[Federal Register Volume 80, Number 53 (Thursday, March 19, 2015)]
[Rules and Regulations]
[Pages 14297-14299]
[FR Doc No: 2015-05715]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0579; Directorate Identifier 2014-SW-020-AD;
Amendment 39-18115; AD 2015-05-05]
RIN 2120-AA64

Airworthiness Directives; Agusta S.p.A. Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: We are superseding Airworthiness Directive (AD) 2014-04-14 for
Agusta S.p.A. (Agusta) Model A109S, AW109SP, A119, and AW119 MKII
helicopters. AD 2014-04-14 required removing certain rod end assemblies
from service because of reports of fractures. This new AD retains the
requirements of AD 2014-04-14 but expands the scope of applicable rod
end assemblies. This AD was prompted by reports of additional fractured
rod end assemblies. We are issuing this AD to prevent failure of a rod
end assembly, which could result in damage to the main rotor assembly
and loss of control of the helicopter.

DATES: This AD is effective April 23, 2015.

ADDRESSES: For service information identified in this AD, contact
AgustaWestland, Product Support Engineering, Via del Gregge, 100, 21015
Lonate Pozzolo (VA) Italy, ATTN: Maurizio D'Angelo; telephone 39-0331-
664757; fax 39-0331-664680; or at http://www.agustawestland.com/technical-bulletins. You may view this referenced service information
at the FAA, Office of the Regional Counsel,

Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas
76137.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the Docket Operations Office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the European Aviation Safety
Agency (EASA) AD, the economic evaluation, any comments received, and
other information. The street address for the Docket Operations Office
(phone:<PHONE_NUMBER>) is U.S. Department of Transportation, Docket
Operations Office, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Robert Grant, Aviation Safety
Engineer, Safety Management Group, FAA, 2601 Meacham Blvd., Fort Worth,
Texas 76137; telephone<PHONE_NUMBER>; email<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to remove AD 2014-04-14, Amendment 39-17773 (79 FR 11699, March
3, 2014) for Agusta Model A109S, AW109SP, A119, and AW119 MKII
helicopters with a main rotor lag damper assembly (lag damper), part
number (P/N) 109-0112-39-103, 109-0112-39-105, 109-0112-05-105, or 109-
0112-05-107, installed with a rod end assembly, P/N M004-01H007-041 or
P/N M004-01H007-045, with a serial number from 84 through 132 or from
4964 through 5011, and add a new AD. The NPRM published in the Federal
Register on August 18, 2014 (79 FR 48698). AD 2014-04-14 required
removing the rod end assemblies from service. AD 2014-04-14 was
prompted by AD No. 2012-0208, dated October 5, 2012, issued by EASA,
which is the Technical Agent for the Member States of the European
Union, to correct an unsafe condition for Agusta Model A109LUH, A109S,
AW109SP, A119, and AW119 MKII helicopters. EASA advises of cases of in-
flight fractures of rod end assembly, P/N M004-01H007-045, installed on
main rotor lag dampers on Model A109LUH and AW109SP helicopters. An
investigation revealed that two batches of rod end assemblies, P/N
M004-01H007-041 and M004-01H007-045, could have cracks, according to
EASA. EASA states that this condition, if not corrected, could lead to
main rotor damage, possibly resulting in loss of control of the
helicopter. The actions of AD 2014-04-14 were intended to prevent such
damage and loss of control of the helicopter.

Actions Since AD 2014-04-14 Was Issued

    Between the time we published the NPRM for AD 2014-04-14 (78 FR
44042, July 23, 2013) and the Final Rule for AD 2014-04-14 (79 FR
11699, March 3, 2014), EASA issued AD No. 2013-0290, dated December 9,
2013. EASA advises in AD No. 2013-0290 that a new case of a fractured
rod end assembly has been reported and that additional batches of rod
end assembly, P/N M004-01H007-041 and P/N M004-01H007-045, as well as
batches of P/N 109-0112-11-101 and P/N 109-0112-22-105 could also have
cracks. EASA expanded the applicability of its AD to include the
additional rod end assemblies.
    We consequently issued the NPRM (79 FR 48698, August 18, 2014) to
amend 14 CFR part 39 to remove AD 2014-04-14 and add a new AD. The NPRM
proposed to retain the requirements of AD 2014-04-14 but expand the
scope of applicable rod end assemblies. The NPRM also proposed to add a
provision requiring compliance with the AD if the rod end assembly is
removed during maintenance before 25 hours time-in-service (TIS).

