners, lots 24057
and 30533. Hamilton Sundstrand was the only company to receive screws
from lot 30533, so no other inventory should be contaminated with them.
Several organizations received screws from lot 24057. All customers who
received the defective screws have been advised of the non-conformance
in lot 24057. There was also a government-industry data exchange
program alert issued to notify other organizations of the potential for
the inventories to be contaminated.
    We have determined that balance washer screws with P/N MS24667-14
from Northeast Fasteners, lots 24057 and 30533, are non-conforming and
are unacceptable for use on the RAT hub assembly. The unsafe condition
of this AD is applicable to RAT balance washer screws; therefore, it is
appropriate to limit the required actions to balance washer screws
installed on RAT hub assemblies. We have changed paragraph (i)(3) of
this AD accordingly.

Request for Clarification of Previous Actions

    FedEx requested clarification concerning whether credit is given
for accomplishment of previous actions using Boeing Alert Service
Bulletin 757-29A0066, dated January 2, 2007 (for Model 757-200 and -
200PF series airplanes). FedEx stated that it has issued engineering
orders to inspect and replace the RAT hub assemblies, if required, for
possible fractured hub assembly counterweights using Boeing Alert
Service Bulletin 757-29A0066, dated January 2, 2007.
    We agree to provide clarification. Paragraph (k) of this AD
provides credit for the actions required by paragraph (g) of this AD,
if those actions were performed before the effective date of this AD
using the service information specified in Boeing Alert Service
Bulletin 757-29A0066, dated January 2, 2007 (for Model 757-200 and -
200PF series airplanes). Boeing Alert Service Bulletin 757-29A0066,
Revision 1, dated March 8, 2010 (for Model 757 airplanes), expanded the
airplane effectivity to include all Model 757 airplanes; no additional
work is specified in this revision of the service information. We have
not changed this AD in this regard.

Request To Revise the Costs of Compliance Paragraph

    Delta Air Lines (DAL) requested that the manpower and cost for
materials specified in Hamilton Sundstrand Service Bulletin 729548-29-
18, dated February 10, 2010, be added to the ``Costs of Compliance''
paragraph in the SNPRM (79 FR 22777, April 24, 2014). DAL stated that
after reviewing the service information and comparing the costs to the
SNPRM, two discrepancies were noted. DAL stated that in Hamilton
Sundstrand Service Bulletin 729548-29-18, dated February 10, 2010, it
states, ``For a turbine assembly or RAT with a missing balance washer,
or with a balance washer screw that cannot be removed in its entirety,
a maximum of 9.0 man-hours will be required to disassemble the unit as
necessary to remove the fractured screw and balance washer, balance the
turbine assembly, assemble the unit, and test the unit.'' DAL stated
that the 9 man-hour requirement and the cost for materials are not
specified in the SNPRM's ``Costs of Compliance'' paragraph.
    We agree that the labor costs specified in Hamilton Sundstrand
Service Bulletin 729548-29-18, dated February 10, 2010, were not
included in the ``Cost of Compliance'' paragraph in the SNPRM (79 FR
22777, April 24, 2014). We have revised the ``Costs of Compliance''
paragraph in this final rule to include 9 work-hours for the
replacement of balance washer screws. However, Hamilton Sundstrand
Service Bulletin 729548-29-18, dated February 10, 2010, does not
specify material costs and we have received no definitive data on
replacement costs.
    In addition, UTC Aerospace Systems has stated it will continue to
cover certain costs associated with the service information free of
charge for 24 months after the effective date of this final rule,
extending the expiration dates in the service information. We have also
added a warranty statement to the ``Costs of Compliance'' paragraph of
this final rule.

Conclusion

    We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the changes described previously and minor editorial
changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the
SNPRM (79 FR 22777, April 24, 2014) for correcting the unsafe
condition; and
     Do not add any additional burden upon the public than was
already proposed in the SNPRM (79 FR 22777, April 24, 2014).
    We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.

