[Federal Register Volume 75, Number 140 (Thursday, July 22, 2010)]
[Rules and Regulations]
[Pages 42592-42597]
[FR Doc No: 2010-17611]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0671; Directorate Identifier 2010-NM-142-AD;
Amendment 39-16363; AD 2010-14-18]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Model 767-200, -300,
and -300F Series Airplanes Powered by General Electric or Pratt &
Whitney Engines

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

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is superseding an existing airworthiness directive
(AD) that applies to certain Model 767-200, -300, and -300F series
airplanes. The

existing AD currently requires repetitive inspections to detect
discrepancies of the 8 aft-most fastener holes in the horizontal tangs
of the midspar fitting of the strut, and corrective actions if
necessary. The existing AD also requires repetitive inspections for
cracks of the closeout angle that covers the 2 aft-most fasteners in
the lower tang of the midspar fitting, and related investigative and
corrective actions if necessary. The existing AD also provides an
optional terminating action for the repetitive inspections. This new AD
reduces the compliance times for doing the inspections. This AD results
from reports of cracks in the midspar fitting tangs. We are issuing
this AD to detect and correct fatigue cracking in the primary strut
structure and reduced structural integrity of the strut, which could
result in separation of the strut and engine.

DATES: This AD becomes effective August 6, 2010.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of August 6,
2010.
    We must receive any comments on this AD by September 7, 2010.

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 AD, contact Boeing
Commercial Airplanes, Attention: Data & Services Management, P.O. Box
3707, MC 2H-65, Seattle, Washington 98124-2207; telephone<PHONE_NUMBER>,
extension 1; fax<PHONE_NUMBER>; e-mail<EMAIL_ADDRESS>Internet
https://www.myboeingfleet.com.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The 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: Berhane Alazar, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office
(ACO), 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6577; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    On September 13, 2005, we issued AD 2005-19-23, amendment 39-14288
(70 FR 55519, September 22, 2005). That AD applies to certain Boeing
Model 767-200, -300, and -300F series airplanes. That AD requires
repetitive inspections to detect discrepancies of the eight aft-most
fastener holes in the horizontal tangs of the midspar fitting of the
strut, and corrective actions if necessary. That AD also requires
repetitive inspections for cracks of the closeout angle that covers the
two aft-most fasteners in the lower tang of the midspar fitting, and
related investigative and corrective actions if necessary. That AD also
provides an optional terminating action for the repetitive inspections.
That AD resulted from a report of a crack in a closeout angle that
covers the two aft-most fasteners in the lower tang of the midspar
fitting, and the discovery of a crack in the lower tang of the midspar
fitting under the cracked closeout angle. The actions specified in that
AD are intended to prevent fatigue cracking in the primary strut
structure and reduced structural integrity of the strut, which could
result in separation of the strut and engine.

Actions Since AD Was Issued

    Since we issued that AD, we received two reports of cracks in the
midspar fitting tangs. The first report indicated severed upper and
lower tangs at the aft two fastener locations in the Number 1 pylon
inboard midspar fitting. The cracks were found during a routine check
of a Model 767-300 airplane at approximately 92,205 total flight hours
and 14,969 total flight cycles. This airplane had incurred 408 flight
cycles from the previous inspection. The second report indicated cracks
in the Number 1 pylon inboard midspar fitting lower tang, between the
aft two fastener holes, on a Model 767-300 airplane at approximately
94,176 total flight hours and 15,405 total flight cycles. This airplane
had incurred 830 cycles from the previous inspection.
    AD 2005-19-23 specified repetitive inspection intervals between
1,500 flight cycles and 16,000 flight cycles, depending on the
inspection type and location. We have determined that the affected
airplanes must be inspected within 400 flight cycles since the previous
inspection and, for those airplanes that have not yet been inspected,
the compliance time threshold of 10,000 total flight cycles specified
in AD 2005-19-23 must be reduced to 8,000 total flight cycles. We have
also determined that repetitive inspection intervals must be reduced to
400 flight cycles and 6,000 flight cycles, depending on the inspection
type.

Relevant Service Information

    We have reviewed Boeing Alert Service Bulletin 767-54A0101,
Revision 5, dated June 29, 2010. We referred to Boeing Alert Service
Bulletin 767-54A0101, Revision 4, dated February 10, 2005, for doing
certain actions required by AD 2005-19-23. The procedures in Revision 5
are similar to the procedures in Revision 4. Revision 5 reduces the
compliance times for doing the procedures.
    We have also reviewed Boeing Alert Service Bulletin 767-54A0062,
Revision 6, dated November 5, 2009; and Boeing Alert Service Bulletin
767-54A0074, Revision 1, dated April 24, 2008; which are the latest
versions of certain service bulletins referred to in AD 2005-19-23 as
additional sources of guidance for doing the terminating action. Boeing
Alert Service Bulletin 767-54A0101, Revision 5, dated June 29, 2010,
refers to Boeing Alert Service Bulletin 767-54A0062, Revision 6, dated
November 5, 2009; and Boeing Alert Service Bulletin 767-54A0074,
Revision 1, dated April 24, 2008; as additional sources of guidance for
doing the terminating action in Part 4 of the alert service bulletin.

