[Federal Register Volume 79, Number 194 (Tuesday, October 7, 2014)]
[Proposed Rules]
[Pages 60389-60391]
[FR Doc No: 2014-23880]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0770; Directorate Identifier 2014-CE-024-AD]
RIN 2120-AA64

Airworthiness Directives; PILATUS Aircraft Ltd. Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
PILATUS Aircraft Ltd. Model PC-7 airplanes. This proposed AD results
from mandatory continuing airworthiness information (MCAI) originated
by an aviation authority of another country to identify and correct an
unsafe condition on an aviation product. The MCAI describes the unsafe
condition as possible cracking from stress corrosion on various parts
of the aircraft structure made of aluminum alloy AA2024-T351. We are
issuing this proposed AD to require actions to address the unsafe
condition on these products.

DATES: We must receive comments on this proposed AD by November 21,
2014.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact
PILATUS AIRCRAFT LTD., Customer Technical Support (MCC), P.O. Box 992,
CH-6371 Stans, Switzerland; phone: +41 (0)41 619 67 74; fax: +41 (0)41
619 67 73; email<EMAIL_ADDRESS>internet: http://
www.pilatus-aircraft.com. You may review this referenced service
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas
City, Missouri 64106. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0770; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this proposed AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone<PHONE_NUMBER>) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2014-0770;
Directorate Identifier 2014-CE-024-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

    The Federal Office of Civil Aviation (FOCA), which is the aviation
authority for Switzerland, has issued AD HB-2014-001, dated July 25,
2014 (referred to after this as ``the MCAI''), to correct an unsafe
condition for PILATUS Aircraft Ltd. Model PC-7 airplanes and was based
on mandatory continuing airworthiness information originated by an
aviation authority of another country. The MCAI states:

    This Airworthiness Directive (AD) is prompted due to the
possibility of cracks in

some critical parts. It is possible that stress corrosion cracks may
occur on various parts of the aircraft structure initially made of
aluminium alloy AA2024-T351 which is susceptible to Stress Corrosion
Cracking (SCC). Later in production, the material specification was
changed to aluminium alloy AA2124-T851 to decrease the risk of
stress corrosion. The Part Number (P/N) of the affected structural
parts are not always changed when the new material was introduced.
    Such a condition, if left uncorrected, could lead to failure of
critical parts on the aircraft structure and will prejudice the
structural integrity of the aircraft.
    In order to correct and control the situation, this AD requires
a one-time check to identify the material specification and inspect
the affected areas of the airframe that are made of aluminium alloy
AA2024-T351. Any structural parts of the aircraft structure found to
be cracked must be reported to Pilatus prior to further flight.

    The MCAI also requires replacement of the elevator center control-
rod, P/N <IP_ADDRESS>1 or <IP_ADDRESS>5; and shackle, P/N
<IP_ADDRESS>. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0770.

Relevant Service Information

    PILATUS Aircraft Ltd. has issued PILATUS PC-7 Service Bulletin No:
51-001, Revision No. 1, dated August 26, 2014. The actions described in
this service information are intended to correct the unsafe condition
identified in the MCAI. PILATUS PC-7 Service Bulletin No: 51-001 was
revised to Revision No. 1 after the issuance of the MCAI.

FAA's Determination and Requirements of the Proposed AD

    This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.

Costs of Compliance

    We estimate that this proposed AD will affect 10 products of U.S.
registry. We also estimate that it would take about 30 work-hours per
product to comply with the basic requirements of this proposed AD. The
average labor rate is $85 per work-hour. Required parts would cost
about $4,700 per product.
    Based on these figures, we estimate the cost of the proposed AD on
U.S. operators to be $72,500, or $7,250 per product.
    In addition, we estimate that any necessary follow-on actions would
take about 14 work-hours and require parts costing $10,000, for a cost
of $11,190 per product. We have no way of determining the number of
products that may need these actions.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
    We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed
regulation:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

PILATUS Aircraft Ltd.: Docket No. FAA-2014-0770; Directorate
Identifier 2014-CE-024-AD.

(a) Comments Due Date

    We must receive comments by November 21, 2014.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to PILATUS Aircraft Ltd. Model PC-7 airplanes,
manufacturer serial numbers (MSN) 101 through MSN 618, certificated
in any category.