Related Service Information Under 1 CFR Part 51

    We reviewed the following service information. The service
information describes procedures for an inspection to determine the
part number and serial number of the RAT hub assembly and replacement
of the RAT or RAT hub assembly.
     Boeing Alert Service Bulletin 757-29A0066, Revision 1,
dated March 8, 2010.
     Boeing Alert Service Bulletin 767-29A0110, Revision 1,
dated March 8, 2010.
     Boeing Special Attention Service Bulletin 757-29-0069,
dated June 24, 2010.
     Boeing Special Attention Service Bulletin 767-29-0112,
dated June 24, 2010.
    We have also reviewed Hamilton Sundstrand Service Bulletin 729548-
29-15, dated November 30, 2005; and Hamilton Sundstrand Service
Bulletin 730814-29-12, dated November 30, 2005. The service information
describes procedures for rework and re-identification of RAT hub
assemblies.
    In addition, we have also reviewed Hamilton Sundstrand Service
Bulletin 729548-29-18, dated February 10, 2010; and Hamilton Sundstrand
Service Bulletin 730814-29-15, dated February 10, 2010. The service
information describes procedures for a general visual inspection for
missing washers and fractured screws of the rotor assembly and
replacement of balance washer screws; and inspection, rework, and re-
identification of RAT hub assemblies.
    This service information is reasonably available; see ADDRESSES for
ways to access this service information.

Costs of Compliance

    We estimate that this AD affects 1,132 airplanes of U.S. registry.

    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per       Cost on U.S.
               Action                        Labor cost           Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
Inspection..........................  1 work-hour x $85 per                $0              $85          $96,220
                                       hour = $85.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary replacements
that would be required based on the results of the inspection. We have
no way of determining the number of aircraft that might need these
replacements:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                 Action                          Labor cost            Parts cost          Cost per product
----------------------------------------------------------------------------------------------------------------
Replacement of balance washer screws...  Up to 9 work-hours x $85            \1\ $0  Up to $765.
                                          per hour = Up to $765.
Removal and installation of RAT          5 work-hours x $85 per                   0  $425.
 assembly.                                hour = $425.
Removal and installation of RAT hub      2 work-hours x $85 per                   0  $170.
 assembly.                                hour = $170.
----------------------------------------------------------------------------------------------------------------
\1\ We have received no definitive data on replacement costs.

    According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all labor costs in our cost
estimate. However, we have received no definitive data that would
enable us to provide cost estimates for the on-condition parts cost
specified in this AD.

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

    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),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

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

2015-05-01 The Boeing Company: Amendment 39-18111; Docket No. FAA-
2008-0561; Directorate Identifier 2007-NM-223-AD.

(a) Effective Date

    This AD is effective April 20, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all The Boeing Company Model 757-200, -200PF,
-200CB, and -300 series airplanes; and Model 767-200, -300, -300F,
and -400ER series airplanes; certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 29, Hydraulic
Power.

(e) Unsafe Condition

    This AD was prompted by reports indicating that the
counterweights in some hub assemblies of the ram air turbine (RAT)
could be understrength and fracture when the RAT is rotating, and
that some RAT hub assemblies were delivered with balance washer
retention screws that were incorrectly heat-treated, and therefore,
susceptible to fracture and cracking. We are issuing this AD to
prevent an inoperative RAT, which, following a dual engine shutdown
in flight, will cause loss of all hydraulic power to the primary
flight controls, resulting in subsequent loss of control of the
airplane.