Other Relevant Rulemaking

    The FAA has issued the following ADs that are related to the
additional sources of guidance specified in this AD.

                                        Table--Other Relevant Rulemaking
----------------------------------------------------------------------------------------------------------------
                                                                 Related Boeing Service
                  AD                        Applicability               Bulletin              AD requirement
----------------------------------------------------------------------------------------------------------------
AD 2000-07-05, amendment 39-11659 (65  Certain Boeing Model     767-54A0094............  Repetitive inspections
 FR 18883, April 10, 2000).             767 series airplanes.                             to detect cracking or
                                                                                damage of the forward
                                                                                and aft lugs of the
                                                                                diagonal brace of the
                                                                                nacelle strut; follow-
                                                                                on actions, if
                                                                                necessary; and
                                                                                terminating action for
                                                                                the repetitive
                                                                                inspections.
AD 2004-16-12, amendment 39-13768 (69  Certain Boeing Model     767-54-0069, 767-54-     Modification of the
 FR 51002, August 17, 2004).            767-200, -300, and -     0080, 767-54-0081, and   nacelle strut and wing
                                        300F series airplanes    767-54A0094.             structure. (AD 2004-16-
                                        powered by Pratt &                                12 superseded AD 2001-
                                        Whitney engines or                                02-07, Amendment 39-
                                        General Electric                                  12091 and AD 2001-06-
                                        engines.                                          12, Amendment 39-
                                                                                12159.)
AD 2009-20-09, amendment 39-16032 (74  Certain Boeing Model     767-54A0074............  Repetitive inspections
 FR 50692, October 1, 2009).            767-200, -300, and -                              for fatigue cracking
                                        300F series airplanes.                            and corrosion of the
                                                                                upper link fuse pin of
                                                                                the nacelle struts,
                                                                                and related
                                                                                investigative and
                                                                                corrective actions if
                                                                                necessary.
AD 2010-03-08, amendment 39-16192 (75  Certain Boeing Model     767-54A0062,...........  Repetitive detailed and
 FR 5677, February 4, 2010).            767-200, -300, and -    767-54-0069............   eddy current
                                        300F series airplanes.                            inspections to detect
                                                                                cracks of certain
                                                                                midspar fuse pins, and
                                                                                corrective action if
                                                                                necessary. (AD 2010-03-
                                                                                08 superseded AD 2003-
                                                                                03-02, Amendment 39-
                                                                                13026.)
----------------------------------------------------------------------------------------------------------------

FAA's Determination and Requirements of This AD

    The unsafe condition described previously is likely to exist or
develop on other airplanes of the same type design. For this reason, we
are issuing this AD to supersede AD 2005-19-23. This AD requires
accomplishing the actions specified in Boeing Alert Service Bulletin
767-54A0101, Revision 5, dated June 29, 2010, described previously,
except as discussed under ``Differences Between the AD and the Service
Bulletin.''

Differences Between the AD and the Service Bulletin

    The service bulletin specifies to contact the manufacturer for
instructions on how to repair certain conditions, but this AD requires
repairing those conditions in one of the following ways:
     In accordance with a method that we approve; or
     Using data that meet the certification basis of the
airplane, and that have been approved by the Boeing Commercial
Airplanes Organization Designation Authorization (ODA) whom we have
authorized to make those findings.
    Steps 4.a. and 4.b. of Part 2 of the Work Instructions of Boeing
Alert Service Bulletin 767-54A0101, Revision 5, dated June 29, 2010,
specify actions if cracking is found and the hole size is either
greater than 0.5322 inch or less than 0.5322 inch but not if the hole
size equals 0.5322 inch. This AD specifies that if cracking is found
and the hole size equals 0.5322 inch, then the terminating action
specified in step 4.a. of Part 2 of the Work Instructions of Boeing
Alert Service Bulletin 767-54A0101, Revision 5, dated June 29, 2010,
must be accomplished.

Interim Action

    We consider this AD interim action. We are currently considering
additional rulemaking to expand the inspection area.