(d) Subject

    Air Transport Association of America (ATA) Code 51: Standard
Practices/Structures.

(e) Reason

    This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as possible
cracking from stress corrosion on various parts of the aircraft
structure made of aluminum alloy AA2024-T351. We are issuing this
proposed AD to detect and correct stress corrosion cracks that may
occur on various parts of the airplane structure initially made of
aluminum alloy AA2024-T351, which is susceptible to stress corrosion
cracking (SCC). Such a condition, if left uncorrected, could lead to
failure of critical parts on the airplane structure and weaken the
structural integrity of the aircraft.

(f) Actions and Compliance

    Unless already done, within the next 12 months after the
effective date of this AD, perform a one-time conductivity test of
items 6 through 9 and 11 through 13 as listed in paragraph 1.A.(2)
of PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1, dated
August 26, 2014, to check the material of the parts--determine
whether they are made of aluminum alloy AA2124-T851 or aluminum
alloy AA2024-T351. Do not install any item

unless it has been inspected following the applicable paragraph of
PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1, dated
August 26, 2014.
    (1) For airplanes with any parts made of aluminum alloy AA2124-
T851: Within 12 months after the effective date of this AD, make an
entry in the aircraft logbook as required by paragraph 3.D.(3) of
PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1, dated
August 26, 2014. The only other actions of this AD that apply to
airplanes with all parts made of aluminum alloy AA2124-T851 are the
actions in paragraphs (f)(3), (f)(4), and (f)(5) of this AD.
    (2) For airplanes with any parts made of aluminum alloy AA2024-
T351: Within 12 months after the effective date of this AD, do the
actions in paragraphs (f)(2)(i) through (f)(2)(iii) as applicable,
including all subparagraphs:
    (i) For items 7 through 9 and 11 through 13 as listed in
paragraph 1.A.(2) of PILATUS PC-7 Service Bulletin No: 51-001,
Revision No. 1, dated August 26, 2014, within 12 months after the
effective date of this AD, do a one-time inspection for cracks. If
any cracks are found as a result of the inspection, before further
flight, you must contact PILATUS Aircraft Ltd. to obtain FAA-
approved repair instructions approved specifically for compliance
with this AD and incorporate those instructions. Use the contact
information found in paragraph (h) of this AD.
    (ii) For item 6 as listed in paragraph 1.A.(2) of PILATUS PC-7
Service Bulletin No: 51-001, Revision No. 1, dated August 26, 2014,
within 12 months after the effective date of this AD, replace with a
part made of aluminum alloy AA2124-T851.
    (iii) For Items 1, 2, 4, 5, and 10 as listed in paragraph
1.A.(2) of PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1,
dated August 26, 2014, within 12 months after the effective date of
this AD, do the following actions in paragraphs (f)(2)(iii)(A) and
(f)(2)(iii)(B), as applicable.
    (A) For items 1, 2, 4, and 10 as listed in paragraph 1.A.(2) of
PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1, dated
August 26, 2014, do a one-time inspection for cracks. If any cracks
are found, before further flight, you must contact PILATUS Aircraft
Ltd. to obtain FAA-approved repair instructions approved
specifically for compliance with this AD and incorporate those
instructions. Use the contact information found in paragraph (h) of
this AD.
    (B) For item 5 as listed in paragraph 1.A.(2) of PILATUS PC-7
Service Bulletin No: 51-001, Revision No. 1, dated August 26, 2014,
replace with a part made of aluminum alloy AA2124-T851.
    (3) For all airplanes: For item 3 as listed in paragraph 1.A.(2)
of PILATUS PC-7 Service Bulletin No: 51-001, Revision No. 1, dated
August 26, 2014, within 12 months after the effective date of this
AD, replace with a part made of aluminum alloy AA2124-T851. You must
replace the elevator center control-rods (item 3 as listed in
paragraph 1.A.(2) of PILATUS PC-7 Service Bulletin No: 51-001,
Revision No. 1, dated August 26, 2014) because it is difficult to
inspect them for cracks.
    (4) For all airplanes: As of 12 months after the effective date
of this AD, do not install the parts listed in items 1 and 2, 4, and
7 through 13 of paragraph 1.A.(2) of PILATUS PC-7 Service Bulletin
No: 51-001, Revision No. 1, dated August 26, 2014, that are made of
aluminum alloy AA2024-T351 unless they have been inspected and found
free of cracks.
    (5) For all airplanes: As of 12 months after the effective date
of this AD, do not install the parts listed in items 3, 5, and 6 of
paragraph 1.A.(2) of PILATUS PC-7 Service Bulletin No: 51-001,
Revision No. 1, dated August 26, 2014, that are made of aluminum
alloy AA2024-T351.