(f) Compliance

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

(g) Inspection and Replacement of Parts With a Counterweight Defect

    Prior to the next RAT backdrive test, or within 24 months after
the effective date of this AD, whichever occurs first: Do an
inspection to determine the part number and serial number of the RAT
hub assembly, in accordance with the Accomplishment Instructions of
Boeing Alert Service Bulletin 757-29A0066, Revision 1, dated March
8, 2010 (for Model 757 airplanes); or Boeing Alert Service Bulletin
767-29A0110,

Revision 1, dated March 8, 2010 (for Model 767 airplanes). A review
of airplane maintenance records is acceptable in lieu of this
inspection if the part number and serial number of the RAT hub
assembly can be conclusively determined from that review.
    (1) If the part number or serial number of the RAT hub assembly
is missing, or if the part number and serial number are specified in
paragraphs (g)(1)(i) and (g)(1)(ii) of this AD, and the hub assembly
has not been reworked and re-identified as specified in Hamilton
Sundstrand Service Bulletin 730814-29-12, dated November 30, 2005
(for Model 757 airplanes); or Hamilton Sundstrand Service Bulletin
729548-29-15, dated November 30, 2005 (for Model 767 airplanes):
Prior to the next RAT backdrive test or within 24 months after the
effective date of this AD, whichever occurs first, replace the RAT
or RAT hub assembly with a new, serviceable, or reworked and re-
identified RAT or RAT hub assembly, in accordance with the
Accomplishment Instructions of Boeing Alert Service Bulletin 757-
29A0066, Revision 1, dated March 8, 2010 (for Model 757 airplanes);
or Boeing Alert Service Bulletin 767-29A0110, Revision 1, dated
March 8, 2010 (for Model 767 airplanes); except as provided by
paragraphs (g)(2) and (g)(3) of this AD.
    (i) Model 757-200, -200PF, -200CB, and -300 series airplanes
having part number (P/N) 733785A or 733785B, and serial number (S/N)
0410 through 0413 inclusive, 0415, 0417 through 0430 inclusive,
0432, or 0434.
    (ii) Model 767-200, -300, -300F, and -400ER series airplanes
having P/N 734350A, 734350B, 734350C, or 734350D; and S/N 0666, 0673
through 0684 inclusive, 0686, 0687, or 0689.
    (2) Where Boeing Alert Service Bulletin 757-29A0066, Revision 1,
dated March 8, 2010 (for Model 757 airplanes); or Boeing Alert
Service Bulletin 767-29A0110, Revision 1, dated March 8, 2010 (for
Model 767 airplanes); specifies to contact Hamilton Sundstrand for a
replacement unit, this AD does not require that action.
    (3) Where Boeing Alert Service Bulletin 757-29A0066, Revision 1,
dated March 8, 2010 (for Model 757 airplanes); or Boeing Alert
Service Bulletin 767-29A0110, Revision 1, dated March 8, 2010 (for
Model 767 airplanes); specifies to return all RAT hub assemblies to
Hamilton Sundstrand for rework and test, operators may return the
RAT or RAT hub assembly to Hamilton Sundstrand or to an FAA-approved
repair facility that has the capability to disassemble, repair,
balance, and test the RAT or RAT hub assembly.