FAA's Justification and Determination of the Effective Date

    Fatigue cracking in the primary strut structure could result in
reduced structural integrity of the strut and consequent separation of
the strut and engine. Because of our requirement to promote safe flight
of civil aircraft and thus, the critical need to ensure the structural
integrity of the pylon structure and midspar fittings and the short
compliance time involved with this action, this AD must be issued
immediately.
    Because an unsafe condition exists that requires the immediate
adoption of this AD, we find that notice and opportunity for prior
public comment hereon are impracticable and that good cause exists for
making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2010-0671; Directorate Identifier 2010-NM-142-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about 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

    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 the 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); and
    3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends part 39 of the Federal Aviation Regulations (14 CFR part
39) as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

0
2. The Federal Aviation Administration (FAA) amends Sec.  39.13 by
removing amendment 39-14288 (70 FR 55519, September 22, 2005) and by
adding the following new airworthiness directive (AD):

2010-14-18 The Boeing Company: Amendment 39-16363. Docket No. FAA-
2010-0671; Directorate Identifier 2010-NM-142-AD.

Effective Date

    (a) This AD becomes effective August 6, 2010.

Affected ADs

    (b) This AD supersedes AD 2005-19-23, Amendment 39-14288.

Applicability

    (c) This AD applies to The Boeing Company Model 767-200, -300,
and -300F series airplanes, certificated in any category; as
identified in Boeing Alert Service Bulletin 767-54A0101, Revision 5,
dated June 29, 2010.

Subject

    (d) Air Transport Association (ATA) of America Code 54:
Nacelles/Pylons.

Unsafe Condition

    (e) This AD results from reports of cracks in the midspar
fitting tangs. The Federal Aviation Administration is issuing this
AD to detect and correct fatigue cracking in the primary strut
structure and reduced structural integrity of the strut, which could
result in separation of the strut and engine.

Compliance

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

    Note 1: Notwithstanding any inspection done in accordance with
AD 2005-19-23, inspect within the compliance times specified in this
AD.

Initial Inspection

    (g) At the applicable time specified in paragraph (h) of this
AD: Do the actions specified in either paragraph (g)(1) or (g)(2) of
this AD.
    (1) Do a detailed inspection for cracking of the 8 aft-most
fastener holes in the horizontal tangs of the midspar fitting of the
strut, and a surface high frequency eddy current (HFEC) inspection
for cracking of the closeout angle that covers the 2 aft-most
fasteners in the lower tang of the midspar fitting, in accordance
with Part 1, ``Detailed Inspection of Midspar Fitting and Surface
High Frequency Eddy Current (HFEC) Inspection of Closeout Angle,''
of the Work Instructions of Boeing Alert Service Bulletin 767-
54A0101, Revision 5, dated June 29, 2010.
    (2) Do an open-hole HFEC inspection for cracking of each
fastener hole, inspect to determine the size of each fastener hole,
and do all applicable related investigative and corrective actions,
in accordance with Part 2, ``Open Hole HFEC Inspection,'' of the
Work Instructions of Boeing Alert Service Bulletin 767-54A0101,
Revision 5, dated June 29, 2010, except as required by paragraphs
(m) and (n) of this AD, and except as provided by paragraph (p) of
this AD. Do all applicable related investigative and corrective
actions before further flight.
    (h) At the applicable time specified in paragraph (h)(1) or
(h)(2) of this AD, do the actions specified in paragraph (g) of this
AD.
    (1) For airplanes on which an inspection (any Part 1 or Part 2
inspection) has not been done in accordance with any service
bulletin listed in Table 1 of this AD as of the effective date of
this AD: Prior to the accumulation of 8,000 total flight cycles, or
within 90 days after the effective date of this AD, whichever occurs
later, do the actions specified in paragraph (g) of this AD.

                       Table 1--Service Bulletins
------------------------------------------------------------------------
       Service Bulletin            Revision               Date
------------------------------------------------------------------------
Boeing Alert Service Bulletin  4..............  February 10, 2005.
 767-54A0101.
Boeing Alert Service Bulletin  5..............  June 29, 2010.
 767-54A0101.
Boeing Service Bulletin 767-   2..............  January 10, 2002.
 54A0101.
Boeing Service Bulletin 767-   3..............  September 5, 2002.
 54A0101.
------------------------------------------------------------------------

     (2) For airplanes on which any inspection (any Part 1 or Part 2
inspection) has been done in accordance with any service bulletin
listed in Table 1 of this AD as of the effective date of this AD:
Within 400 flight cycles after doing the most recent inspection or
within 90 days after the effective date of this AD, whichever occurs
later, do the actions specified in paragraph (g) of this AD.