Comments

    We gave the public the opportunity to participate in developing
this AD, but we received no comments on the NPRM (79 FR 48698, August
18, 2014).

FAA's Determination

    These helicopters have been approved by the aviation authority of
Italy and are approved for operation in the United States. Pursuant to
our bilateral agreement with Italy, EASA, its technical representative,
has notified us of the unsafe condition described in the EASA AD. We
are issuing this AD because we evaluated all information provided by
EASA and determined the unsafe condition exists and is likely to exist
or develop on other helicopters of these same type designs and that air
safety and the public interest require adopting the AD requirements as
proposed, except we have correctly stated the design holder's name as
Agusta S.p.A. instead of AgustaWestland S.p.A. as specified by the
current FAA type certificate. This change is consistent with the intent
of the proposals in the NPRM (79 FR 48698, August 18, 2014) and will
not increase the economic burden on any operator nor increase the scope
of the AD.

Differences Between This AD and the EASA AD

    The EASA AD calls for replacing certain rod end assemblies with
airworthy rod end assemblies within 25 hours TIS, 2 months, or the next
time maintenance of the applicable helicopters involves removing the
rod end assembly. This AD does not have a calendar time requirement.
The EASA AD applies to Agusta Model A109LUH helicopters. This AD does
not apply to Model A109LUH helicopters because that model does not have
a U.S. type certificate.

Related Service Information

    We reviewed AgustaWestland Bollettino Tecnico (BT) No. 109S-49 for
Model A109S helicopters, BT No. 109SP-052 for Model AW109SP
helicopters, and BT No. 119-50 for Model A119 and AW119 MKII
helicopters. All of the BTs are revision A, and dated December 3, 2013.
The BTs specify a one-time inspection of each rod end assembly to
determine its serial number. The BTs then require removal from service
of certain serial-numbered rod end assemblies because fractures had
been reported on rod ends in these batches. According to the BTs, no
one was injured in the helicopters, and no helicopters were damaged
because of these fractures.

Costs of Compliance

    We estimate that this AD affects 91 helicopters of U.S. Registry
and that labor costs average $85 a work-hour. Based on these estimates,
we expect the following costs:
     Replacing a rod end assembly requires 1.5 work-hours for a
labor cost of $128. Parts cost $3,918 for a total cost of $4,046 per
helicopter, $368,186 for the U.S. fleet.
    According to the manufacturer's service information, costs of this
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. We do not control warranty coverage by
manufacturers. Accordingly, we have included all costs in our cost
estimate.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.

    We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979),
    (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 removing Airworthiness Directive (AD)
2014-04-14, Amendment 39-17773 (79 FR 11699, March 3, 2014), and adding
the following new AD:

2015-05-05 Agusta S.p.A.: Amendment 39-18115; Docket No. FAA-2014-
0579; Directorate Identifier 2014-SW-020-AD.

(a) Applicability

    This AD applies to the following helicopters, certificated in
any category:
    (1) Agusta S.p.A. (Agusta) Model A109S and AW109SP helicopters,
with a main rotor lag damper assembly (lag damper), part number (P/
N) 109-0112-39-103 or 109-0112-39-105, installed on rod end
assembly, P/N M004-01H007-041 with a serial number (S/N) 1 through
202; or rod end assembly, P/N M004-01H007-045 with a S/N 1RW through
202RW or 4964 through 5011.
    (2) Agusta Model A119 and AW119 MKII helicopters, with a lag
damper, P/N 109-0112-05-105 or 109-0112-05-107, installed on rod end
assembly, P/N 109-0112-11-101 with a S/N 1 through 78; or rod end
assembly, P/N 109-0112-11-105 with a S/N 1RW through 78RW; or rod
end assembly, P/N M004-01H007-045 with a S/N 1RW through 202RW or
4964 through 5011.