(h) Inspection and Replacement of Parts With a Balance Washer Screw
Defect

    Prior to the next RAT backdrive test, or within 24 months after
the effective date of this AD, whichever occurs first: Do an
inspection to determine the part number and serial number on the RAT
hub assembly, in accordance with the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 757-29-0069, dated June
24, 2010 (for Model 757 airplanes); or Boeing Special Attention
Service Bulletin 767-29-0112, dated June 24, 2010 (for Model 767
airplanes). A review of airplane maintenance records is acceptable
in lieu of this inspection if the part number and serial number of
the RAT hub assembly can be conclusively determined from that
review.
    (1) If the part number or serial number of the RAT hub assembly
is missing or if the part number and serial number is listed in
paragraph 1.A., ``Effectivity,'' of Hamilton Sundstrand Service
Bulletin 730814-29-15, dated February 10, 2010 (for Model 757
airplanes); or Hamilton Sundstrand Service Bulletin 729548-29-18,
dated February 10, 2010 (for Model 767 airplanes); and the RAT hub
assembly has not been reworked and re-identified, as specified in
Hamilton Sundstrand Service Bulletin 730814-29-15, dated February
10, 2010 (for Model 757 airplanes); or Hamilton Sundstrand Service
Bulletin 729548-29-18, dated February 10, 2010 (for Model 767
airplanes): Prior to the next RAT backdrive test or within 24 months
after the effective date of this AD, whichever occurs first, do a
general visual inspection of the 12 balance washer screws installed
around the perimeter of the rotor assembly for missing washers and
fractured screws, in accordance with the Accomplishment Instructions
of Hamilton Sundstrand Service Bulletin 730814-29-15, dated February
10, 2010 (for Model 757 airplanes); or Hamilton Sundstrand Service
Bulletin 729548-29-18, dated February 10, 2010 (for Model 767
airplanes).
    (2) If, during any inspection required by paragraph (h)(1) of
this AD, any balance washer is missing or any fractured screw is
found, prior to the next RAT backdrive test or within 24 months
after the effective date of this AD, whichever occurs first: Replace
the RAT or RAT hub assembly with a new, serviceable, or reworked and
re-identified RAT or RAT hub assembly, in accordance with the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 757-29-0069, dated June 24, 2010 (for Model 757 airplanes);
or Boeing Special Attention Service Bulletin 767-29-0112, dated June
24, 2010 (for Model 767 airplanes); except as provided by paragraphs
(h)(2)(i), (h)(2)(ii), and (h)(2)(iii) of this AD.
    (i) Where Boeing Special Attention Service Bulletin 757-29-0069,
dated June 24, 2010 (for Model 757 airplanes); and Boeing Special
Attention Service Bulletin 767-29-0112, dated June 24, 2010 (for
Model 767 airplanes); specify to contact Hamilton Sundstrand for a
replacement unit, this AD does not require that action.
    (ii) Where Boeing Special Attention Service Bulletin 757-29-
0069, dated June 24, 2010 (for Model 757 airplanes); and Boeing
Special Attention Service Bulletin 767-29-0112, dated June 24, 2010
(for Model 767 airplanes); instruct operators to return all RAT or
RAT hub assemblies to Hamilton Sundstrand for rework and test,
operators may return the RAT or RAT hub assembly to Hamilton
Sundstrand or an FAA-approved repair facility that has the
capability to disassemble, repair, balance, and test the RAT or RAT
hub assembly.
    (iii) Where Hamilton Sundstrand Service Bulletin 730814-29-15,
dated February 10, 2010 (for Model 757 airplanes); or Hamilton
Sundstrand Service Bulletin 729548-29-18, dated February 10, 2010
(for Model 767 airplanes); instructs operators to return all of the
removed screws (including the remnants of the fractured screws) to
Hamilton Sundstrand for further investigation, this AD does not
include that requirement.
    (3) If, during any inspection required by paragraph (h)(1) of
this AD, there are no missing balance washers and no fractured
screws: Prior to the next RAT backdrive test or within 24 months
after the effective date of this AD, whichever occurs first, replace
the balance washer screws, one at a time, in accordance with
Hamilton Sundstrand Service Bulletin 730814-29-15, dated February
10, 2010 (for Model 757 airplanes); or Hamilton Sundstrand Service
Bulletin 729548-29-18, dated February 10, 2010 (for Model 767
airplanes).