Repetitive Inspections

    (i) If, during any detailed and surface HFEC inspection
specified by paragraph (g)(1) of this AD, no cracking is found, do
the actions specified in either paragraph (i)(1) or (i)(2) of this
AD.
    (1) Repeat the inspections specified in paragraph (g)(1) of this
AD thereafter at intervals not to exceed 400 flight cycles.
    (2) Within 400 flight cycles after doing the most recent
inspections specified in paragraph (g)(1) of this AD, do the actions
specified in paragraph (g)(2) of this AD and repeat thereafter at
intervals not to exceed 6,000 flight cycles.
    (j) If, during the actions specified by paragraph (g)(2) of this
AD, the terminating action specified in Part 4 of the Work
Instructions of Boeing Alert Service Bulletin

767-54A0101, Revision 5, dated June 29, 2010, is not done, do the
actions specified in either paragraph (j)(1) or (j)(2) of this AD.
    (1) Within 6,000 flight cycles after doing the actions specified
in paragraph (g)(2) of this AD, do the inspections specified in
paragraph (g)(1) of this AD and repeat the inspections thereafter at
intervals not to exceed 400 flight cycles.
    (2) Repeat the actions specified in paragraph (g)(2) of this AD
thereafter at intervals not to exceed 6,000 flight cycles.

Corrective Actions for Inspections Done per Paragraph (g)(1) of This AD

    (k) If, during any inspection specified by paragraph (g)(1) of
this AD, any crack is found in the midspar fitting tangs, before
further flight, do the actions specified in paragraph (k)(1) or
(k)(2) of this AD.
    (1) Do the terminating action specified in Part 4 of the Work
Instructions of Boeing Alert Service Bulletin 767-54A0101, Revision
5, dated June 29, 2010, except as required by paragraph (m) of this
AD. Accomplishment of this paragraph terminates the requirements of
this AD.
    (2) Replace the midspar fitting of the strut with a new part, or
repair in accordance with a method approved by the Manager, Seattle
Aircraft Certification Office (ACO), FAA. Within 8,000 flight cycles
after doing the replacement, do the actions specified in either
paragraph (k)(2)(i) or (k)(2)(ii) of this AD.
    (i) Do the inspections specified in paragraph (g)(1) of this AD
and repeat the inspections thereafter at intervals not to exceed 400
flight cycles.
    (ii) Do the actions specified in paragraph (g)(2) of this AD and
repeat the actions thereafter at intervals not to exceed 6,000
flight cycles.
    (l) If, during any surface HFEC inspection specified by
paragraph (g)(1) of this AD, any crack is found in the closeout
angle, before further flight, do the open-hole HFEC inspection for
cracking and all applicable related investigative and corrective
actions, in accordance with Part 2, ``Open Hole HFEC Inspection,''
and step 4.b.(2) of Part 1, ``Detailed Inspection of Midspar Fitting
and Surface High Frequency Eddy Current (HFEC) Inspection of
Closeout Angle,'' of the Work Instructions of Boeing Alert Service
Bulletin 767-54A0101, Revision 5, dated June 29, 2010, except as
required by paragraphs (m) and (n) of this AD, and except as
provided by paragraph (p) of this AD. If the terminating action
specified in Part 4 of the Work Instructions of Boeing Alert Service
Bulletin 767-54A0101, Revision 5, dated June 29, 2010, is not done,
do the actions specified in either paragraph (l)(1) or (l)(2) of
this AD.
    (1) Within 6,000 flight cycles after doing the actions specified
in paragraph (l) of this AD, do the inspections specified in
paragraph (g)(1) of this AD and repeat the inspections thereafter at
intervals not to exceed 400 flight cycles.
    (2) Within 6,000 flight cycles after doing the actions specified
in paragraph (l) of this AD, do the actions specified in paragraph
(g)(2) of this AD, and repeat the actions thereafter at intervals
not to exceed 6,000 flight cycles.

Service Bulletin Exceptions

    (m) Where Boeing Alert Service Bulletin 767-54A0101, Revision 5,
dated June 29, 2010, specifies that the manufacturer may be
contacted for disposition of repair conditions: Before further
flight, accomplish the repair using a method approved in accordance
with the procedures specified in paragraph (r) of this AD.
    (n) If, during any open-hole HFEC inspection required by
paragraph (g)(2) or (l) of this AD, any crack is found in the
midspar fitting and the hole size is 0.5322 inch, before further
flight, do the terminating action specified in paragraph (k)(1) of
this AD.

Optional Terminating Action

    (o) Doing the terminating action specified in Part 4 of the Work
Instructions of Boeing Alert Service Bulletin 767-54A0101, Revision
5, dated June 29, 2010, terminates the requirements of this AD.