(b) Unsafe Condition

    This AD defines the unsafe condition as a crack in a rod end
assembly, which could result in fracture of the rod end assembly,
damage to the main rotor, and subsequent loss of control of the
helicopter.

(c) Affected ADs

    This AD supersedes AD 2014-04-14, amendment 39-17773 (79 FR
11699, March 3, 2014).

(d) Effective Date

    This AD becomes effective April 23, 2015.

(e) Compliance

    You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.

(f) Required Actions

    (1) Within 25 hours time-in-service or the next time maintenance
of the helicopter involves removing the rod end assembly, whichever
occurs first, remove the rod end assembly from service.
    (2) Do not install a rod end assembly, P/N M004-01H007-041 with
a S/N 1 through 202; P/N M004-01H007-045 with a S/N 1RW through
202RW or 4964 through 5011; P/N 109-0112-11-101 with a S/N 1 through
78; or P/N 109-0112-11-105 with a S/N 1RW through 78RW, on any
helicopter.

(g) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: Robert Grant, Aviation Safety
Engineer, Safety Management Group, FAA, 2601 Meacham Blvd., Fort
Worth, Texas 76137; telephone<PHONE_NUMBER>; email
<EMAIL_ADDRESS>    (2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, we suggest that you
notify your principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office or
certificate holding district office, before operating any aircraft
complying with this AD through an AMOC.

(h) Additional Information

    (1) AgustaWestland S.p.A. Bollettino Tecnico (BT) No. 109S-49,
BT No. 109SP-052, and BT No. 119-50, all Revision A, and all dated
December 3, 2013, which are not incorporated by reference, contain
additional information about the subject of this AD. For service
information identified in this AD, contact AgustaWestland, Product
Support Engineering, Via del Gregge, 100, 21015 Lonate Pozzolo (VA)
Italy, ATTN: Maurizio D'Angelo; telephone 39-0331-664757; fax 39-
0331-664680; or at http://www.agustawestland.com/technical-bulletins. You may review a copy of the service information at the
FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham
Blvd., Room 663, Fort Worth, Texas 76137.
    (2) The subject of this AD is addressed in the European Aviation
Safety Agency (EASA) AD No. 2013-0290, dated December 9, 2013. You
may view the EASA AD on the Internet at http://www.regulations.gov
in Docket No. FAA-2014-0579.

 (i) Subject

    Joint Aircraft Service Component (JASC) Code: 6200, Main Rotor
System.

    Issued in Fort Worth, Texas, on March 4, 2015.
Bruce E. Cain,
Acting Directorate Manager, Rotorcraft Directorate, Aircraft
Certification Service.
[FR Doc. 2015-05715 Filed 3-18-15; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 81, Number 227 (Friday, November 25, 2016)]
[Notices]
[Page 85236]
[FR Doc No: 2016-28357]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Docket ID FEMA-2016-0002]

Final Flood Hazard Determinations

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Final Notice.

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SUMMARY: Flood hazard determinations, which may include additions or
modifications of Base Flood Elevations (BFEs), base flood depths,
Special Flood Hazard Area (SFHA) boundaries or zone designations, or
regulatory floodways on the Flood Insurance Rate Maps (FIRMs) and where
applicable, in the supporting Flood Insurance Study (FIS) reports have
been made final for the communities listed in the table below.
    The FIRM and FIS report are the basis of the floodplain management
measures that a community is required either to adopt or to show
evidence of having in effect in order to qualify or remain qualified
for participation in the Federal Emergency Management Agency's (FEMA's)
National Flood Insurance Program (NFIP). In addition, the FIRM and FIS
report are used by insurance agents and others to calculate appropriate
flood insurance premium rates for buildings and the contents of those
buildings.

DATES: The effective date of October 2, 2015 which has been established
for the FIRM and, where applicable, the supporting FIS report showing
the new or modified flood hazard information for each community.