(i) Parts Installation Limitations

    (1) As of the effective date of this AD, no person may install a
RAT hub assembly having any part number and serial number specified
in paragraphs (i)(1)(i) and (i)(1)(ii) of this AD, on any airplane,
unless it has been reworked and re-identified in accordance with
Hamilton Sundstrand Service Bulletin 730814-29-12, dated November
30, 2005 (for Model 757 airplanes); or Hamilton Sundstrand Service
Bulletin 729548-29-15, dated November 30, 2005 (for Model 767
airplanes).
    (i) Model 757-200, -200PF, -200CB, and -300 series airplanes
having P/N 733785A or 733785B; and S/N 0410 through 0413 inclusive,
0415, 0417 through 0430 inclusive, 0432, or 0434.
    (ii) Model 767-200, -300, -300F, and -400ER series airplanes
having P/N 734350A, 734350B, 734350C, or 734350D, and S/N 0666, 0673
through 0684 inclusive, 0686, 0687, or 0689.
    (2) As of the effective date of this AD, no person may install a
RAT hub assembly having any applicable part number and serial number
specified in paragraphs (i)(2)(i) and (i)(2)(ii) of this AD, on any
airplane, unless it has been inspected, reworked, and re-identified
in accordance with Hamilton Sundstrand Service Bulletin 730814-29-
15, dated February 10, 2010 (for Model 757 airplanes); or Hamilton
Sundstrand Service Bulletin 729548-29-18, dated February 10, 2010
(for Model 767 airplanes).
    (i) Model 757-200, -200PF, -200CB, and -300 series airplanes
having P/N 733785AB Series, and S/N 0107, 0105, 0121, 0151, 0179,
0204, 0282, 0289, 0296, 0315, 0319, 0337, 0390, 0403, 0412, 0421,
0424, 0426, 0429, 0430, 0439, 0445, 0450, 0477, 0503, 0510, 0512,
0584, 0585, 0591, 0599, 0609, 0617, 0624, 0656, 0673, 0685, 0789,
0822, 0841, 0854, 0911, 0912, 0936, 0957, 0961, 0971, 1061, 1064,
1096, 1101, 1102, 1105, 1113, 1117, 1170, 1172, 1173, or X2069.
    (ii) Model 767-200, -300, -300F, and -400ER series airplanes
having P/N 734350 Series, and S/N 0042, 0074, 0170, 0183, 0207,
0311, 0312, 0324, 0336, 0337, 0347, 0367, 0372, 0379, 0381, 0391,
0427, 0431, 0469, 0495, 0500, 0530, 0531, 0533, 0538, 0539, 0550,
0551, 0575, 0584, 0619, 0626, 0666, 0670, 0676, 0690, 0700, 0701,
0734, 0750, 0800, 0801, 0813, 0835, 0836, 0908, 0923,

0958, 0968, 0980, 1009, 1012, 1019, 1046, 1052, 1054, 1102, 1127,
1167, 1264, 1285, 1300, 1317, 1322, 1362, 1372, 1394, 1398, 1436,
1594, 1633, 1634, 1635, 1636, 1637, 1638, 1639, 1640, 1641, 1642,
1643, 1644, 1645, 1646, 1647, 1648, 1649, 1650, 1651, 1652, or
X2063.
    (3) As of the effective date of this AD, no person may install a
balance washer screw having P/N MS24667-14, on the RAT hub assembly
of any airplane unless it can be positively determined from a
records review that the screws did not come from Northeast
Fasteners, lots 24057 and 30533.

(j) No Information Submission

    Although Boeing Alert Service Bulletin 757-29A0066, Revision 1,
dated March 8, 2010 (for Model 757 airplanes); and Boeing Alert
Service Bulletin 767-29A0110, Revision 1, dated March 8, 2010 (for
Model 767 airplanes); specify to submit information to the
manufacturer, this AD does not include that requirement.

(k) Credit for Previous Actions

    This paragraph provides credit for the actions required by
paragraph (g) of this AD, if those actions were performed before the
effective date of this AD using the service information specified in
paragraph (k)(1) or (k)(2) of this AD, as applicable. These
documents are not incorporated by reference in this AD.
    (1) Boeing Alert Service Bulletin 757-29A0066, dated January 2,
2007 (for Model 757-200 and -200PF series airplanes).
    (2) Boeing Alert Service Bulletin 767-29A0110, dated January 2,
2007 (for Model 767-200 and -300 series airplanes).