    Note 2:  Boeing Alert Service Bulletin 767-54A0101, Revision 5,
dated June 29, 2010, refers to the Boeing service bulletins in Table
2 of this AD as additional sources of guidance for doing the
terminating action in paragraphs (k) and (o) of this AD.

                                     Table 2--Additional Sources of Guidance
----------------------------------------------------------------------------------------------------------------
    Boeing Service Bulletin       Revision level          Date                           Title
----------------------------------------------------------------------------------------------------------------
767-54-0052...................  Original.........  June 11, 1992....  Nacelles/Pylons--Strut--Aft Lower Spar--
                                                                       Fastener Corrosion--Inspection and
                                                                       Replacement.
767-54-0061...................  2................  November 23, 1999  Nacelles/Pylons--Wing-to-Strut Attach
                                                                       Fittings--Lower Spar Bushing Inspection
                                                                       and Replacement.
767-54-0069...................  2................  August 31, 2000..  Nacelles/Pylons--Midspar Fitting--
                                                                       Underwing Sideload Fitting--Fuse Pin
                                                                       Replacement and Wing Rework.
767-54-0072...................  Original.........  March 13, 1997...  Nacelles/Pylons--Strut Attach Upper Link--
                                                                       Upper Link Inspection, Rework or
                                                                       Replacement.
767-54-0080...................  1................  May 9, 2002......  Nacelles/Pylons--Pratt and Whitney Powered
                                                                       Airplanes--Nacelle Strut and Wing
                                                                       Structure Modification.
767-54-0081...................  1................  February 7, 2002.  Nacelles/Pylons--General Electric Powered
                                                                       Airplanes--Nacelle Strut and Wing
                                                                       Structure Modification.
767-54A0062...................  6................  November 5, 2009.  Nacelles/Pylons--Strut Attach Fuse Pins--
                                                                       Midspar Fuse Pin Inspection and
                                                                       Replacement.
767-54A0074...................  1................  April 24, 2008...  Nacelles/Pylons--Strut Attach Fuse Pins--
                                                                       Upper link Fuse Pin Inspection/
                                                                       Replacement.
767-54A0094...................  2................  February 7, 2002.  Nacelles/Pylons--Strut--to--Wing
                                                                       Attachment--Diagonal Brace Inspection/
                                                                       Rework/Replacement.
767-57-0063...................  1................  November 30, 2000  Wings--Side Load Underwing Fitting --
                                                                       Inspection/Rework.
----------------------------------------------------------------------------------------------------------------

    Note 3:  Certain service bulletins referenced in Table 2 of this
AD are related to the ADs listed in Table 3 of this AD.

                                       Table 3--Other Relevant Rulemaking
----------------------------------------------------------------------------------------------------------------
                                                     Related Boeing
              AD                  Applicability     Service Bulletin                AD requirement
----------------------------------------------------------------------------------------------------------------
AD 2000-07-05, amendment 39-    Certain Boeing     767-54A0094......  Repetitive inspections to detect cracking
 11659.                          Model 767 series                      or damage of the forward and aft lugs of
                                 airplanes.                            the diagonal brace of the nacelle strut;
                                                                       follow-on actions, if necessary; and
                                                                       terminating action for the repetitive
                                                                       inspections.

AD 2004-16-12, amendment 39-    Certain Boeing     767-54-0069, 767-  Modification of the nacelle strut and wing
 13768.                          Model 767-200, -   54-0080, 767-54-   structure.
                                 300, and -300F     0081, and 767-
                                 series airplanes   54A0094.
                                 powered by Pratt
                                 & Whitney
                                 engines or
                                 General Electric
                                 engines.
AD 2009-20-09, amendment 39-    Certain Boeing     767-54A0074......  Repetitive inspections for fatigue
 16032.                          Model 767-200, -                      cracking and corrosion of the upper link
                                 300, and -300F                        fuse pin of the nacelle struts, and
                                 series airplanes.                     related investigative and corrective
                                                                       actions if necessary.
AD 2010-03-08, amendment 39-    Certain Boeing     767-54A0062, 767-  Repetitive detailed and eddy current
 16192.                          Model 767-200, -   54-0069.           inspections to detect cracks of certain
                                 300, and -300F                        midspar fuse pins, and corrective action
                                 series airplanes.                     if necessary.
----------------------------------------------------------------------------------------------------------------

Optional Corrective Action for Paragraph (g)(2) or (l) of This AD

    (p) In lieu of doing the related investigative and corrective
actions required by paragraph (g)(2) or (l) of this AD, before
further flight, replace the midspar fitting of the strut with a new
part, or repair in accordance with a method approved by the Manager,
Seattle Aircraft Certification Office (ACO), FAA. Within 8,000
flight cycles after doing any replacement, do the actions specified
in either paragraph (p)(1) or (p)(2) of this AD.
    (1) Do the inspections specified in paragraph (g)(1) of this AD
and repeat the inspections thereafter at intervals not to exceed 400
flight cycles.
    (2) Do the actions specified in paragraph (g)(2) of this AD and
repeat the actions thereafter at intervals not to exceed 6,000
flight cycles.