ADDRESSES: The FIRM, and if applicable, the FIS report containing the
final flood hazard information for each community is available for
inspection at the respective Community Map Repository address listed in
the tables below and will be available online through the FEMA Map
Service Center at www.msc.fema.gov by the effective date indicated
above.

FOR FURTHER INFORMATION CONTACT: Rick Sacbibit, Chief, Engineering
Services Branch, Federal Insurance and Mitigation Administration, FEMA,
500 C Street SW., Washington, DC 20472,<PHONE_NUMBER>, or (email)
<EMAIL_ADDRESS>or visit the FEMA Map Information
eXchange (FMIX) online at www.floodmaps.fema.gov/fhm/fmx_main.html.

SUPPLEMENTARY INFORMATION: The Federal Emergency Management Agency
(FEMA) makes the final determinations listed below for the new or
modified flood hazard information for each community listed.
Notification of these changes has been published in newspapers of local
circulation and 90 days have elapsed since that publication. The Deputy
Associate Administrator for Mitigation has resolved any appeals
resulting from this notification.
    This final notice is issued in accordance with section 110 of the
Flood Disaster Protection Act of 1973, 42 U.S.C. 4104, and 44 CFR part
67. FEMA has developed criteria for floodplain management in floodprone
areas in accordance with 44 CFR part 60.
    Interested lessees and owners of real property are encouraged to
review the new or revised FIRM and FIS report available at the address
cited below for each community or online through the FEMA Map Service
Center at www.msc.fema.gov.
    The flood hazard determinations are made final in the watersheds
and/or communities listed in the table below.

(Catalog of Federal Domestic Assistance No. 97.022, ``Flood
Insurance.'')

    Dated: October 31, 2016.
Roy E. Wright,
Deputy Associate Administrator for Insurance and Mitigation, Department
of Homeland Security, Federal Emergency Management Agency.

    I. Non-watershed-based studies:

------------------------------------------------------------------------
                                             Community map repository
               Community                             address
------------------------------------------------------------------------
            Sonoma County, California and Incorporated Areas

                         Docket No.: FEMA-B-1440
------------------------------------------------------------------------
City of Petaluma.......................  Community Development
                                          Department, 11 English Street,
                                          Petaluma, CA 94952.
Unincorporated Areas of Sonoma County..  Permit and Resource Management,
                                          2550 Ventura Avenue, Santa
                                          Rosa, CA 95403.
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[FR Doc. 2016-28357 Filed 11-23-16; 8:45 am]
 BILLING CODE 9110-12-P


[Federal Register: January 24, 2011 (Volume 76, Number 15)]
[Rules and Regulations]
[Page 4064-4066]
[DOCID:fr24ja11-5]

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DEPARTMENT OF TRANSPORTATION

14 CFR Part 97

[Docket No. 30764; Amdt. No. 3409]

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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

DATES: This rule is effective January 24, 2011. The compliance date for
each SIAP, associated Takeoff Minimums, and ODP is specified in the
amendatory provisions.
    The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of January 24, 2011.

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

FOR FURTHER INFORMATION CONTACT: Harry J. Hodges, Flight Procedure
Standards Branch (AFS-420), Flight Technologies and Programs 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 rule amends Title 14, Code of Federal
Regulations, Part 97 (14 CFR part 97) by amending the referenced SIAPs.
The complete regulatory description of each SIAP is listed on the
appropriate FAA Form 8260, as modified by the National Flight Data
Center (FDC)/Permanent Notice to Airmen (P-NOTAM), and is incorporated
by reference in the amendment under 5 U.S.C. 552(a), 1 CFR part 51, and
Sec.  97.20 of Title 14 of the Code of Federal Regulations.
    The large number of SIAPs, their complex nature, and the need for a
special format make their verbatim publication in the Federal Register
expensive and impractical. Further, airmen do not use the regulatory
text of the SIAPs, but refer to their graphic depiction on charts
printed by publishers of aeronautical materials. Thus, the advantages
of incorporation by reference are realized and publication of the
complete description of each SIAP contained in FAA form documents is
unnecessary. This amendment provides the affected CFR sections and
specifies the types of SIAP and the corresponding effective dates. This
amendment also identifies the airport and its location, the procedure
and the amendment number.