(l) Alternative Methods of Compliance (AMOCs)

    (1) For Boeing Model 757-200, -200PF, -200CB, and -300 series
airplanes: The Manager, Los Angeles Aircraft Certification Office
(ACO), FAA, has the authority to approve AMOCs for this AD, if
requested using the procedures found in 14 CFR 39.19. In accordance
with 14 CFR 39.19, send your request to your principal inspector or
local Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in paragraph (m)(1) of this AD.
Information may be emailed to<EMAIL_ADDRESS>    (2) For Boeing Model 767-200, -300, -300F, and -400ER series
airplanes: The Manager, Seattle Aircraft Certification Office (ACO),
FAA, has the authority to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19. In accordance with 14
CFR 39.19, send your request to your principal inspector or local
Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in paragraph (m)(2) of this AD.
Information may be emailed to<EMAIL_ADDRESS>    (3) 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.
    (4) For Boeing Model 757-200, -200PF, -200CB, and -300 series
airplanes: An AMOC that provides an acceptable level of safety may
be used for any repair required by this AD if it is approved by the
Boeing Commercial Airplanes Organization Designation Authorization
(ODA) that has been authorized by the Manager, Los Angeles ACO, to
make those findings. For a repair method to be approved, the repair
must meet the certification basis of the airplane and the approval
must specifically refer to this AD.
    (5) For Boeing Model 767-200, -300, -300F, and -400ER series
airplanes: An AMOC that provides an acceptable level of safety may
be used for any repair required by this AD if it is approved by the
Boeing Commercial Airplanes Organization Designation Authorization
(ODA) that has been authorized by the Manager, Seattle ACO, to make
those findings. For a repair method to be approved, the repair must
meet the certification basis of the airplane and the approval must
specifically refer to this AD.

(m) Related Information

    (1) For more information about Boeing Model 757-200, -200PF, -
200CB, and -300 series airplanes in this AD, contact: Jerry Ramos,
Aerospace Engineer, Systems and Equipment Branch, ANM-130L, FAA, Los
Angeles ACO, 3960 Paramount Boulevard, Lakewood, CA 90712-4137;
phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>    (2) For more information about Boeing Model 767-200, -300, -
300F, and -400ER series airplanes in this AD, contact Douglas Tsuji,
Senior Aerospace Engineer, Systems and Equipment Branch, ANM-130S,
FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER><EMAIL_ADDRESS>    (3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(3) and (n)(5) of this AD.

(n) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
    (i) Boeing Alert Service Bulletin 757-29A0066, Revision 1, dated
March 8, 2010.
    (ii) Boeing Alert Service Bulletin 767-29A0110, Revision 1,
dated March 8, 2010.
    (iii) Boeing Special Attention Service Bulletin 757-29-0069,
dated June 24, 2010.
    (iv) Boeing Special Attention Service Bulletin 767-29-0112,
dated June 24, 2010.
    (v) Hamilton Sundstrand Service Bulletin 729548-29-15, dated
November 30, 2005.
    (vi) Hamilton Sundstrand Service Bulletin 729548-29-18, dated
February 10, 2010.
    (vii) Hamilton Sundstrand Service Bulletin 730814-29-12, dated
November 30, 2005.
    (viii) Hamilton Sundstrand Service Bulletin 730814-29-15, dated
February 10, 2010.
    (3) For Boeing service information identified in this AD,
contact Boeing Commercial Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207;
telephone<PHONE_NUMBER>, extension 1; fax<PHONE_NUMBER>; email
<EMAIL_ADDRESS>Internet https://www.myboeingfleet.com.
    (4) For Hamilton Sundstrand service information identified in
this AD, contact Hamilton Sundstrand, Technical Publications, Mail
Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, IL 61125-
7002; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>Internet: http://www.hamiltonsundstrand.com.
    (5) You may view this service information at FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on February 23, 2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-05035 Filed 3-13-15; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 83, Number 208 (Friday, October 26, 2018)]
[Notices]
[Pages 54133-54134]
[FR Doc No: 2018-23379]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-4399-DR; Docket ID FEMA-2018-0001]

Florida; Amendment No. 2 to Notice of a Major Disaster
Declaration

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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

SUMMARY: This notice amends the notice of a major disaster declaration
for the State of Florida (FEMA-4399-DR), dated October 11, 2018, and
related determinations.