(g) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Doug Rudolph, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>Before using any approved AMOC on any airplane
to which the AMOC applies, notify your appropriate principal
inspector (PI) in the FAA Flight Standards District Office (FSDO),
or lacking a PI, your local FSDO.
    (2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in
this AD, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information
subject to the requirements of the Paperwork Reduction Act unless
that collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 5 minutes per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.

(h) Related Information

    Refer to Federal Office of Civil Aviation (FOCA) AD HB-2014-001,
dated July 25, 2014, for related information. You may examine the
MCAI on the Internet at http://www.regulations.gov by searching for
and locating Docket No. FAA-2014-0770. For service information
related to this AD, contact PILATUS AIRCRAFT LTD., Customer
Technical Support (MCC), P.O. Box 992, CH-6371 Stans, Switzerland;
phone: +41 (0)41 619 67 74; fax: +41 (0)41 619 67 73; email:
<EMAIL_ADDRESS>Internet: http://www.pilatus-
aircraft.com. You may review this referenced service information at
the FAA, Small Airplane Directorate, 901 Locust, Kansas City,
Missouri 64106. For information on the availability of this material
at the FAA, call<PHONE_NUMBER>.

    Issued in Kansas City, Missouri, on September 30, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-23880 Filed 10-6-14; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 77, Number 85 (Wednesday, May 2, 2012)]
[Notices]
[Pages 26067-26068]
[FR Doc No: 2012-10586]

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DEPARTMENT OF TRANSPORTATION

Intelligent Transportation Systems Program Advisory Committee;
Notice of Meeting

AGENCY: ITS Joint Program Office, Research and Innovative Technology
Administration, U.S. Department of Transportation.

ACTION: Notice.

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    The Intelligent Transportation Systems (ITS) Program Advisory
Committee (ITS PAC) will hold a meeting on May 24, 2012, from 8:00 a.m.
to 4:00 p.m. (EDT), in conference room 7 of the U.S.
Department of Transportation (U.S. DOT) Conference Center on the lobby
level of the U.S. DOT West Building, 1200 New Jersey Avenue SE,
Washington, DC 20590.
    The ITS PAC, established under Section 5305 of Public Law 109-59,
Safe, Accountable, Flexible, Efficient Transportation Equity Act: A
Legacy for Users, August 10, 2005, and re-chartered on January 23,
2012, was created to advise the Secretary of Transportation on all
matters relating to the study, development, and implementation of
intelligent transportation systems. Through its sponsor, the ITS Joint
Program Office, the ITS PAC makes recommendations to the Secretary
regarding ITS Program needs, objectives,

plans, approaches, content, and progress.
    The following is a summary of the meeting tentative agenda: (1)
Welcome by RITA Acting Administrator; (2) Meeting purpose and agenda
review; (3) Introduction of committee members and background; (4)
Committee expectations and individual goals; (5) Briefings on various
aspects of Connected Vehicle research; (6) Network security discussion;
(7) Key ITS Research Program Issues; and (8) Timeline for future
committee work.
    The meeting will be open to the public, but limited space will be
available on a first-come, first-served basis. Since access to the U.S.
DOT building is controlled, non-committee members who plan to attend
the meeting must notify Mr. Stephen Glasscock, the Committee Designated
Federal Official, at<PHONE_NUMBER> not later than May 17, 2012.
Individuals attending the meeting must report to the 1200 New Jersey
Avenue entrance of the U.S. DOT building for admission. Members of the
public who wish to present oral statements at the meeting must request
approval from Mr. Glasscock not later than May 17, 2012.
    Questions about the agenda or written comments may be submitted by
U.S. Mail to: U.S. Department of Transportation, Research and
Innovative Technology Administration, ITS Joint Program Office,
Attention: Stephen Glasscock, 1200 New Jersey Avenue SE., HOIT,
Washington, DC 20590 or faxed to<PHONE_NUMBER>. The ITS Joint Program
Office requests that written comments be submitted prior to the
meeting.
    Notice of this meeting is provided in accordance with the Federal
Advisory Committee Act and the General Services Administration
regulations (41 CFR part 102-3) covering management of Federal advisory
committees.