The Rule

    This amendment to 14 CFR part 97 is effective upon publication of
each separate SIAP as amended in the transmittal. For safety and
timeliness of change considerations, this amendment incorporates only
specific changes contained for each SIAP as modified by FDC/P-NOTAMs.
    The SIAPs, as modified by FDC P-NOTAM, and contained in this
amendment are based on the criteria contained in the U.S. Standard for
Terminal Instrument Procedures (TERPS). In developing these changes to
SIAPs, the TERPS criteria were applied only to specific conditions
existing at the affected airports. All SIAP amendments in this rule
have been previously issued by the FAA in a FDC NOTAM as an emergency
action of immediate flight safety relating directly to published
aeronautical charts. The circumstances which created the need for all
these SIAP amendments requires making them effective in less than 30
days.
    Because of the close and immediate relationship between these SIAPs
and safety in air commerce, I find that notice and public procedure
before adopting these SIAPs are impracticable and contrary to the
public interest and, where applicable, that good cause exists for
making these SIAPs effective in less than 30 days.

Conclusion

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

List of Subjects in 14 CFR Part 97

    Air traffic control, Airports, Incorporation by reference, and
Navigation (Air).

    Issued in Washington, DC, on January 7, 2011.
John McGraw,
Deputy Director, Flight Standards Service.

Adoption of the Amendment

    Accordingly, pursuant to the authority delegated to me, Title 14,
Code of Federal Regulations, Part 97, 14 CFR part 97, is amended by
amending Standard Instrument Approach Procedures, effective at 0901 UTC
on the dates specified, as follows:

PART 97--STANDARD INSTRUMENT APPROACH PROCEDURES

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

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

0
2. Part 97 is amended to read as follows:
    By amending: Sec.  97.23 VOR, VOR/DME, VOR or TACAN, and VOR/DME or
TACAN; Sec.  97.25 LOC, LOC/DME, LDA, LDA/DME, SDF, SDF/DME; Sec.
97.27 NDB, NDB/DME; Sec.  97.29 ILS, ILS/DME, MLS, MLS/DME, MLS/RNAV;
Sec.  97.31 RADAR SIAPs; Sec.  97.33 RNAV SIAPs; and Sec.  97.35 COPTER
SIAPs, identified as follows:

* * * Effective Upon Publication

--------------------------------------------------------------------------------------------------------------------------------------------------------
      AIRAC date            State               City               Airport          FDC No.      FDC date                      Subject
--------------------------------------------------------------------------------------------------------------------------------------------------------
10-Feb-11............  OH               Ashland............  Ashland County.....       0/0448      12/6/10  NDB RWY 19, Amdt 11.
10-Feb-11............  OH               Ashland............  Ashland County.....       0/0449      12/6/10  VOR A, Amdt 9.
10-Feb-11............  OH               Ashland............  Ashland County.....       0/0450      12/6/10  RNAV (GPS) RWY 19, Orig.
10-Feb-11............  IL               Kewanee............  Kewanee Muni.......       0/1242     12/17/10  RNAV (GPS) RWY 27, Orig.
10-Feb-11............  IL               Kewanee............  Kewanee Muni.......       0/1243     12/17/10  RNAV (GPS) RWY 19, Orig.
10-Feb-11............  IL               Kewanee............  Kewanee Muni.......       0/1245     12/17/10  RNAV (GPS) RWY 9, Orig.
10-Feb-11............  LA               Natchitoches.......  Natchitoches Rgnl..       0/1309     12/13/10  LOC RWY 35, Amdt 3E.
10-Feb-11............  TX               Weslaco............  Mid Valley.........       0/1310     12/13/10  GPS RWY 13, Orig.
10-Feb-11............  NM               Farmington.........  Four Corners Rgnl..       0/1316     12/13/10  ILS OR LOC RWY 25, Amdt 7C.
10-Feb-11............  LA               Lake Charles.......  Chennault Intl.....       0/1703     12/13/10  RNAV (GPS) RWY 15, Orig.
10-Feb-11............  MT               Lewistown..........  Lewistown Muni.....       0/1707     12/18/10  Takeoff Minimums and (Obstacle) DP, Amdt 3.
10-Feb-11............  LA               Lake Charles.......  Chennault Intl.....       0/1731     12/13/10  ILS OR LOC RWY 15, Amdt 5.
10-Feb-11............  LA               Bastrop............  Morehouse Memorial.       0/1929     12/14/10  RNAV (GPS) RWY 16, Amdt 1.
10-Feb-11............  LA               Bastrop............  Morehouse Memorial.       0/1930     12/14/10  RNAV (GPS) RWY 34, Orig.
10-Feb-11............  LA               Bastrop............  Morehouse Memorial.       0/1931     12/14/10  NDB RWY 34, Amdt 6.
10-Feb-11............  LA               Bastrop............  Morehouse Memorial.       0/1932     12/14/10  VOR/DME A, Amdt 9.
10-Feb-11............  OH               Toledo.............  Toledo Express.....       0/2155     12/20/10  RNAV (GPS) RWY 7, Amdt 1.
10-Feb-11............  PA               Quakertown.........  Quakertown.........       0/2366     12/27/10  NDB RWY 29, Amdt 10.
10-Feb-11............  PA               Quakertown.........  Quakertown.........       0/2367     12/27/10  RNAV (GPS) RWY 29, Orig.
10-Feb-11............  MO               St Louis...........  Lambert-St Louis          0/2654     12/23/10  ILS PRM RWY 11 (Sim. Close Parallel), Orig-
                                                              Intl.                                          B; ILS PRM RWY 11 (CAT II) (Sim Close
                                                                                Parallel), Orig-B; ILS PRM RWY 11 (CAT III)
                                                                                (Sim Close Parallel), Orig-B.
10-Feb-11............  MO               St Louis...........  Lambert-St Louis          0/2655     12/23/10  ILS PRM RWY 12L (Sim. Close Parallel), Amdt
                                                              Intl.                                          1; ILS PRM RWY 12L (CAT II) (Sim Close
                                                                                Parallel), Amdt 1; ILS PRM RWY 12L (CAT
                                                                                III) (Sim Close Parallel), Amdt 1.
10-Feb-11............  MO               St Louis...........  Lambert-St Louis          0/2656     12/23/10  ILS PRM RWY 29 (Sim. Close Parallel), Amdt
                                                              Intl.                                          1A.
10-Feb-11............  MO               St Louis...........  Lambert-St Louis          0/2657     12/23/10  ILS PRM RWY 30R (Sim. Close Parallel), Amdt
                                                              Intl.                                          1A; ILS PRM RWY 30R (CAT II) (Sim Close
                                                                                Parallel), Amdt 1A; ILS PRM RWY 30R (CAT
                                                                                III) (Sim Close Parallel), Amdt 1A.
10-Feb-11............  MO               St Louis...........  Lambert-St Louis          0/2660     12/23/10  LDA PRM RWY 30L (Sim. Close Parallel), Amdt
                                                              Intl.                                          1A.
10-Feb-11............  MI               Detroit............  Detroit                   0/2668     12/23/10  ILS PRM RWY 3R (Sim. Close Parallel), Orig;
                                                              Metropolitan Wayne                             ILS PRM RWY 3R (CAT II) (Sim. Close
                                                              County.                                        Parallel), Orig; ILS PRM RWY 3R (CAT III)
                                                                                (Sim. Close Parallel), Orig.
10-Feb-11............  MI               Detroit............  Detroit                   0/2669     12/23/10  ILS PRM RWY 4R (Sim. Close Parallel), Orig;
                                                              Metropolitan Wayne                             ILS PRM RWY 4R (CAT II) (Sim. Close
                                                              County.                                        Parallel), Orig; ILS PRM RWY 4R (CAT III)
                                                                                (Sim. Close Parallel), Orig.
10-Feb-11............  MI               Detroit............  Detroit                   0/2670     12/23/10  ILS Y PRM RWY 4L (Sim. Close Parallel), Orig-
                                                              Metropolitan Wayne                             A.
                                                              County.
10-Feb-11............  MI               Detroit............  Detroit                   0/2671     12/23/10  ILS Y PRM RWY 22R (Sim. Close Parallel),
                                                              Metropolitan Wayne                             Orig-A.
                                                              County.
10-Feb-11............  NE               Hebron.............  Hebron Muni........       0/2696     12/20/10  GPS RWY 12, Orig.
10-Feb-11............  NE               Hebron.............  Hebron Muni........       0/2697     12/20/10  NDB RWY 12, Amdt 4.
10-Feb-11............  NE               Hebron.............  Hebron Muni........       0/2698     12/20/10  GPS RWY 30, Orig.
10-Feb-11............  OH               Cleveland..........  Cleveland-Hopkins         0/2702     12/23/10  ILS PRM RWY 24R (Sim. Close Parallel), Orig-
                                                              Intl.                                          B.