Terminating Action Accomplished per Previous Issues of Service Bulletin

    (q) Doing the terminating action specified in Part 4 of the Work
Instructions of any service bulletin listed in Table 4 of this AD
before the effective date of this AD is acceptable for compliance
with the requirements of this AD.

        Table 4--Credit Service Bulletins for Terminating Action
------------------------------------------------------------------------
      Service Bulletin            Revision                Date
------------------------------------------------------------------------
Boeing Alert Service          Original.......  September 23, 1999.
 Bulletin 767-54A0101.
Boeing Alert Service          4..............  February 10, 2005.
 Bulletin 767-54A0101.
Boeing Service Bulletin 767-  1..............  February 3, 2000.
 54A0101.
Boeing Service Bulletin 767-  2..............  January 10, 2002.
 54A0101.
Boeing Service Bulletin 767-  3..............  September 5, 2002.
 54A0101.
------------------------------------------------------------------------

Alternative Methods of Compliance (AMOCs)

    (r)(1) The Manager, Seattle Aircraft Certification 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:
Berhane Alazar, Aerospace Engineer, Airframe Branch, ANM-120S, FAA,
Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone<PHONE_NUMBER>; fax (425)
917-6590. Information may be e-mailed to<EMAIL_ADDRESS>    (2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards District Office.
The AMOC approval letter must specifically reference this AD.
    (3) 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.

Material Incorporated by Reference

    (s) You must use Boeing Alert Service Bulletin 767-54A0101,
Revision 5, dated June 29, 2010, to do the actions required by this
AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone
206-544-5000, extension 1; fax<PHONE_NUMBER>; e-mail
<EMAIL_ADDRESS>Internet https://www.myboeingfleet.com.
    (3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.
    (4) You may also review copies of the 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/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on July 9, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-17611 Filed 7-21-10; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register: March 5, 2008 (Volume 73, Number 44)]
[Notices]
[Page 11899-11901]
[DOCID:fr05mr08-48]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice of Filings 1

February 27, 2008.
    Take notice that the Commission received the following electric
corporate filings:

    Docket Numbers: EC08-44-000.
    Applicants: Birchwood Power Partners, L.P., J-POWER USA Investment
Co., Ltd.
    Description: Birchwood Power Partners, LP and J-Power USA
Investment Co, Ltd submits application seeking authorization for the
acquisition of a portion of the ownership interests in Birchwood etc.
    Filed Date: 02/21/2008.
    Accession Number: 20080225-0190.
    Comment Date: 5 p.m. Eastern Time on Thursday, March 13, 2008.

    Docket Numbers: EC08-45-000.
    Applicants: Cinergy Capital & Trading, Inc., Brownsville Power I,
LLC
    Description: Cinergy Capital & Trading, Inc and Brownsville Power
I, LLC submits an Application for Authorization for Disposition of
Jurisdictional Assets.
    Filed Date: 02/21/2008.
    Accession Number: 20080225-0192.
    Comment Date: 5 p.m. Eastern Time on Thursday, March 13, 2008.

    Docket Numbers: EC08-46-000.
    Applicants: Entergy Nuclear Generation Company, Entergy Nuclear

FitzPatrick, LLC, Entergy Nuclear Vermont Yankee, LLC, Entergy Nuclear
Indian Point 2, LLC, Entergy Nuclear Indian Point 3, LLC, Entergy
Nuclear Palisades, LLC, Entergy Nuclear Power Marketing, LLC.
    Description: Application under Section 203 of the Federal Power Act
for authorization of indirect disposition of jurisdictional facilities
and requests for waivers of Entergy Nuclear Generation Company et al.
    Filed Date: 02/21/2008.
    Accession Number: 20080225-0194.
    Comment Date: 5 p.m. Eastern Time on Thursday, March 13, 2008.