    Dated: Issued in Washington, DC, on the 26th day of April 2012.
John Augustine,
Managing Director, ITS Joint Program Office.
[FR Doc. 2012-10586 Filed 5-1-12; 8:45 am]
BILLING CODE 4910-P


[Federal Register Volume 81, Number 61 (Wednesday, March 30, 2016)]
[Rules and Regulations]
[Pages 17602-17603]
[FR Doc No: 2016-07077]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Docket No. FAA-2015-4532; Airspace Docket No. 15-AEA-10]

Amendment of Class D Airspace and Class E Airspace for the
Following New York Towns; Ithaca, NY; Poughkeepsie, NY

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; delay of effective date, correction.

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SUMMARY: This action changes the effective date of a final rule
published in the Federal Register of February 4, 2016, amending Class E
Airspace designated as an extension at Ithaca Tompkins Regional
Airport, Ithaca, NY; and the Kingston VORTAC, Poughkeepsie, NY. This
correction updates the geographic coordinates of each navigation aid
and Ithaca Tompkins Regional Airport (formerly Tompkins County
Airport), under Class D airspace and Class E surface area airspace to
coincide with the FAA's aeronautical database. Also, Dutchess County
Airport is added to the Kingston VORTAC, Poughkeepsie, NY, designation
in Class E airspace designated as an extension. The Kingston VORTAC
reference is removed from the Class D airspace designation. This action
also adds Class D airspace to the title of this rulemaking.

DATES: This correction is effective 0901 UTC, May 26, 2016, and the
effective date of the rule amending 14 CFR part 71, published on
February 4, 2016 (81 FR 5902), is delayed to 0901 UTC May 26, 2016. The
Director of the Federal Register approves this incorporation by
reference action under Title 1, Code of Federal Regulations, part 51,
subject to the annual revision of FAA Order 7400.9 and publication of
conforming amendments.

FOR FURTHER INFORMATION CONTACT: John Fornito, Operations Support
Group, Eastern Service Center, Federal Aviation Administration, P.O.
Box 20636, Atlanta, Georgia 30320; telephone<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Authority for This Rulemaking

History

    The Federal Register published a final rule amending Class E
Airspace Designated as an Extension at Ithaca Tompkins Regional
Airport, Ithaca, NY, (formerly Tompkins County Airport), and the
Kingston VORTAC, Poughkeepsie, NY (81 FR 5902, February 4, 2016) Docket
No. FAA-2015-4532. Further review revealed the geographic coordinates
for the airport and navaids needed to be amended in Class D airspace
and Class E surface area airspace. It is also noted that the Kingston
VORTAC is erroneously listed in Class D airspace for Poughkeepsie, NY,
and is removed. Also, Class D Airspace is added to the title.
    Class D and Class E airspace designations are published in
paragraphs 5000, 6002, and 6004, respectively, of FAA Order 7400.9Z
dated August 6, 2015, and effective September 15, 2015, which is
incorporated by reference in 14 CFR part 71.1. The Class D and Class E
airspace designations listed in this document will be published
subsequently in the Order. These are administrative corrections and do
not affect the controlled airspace boundaries or operating requirements
supporting operations in the Ithaca and Poughkeepsie, NY areas.

Availability and Summary of Documents for Incorporation by Reference

    This document amends FAA Order 7400.9Z, Airspace Designations and
Reporting Points, dated August 6, 2015, and effective September 15,
2015. FAA Order 7400.9Z lists Class A, B, C, D, and E airspace areas,
air traffic service routes, and reporting points.

Correction to Final Rule

    Accordingly, pursuant to the authority delegated to me, in the
Federal Register of February 4, 2016 (81 FR 5902) FR Doc. FAA-2016-
02040, Amendment of Class E Airspace for the following NY Towns;
Ithaca, NY; Poughkeepsie, NY, is corrected as follows:
    On page 5902, column 2, beginning on line 6, remove the following
text: ``Amendment of Class E Airspace for the following New York Towns;
Ithaca, NY; Poughkeepsie, NY'' and add in its place ``Amendment of
Class D and E Airspace for the following New York Towns; Ithaca, NY,
Poughkeepsie, NY
    On page 5903, column 2, after line 23, add the following text:

Paragraph 5000 Class D Airspace.