10-Feb-11............  OH               Cleveland..........  Cleveland-Hopkins         0/2704     12/23/10  LDA PRM RWY 6R (Sim. Close Parallel), Amdt
                                                              Intl.                                          1B.
10-Feb-11............  OH               Cleveland..........  Cleveland-Hopkins         0/2707     12/23/10  ILS PRM RWY 6L (Sim. Close Parallel), Orig-
                                                              Intl.                                          C.
10-Feb-11............  OH               Cleveland..........  Cleveland-Hopkins         0/2708     12/23/10  LDA PRM RWY 24L (Sim. Close Parallel), Orig-
                                                              Intl.                                          B.
10-Feb-11............  MI               Detroit............  Detroit                   0/2710     12/23/10  ILS PRM RWY 22L (Sim. Close Parallel), Orig.
                                                              Metropolitan Wayne
                                                              County.
10-Feb-11............  MI               Detroit............  Detroit                   0/2711     12/23/10  ILS PRM RWY 21L (Sim. Close Parallel), Orig.
                                                              Metropolitan Wayne
                                                              County.
10-Feb-11............  IA               Sioux City.........  Sioux Gateway/Col         0/2714     12/23/10  VOR OR TACAN RWY 31, Amdt 26.
                                                              Bud Day Field.
10-Feb-11............  IA               Sioux City.........  Sioux Gateway/Col         0/2715     12/23/10  ILS OR LOC RWY 13, Amdt 1F.
                                                              Bud Day Field.
10-Feb-11............  PA               Philadelphia.......  Philadelphia Intl..       0/3257     12/28/10  ILS PRM RWY 27L (Sim. Close Parallel), Amdt
                                                                                3.
10-Feb-11............  PA               Philadelphia.......  Philadelphia Intl..       0/3258     12/28/10  ILS PRM RWY 26 (Sim. Close Parallel), Amdt
                                                                                3.
10-Feb-11............  TX               Pampa..............  Perry Lefors Field.       0/4249      12/6/10  GPS RWY 17, Orig-A.
10-Feb-11............  IL               Champaign/Urbana...  University of             0/7104     12/20/10  LOC/DME BC RWY 14L, Amdt 8.
                                                              Illinois-Willard.
10-Feb-11............  LA               Lake Charles.......  Lake Charles Rgnl..       0/9701     12/13/10  RADAR-1, Amdt 5A.
10-Feb-11............  LA               Lake Charles.......  Lake Charles Rgnl..       0/9702     12/13/10  LOC BC RWY 33, Amdt 19A.
10-Feb-11............  LA               Lake Charles.......  Lake Charles Rgnl..       0/9703     12/13/10  RNAV (GPS) RWY 33, Amdt 1B.
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[FR Doc. 2011-816 Filed 1-21-11; 8:45 am]
BILLING CODE 4910-13-P