    Take notice that the Commission received the following electric
rate filings:

    Docket Numbers: ER99-2369-004.
    Applicants: Alliance for Cooperative Energy Services.
    Description: Alliance for Cooperative Energy Services Power
Marketing LLC submits amendment to its market-based rate tariff to
comply with Order 697.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0051.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-321-001.
    Applicants: New York Independent System Operator, Inc.
    Description: Public Submission of Pages of 12/10/07 Filing
Previously Submitted Pursuant to a Claim of Privilege of New York
Independent System Operator, Inc.
    Filed Date: 02/22/2008.
    Accession Number: 20080222-5044.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-397-001.
    Applicants: ALLETE, Inc.
    Description: ALLETE, Inc submits Original Sheet 7 of Rate Schedule
119 which was inadvertently omitted from the 2/8/08 filing.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0053.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-425-001.
    Applicants: Energy Exchange Direct, LLC.
    Description: Energy Exchange Direct, LLC submits an amended
petition for acceptance of initial tariff etc.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0052.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-551-001.
    Applicants: MidAmerican Energy Company.
    Description: MidAmerican Energy Co submits the amended Engineering
and Procurement Agreement to its 2/11/08 filing.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0054.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-590-000.
    Applicants: PJM Interconnection, L.L.C.
    Description: PJM Interconnection, LLC submits an executed Interim
Interconnection Service Agreement with Luke Paper Co et al.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0055
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-591-000.
    Applicants: Wisconsin Public Service Corporation.
    Description: Wisconsin Public Service Corp submits the actual 2007
value for billing for post-employment benefits.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0056.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-592-000.
    Applicants: Midwest Independent Transmission System Operator, Inc.
    Description: Midwest Independent Transmission System Operator, Inc
submits proposed revisions to the Coordination Agreement with Manitoba
Hydro.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0057.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-593-000.
    Applicants: American Electric Power Service Corporation.
    Description: American Electric Power Service Corp submits a fully
executed interconnection agreement with Turkey Track Wind Energy LLC.
    Filed Date: 02/22/2008.
    Accession Number: 20080226-0058.
    Comment Date: 5 p.m. Eastern Time on Friday, March 14, 2008.

    Docket Numbers: ER08-594-000.
    Applicants: Pacific Gas and Electric Company.
    Description: Pacific Gas and Electric Co submits a Notice of
Termination of the Agreement to Implement the Scheduling Coordinator
Transition with the County of San Francisco.
    Filed Date: 02/21/2008.
    Accession Number: 20080226-0059.
    Comment Date: 5 p.m. Eastern Time on Thursday, March 13, 2008.

    Docket Numbers: ER08-595-000.
    Applicants: Duke Energy Carolinas, LLC.
    Description: Duke Energy Carolinas, LLC submits the long-term
Transmission Service Agreement with the Carolina Power and Light Co.
    Filed Date: 02/25/2008.
    Accession Number: 20080227-0108.
    Comment Date: 5 p.m. Eastern Time on Monday, March 17, 2008.

    Docket Numbers: ER08-596-000.
    Applicants: PJM Interconnection, L.L.C.
    Description: PJM Interconnection, LLC submits amendments to
Schedule 12 of the Amended and Restated Operating Agreement to update
the member list.
    Filed Date: 02/25/2008.
    Accession Number: 20080227-0106.
    Comment Date: 5 p.m. Eastern Time on Monday, March 17, 2008.

    Docket Numbers: ER08-597-000.
    Applicants: Commonwealth Edison Company.
    Description: Commonwealth Edison Co submits an cancellation of the
executed Interconnection Agreement 729.
    Filed Date: 02/26/2008.
    Accession Number: 20080227-0107.
    Comment Date: 5 p.m. Eastern Time on Tuesday, March 18, 2008.

    Any person desiring to intervene or to protest in any of the above
proceedings must file in accordance with Rules 211 and 214 of the
Commission's Rules of Practice and Procedure (18 CFR 385.211 and
385.214) on or before 5 p.m. Eastern time on the specified comment
date. It is not necessary to separately intervene again in a subdocket
related to a compliance filing if you have previously intervened in the
same docket. Protests will be considered by the Commission in
determining the appropriate action to be taken, but will not serve to
make protestants parties to the proceeding. Anyone filing a motion to
intervene or protest must serve a copy of that document on the
Applicant. In reference to filings initiating a new proceeding,
interventions or protests submitted on or before the comment deadline
need not be served on persons other than the Applicant.
    The Commission encourages electronic submission of protests and
interventions in lieu of paper, using the FERC Online links at http://
www.ferc.gov. To facilitate electronic service, persons with Internet
access who will eFile a document and/or be listed as a contact for an
intervenor must create and validate an eRegistration account using the
eRegistration link. Select the eFiling link to log on and submit the
intervention or protests.
    Persons unable to file electronically should submit an original and
14 copies of the intervention or protest to the

Federal Energy Regulatory Commission, 888 First St., NE., Washington,
DC 20426.
    The filings in the above proceedings are accessible in the
Commission's eLibrary system by clicking on the appropriate link in the
above list. They are also available for review in the Commission's
Public Reference Room in Washington, DC. There is an eSubscription link
on the Web site that enables subscribers to receive e-mail notification
when a document is added to a subscribed docket(s). For assistance with
any FERC Online service, please e-mail<EMAIL_ADDRESS>or
call<PHONE_NUMBER> (toll free). For TTY, call<PHONE_NUMBER>.