* * * * *

AEA NY D Ithaca, NY [Corrected]

Ithaca Tompkins Regional Airport, Ithaca, NY
    (Lat. 42[deg]29'29'' N., long. 76[deg]27'31'' W.)

    That airspace extending upward from the surface to and including
3,600 feet MSL within a 4-mile radius of Ithaca Tompkins Regional
Airport. This Class D airspace area is effective during specific
dates and times established in advance by a Notice to Airmen. The
effective date and time will thereafter be published continuously in
the Airport/Facility Directory.

AEA NY D Poughkeepsie, NY [Corrected]

Dutchess County Airport, Poughkeepsie, NY
    (Lat. 41[deg]37'36'' N., long. 73[deg]53'03'' W.)

    That airspace extending upward from the surface to and including
2,700 feet MSL within a 4-mile radius of Dutchess County Airport.
This Class D airspace area is effective during the specific dates
and times established in advance by a Notice to Airmen. The
effective date and time will thereafter be continuously published in
the Airport/Facility Directory.

Paragraph 6002 Class E Surface Area Airspace

* * * * *

AEA NY E2 Ithaca, NY [Corrected]

Ithaca Tompkins Regional Airport, Ithaca, NY
    (Lat. 42[deg]29'29'' N., long. 76[deg]27'31'' W.)
Ithaca VOR/DME
    (Lat. 42[deg]29'42'' N., long. 76[deg]27'35'' W.)

    Within a 4-mile radius of Ithaca Tompkins Regional Airport and
that airspace extending upward from the surface from the 4-mile
radius of the airport to the 5.7-mile radius of the airport
clockwise from the 329[deg] bearing to the 081[deg] bearing from the
airport; that airspace from the 4-mile radius of the airport to the
8.7-mile radius of the airport extending clockwise from the 081[deg]
bearing to the 137[deg] bearing from the airport; that airspace from
the 4-mile radius of the airport to the 6.6-mile radius of the
airport extending clockwise from the 137[deg] bearing to the
170[deg] bearing from the airport; that airspace from the 4-mile
radius to the 5.7-mile radius of the airport extending clockwise
from the 170[deg] bearing to the 196[deg] bearing from the airport,
and that airspace within 2.7 miles each side of the Ithaca VOR/DME
305[deg] radial extending from the 4-mile radius of the airport to
7.4 miles northwest of the Ithaca VOR/DME. This Class E airspace
area is effective during the specific dates and times established in
advance by a Notice to Airmen. The effective date and time will
thereafter be continuously published in the Airport/Facility
Directory.
* * * * *

AEA NY E2 Poughkeepsie, NY [Corrected]

Dutchess County Airport, Poughkeepsie, NY
    (Lat. 41[deg]37'36'' N., long. 73[deg]53'03'' W.)
Kingston VORTAC
    (Lat. 41[deg]39'56'' N., long. 73[deg]49'20'' W.)

    Within a 4-mile radius of the Dutchess County Airport; and that
airspace extending upward from the surface within 3.1 miles each
side of the Kingston VORTAC 025[deg] radial extending from the
VORTAC to 8.3 miles northeast of the VORTAC, and within 1.8 miles
each side of the Kingston VORTAC 231[deg] radial extending from the
4-mile radius to 9.2 miles southwest of the VORTAC and within 3.1
miles each side of the Kingston VORTAC 050[deg] radial extending
from the VORTAC to 9.2 miles northeast of the VORTAC. This Class E
airspace area is effective during the specific dates and times
established in advance by a Notice to Airmen. The effective date and
time will thereafter be continuously published in the Airport/
Facility Directory.

    Issued in College Park, Georgia, on March 23, 2016.
Jim Dickinson,
Acting Manager, Operations Support Group, Eastern Service Center, Air
Traffic Organization.
[FR Doc. 2016-07077 Filed 3-29-16; 8:45 am]
 BILLING CODE 4910-13-P