DATES: This amendment was issued October 13, 2018.

FOR FURTHER INFORMATION CONTACT: Dean Webster, Office of Response and

Recovery, Federal Emergency Management Agency, 500 C Street SW,
Washington, DC 20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The notice of a major disaster declaration
for the State of Florida is hereby amended to include the following
areas among those areas determined to have been adversely affected by
the event declared a major disaster by the President in his declaration
of October 11, 2018.

    Holmes and Washington Counties for Individual Assistance and
assistance for debris removal and emergency protective measures
(Categories A and B), including direct federal assistance under the
Public Assistance program.

The following Catalog of Federal Domestic Assistance Numbers (CFDA)
are to be used for reporting and drawing funds: 97.030, Community
Disaster Loans; 97.031, Cora Brown Fund; 97.032, Crisis Counseling;
97.033, Disaster Legal Services; 97.034, Disaster Unemployment
Assistance (DUA); 97.046, Fire Management Assistance Grant; 97.048,
Disaster Housing Assistance to Individuals and Households In
Presidentially Declared Disaster Areas; 97.049, Presidentially
Declared Disaster Assistance--Disaster Housing Operations for
Individuals and Households; 97.050 Presidentially Declared Disaster
Assistance to Individuals and Households--Other Needs; 97.036,
Disaster Grants--Public Assistance (Presidentially Declared
Disasters); 97.039, Hazard Mitigation Grant.

Brock Long,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2018-23379 Filed 10-25-18; 8:45 am]
 BILLING CODE 9111-11-P


[Federal Register: April 16, 2010 (Volume 75, Number 73)]
[Notices]
[Page 19985-19986]
[DOCID:fr16ap10-97]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-1894-DR; Docket ID FEMA-2010-0002]

Rhode Island; Amendment No. 3 to Notice of a Major Disaster
Declaration

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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

SUMMARY: This notice amends the notice of a major disaster declaration
for the State of Rhode Island (FEMA-1894-DR), dated March 29, 2010, and
related determinations.

DATES: Effective Date: April 8, 2010.

FOR FURTHER INFORMATION CONTACT: Peggy Miller, Recovery Directorate,
Federal Emergency Management Agency, 500 C Street, SW., Washington, DC
20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The notice of a major disaster declaration
for the State of Rhode Island is hereby amended to include the Public
Assistance program for the following areas among those areas determined
to have been adversely affected by the event declared a major disaster
by the President in his declaration of March 29, 2010.

    Bristol, Kent, Newport, Providence, and Washington Counties for
Public Assistance (already designated for Individual Assistance).
    The following Catalog of Federal Domestic Assistance Numbers
(CFDA) are to be used

for reporting and drawing funds: 97.030, Community Disaster Loans;
97.031, Cora Brown Fund; 97.032, Crisis Counseling; 97.033, Disaster
Legal Services; 97.034, Disaster Unemployment Assistance (DUA);
97.046, Fire Management Assistance Grant; 97.048, Disaster Housing
Assistance to Individuals and Households In Presidentially Declared
Disaster Areas; 97.049, Presidentially Declared Disaster
Assistance--Disaster Housing Operations for Individuals and
Households; 97.050, Presidentially Declared Disaster Assistance to
Individuals and Households--Other Needs; 97.036, Disaster Grants--
Public Assistance (Presidentially Declared Disasters);
    97.039, Hazard Mitigation Grant.

W. Craig Fugate,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2010-8749 Filed 4-15-10; 8:45 am]
BILLING CODE 9111-23-P