Nathaniel J. Davis, Sr.,
Deputy Secretary.
[FR Doc. E8-4204 Filed 3-4-08; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 77, Number 156 (Monday, August 13, 2012)]
[Notices]
[Pages 48202-48203]
[FR Doc No: 2012-19802]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. PE-2012-31]

Petition for Exemption; Summary of Petition Received

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of petition for exemption received.

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

SUMMARY: This notice contains a summary of a petition seeking relief
from specified requirements of 14 CFR. The purpose of this notice is to
improve the public's awareness of, and participation in, this aspect of
FAA's regulatory activities. Neither publication of this notice nor the
inclusion or omission of information in the summary is intended to
affect the legal status of any petition or its final disposition.

DATES: Comments on this petition must identify the petition docket
number and must be received on or before August 23, 2012.

ADDRESSES: You may send comments identified by Docket Number FAA-2012-
0553 using any of the following methods:
     Government-wide rulemaking web site: Go to http://www.regulations.gov and follow the instructions for sending your
comments electronically.
     Mail: Send comments to the Docket Management Facility;
U.S. Department of Transportation, 1200 New Jersey Avenue SE., West
Building Ground Floor, Room W12-140, Washington, DC 20590.
     Fax: Fax comments to the Docket Management Facility at
202-493-2251.
     Hand Delivery: Bring comments to the Docket Management
Facility in Room W12-140 of the West Building Ground Floor at 1200 New
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
    Privacy: We will post all comments we receive, without change, to
http://www.regulations.gov, including any personal information you
provide. Using the search function of our docket Web site, anyone can
find and read the comments received into any of our dockets, including
the name of the individual sending the comment (or signing the comment
for an association, business, labor union, etc.). You may review DOT's
complete Privacy Act Statement in the Federal Register published on
April 11, 2000 (65 FR 19477-78).
    Docket: To read background documents or comments received, go to
http://www.regulations.gov at any time or to the Docket Management
Facility in Room W12-140 of the West Building Ground Floor at 1200 New
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Mark Forseth,<PHONE_NUMBER>),
Standardization Branch, ANM-113, Federal Aviation Administration, 1601
Lind Avenue SW., Renton, WA 98057-3356, or Frances Shaver, (202) 267-
4059, Office of Rulemaking, ARM-207, Federal Aviation Administration,
800 Independence Avenue SW., Washington, DC 20591.

    This notice is published pursuant to 14 CFR 11.85.

    Issued in Washington, DC, on August 2, 2012.
Lirio Liu,
Acting Director, Office of Rulemaking.

Petitions for Exemption

    Docket No.: FAA-2012-0553.
    Petitioner: Gulfstream Aerospace LP.
    Sections of 14 CFR Affected: Sec.  25.901(b)(2), Sec.
25.903(d)(2), Sec.  25.939(a), Sec.  25.1301(c) and (d), Sec.
25.1305(c)(1), Sec.  25.1322(a), and Sec.  25.1309(c) and (d).
    Description of Relief Sought: Gulfstream requests relief from
certain engine installation, operational limitation and engine
indication requirements which apply to the Gulfstream G280 airplane and
installed Honeywell AS907-2-1G engines.

[FR Doc. 2012-19802 Filed 8-10-12; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 83, Number 89 (Tuesday, May 8, 2018)]
[Rules and Regulations]
[Pages 20728-20731]
[FR Doc No: 2018-09565]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 97

[Docket No. 31191; Amdt. No. 3798]

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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: This rule amends, suspends, or removes 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 for the safe and efficient use of the
navigable airspace and to promote safe flight operations under
instrument flight rules at the affected airports.

DATES: This rule is effective May 8, 2018. The compliance date for each
SIAP, associated Takeoff Minimums, and ODP is specified in the
amendatory provisions.
    The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of May 8, 2018.

ADDRESSES: Availability of matter incorporated by reference in the
amendment is as follows:

For Examination

    1. U.S. Department of Transportation, Docket Ops-M30, 1200 New
Jersey Avenue SE, West Bldg., Ground Floor, Washington, DC, 20590-0001;
    2. The FAA Air Traffic Organization Service Area in which the
affected airport is located;
    3. The office of Aeronautical Navigation Products, 6500 South
MacArthur Blvd., Oklahoma City, OK 73169 or,
    4. The National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, call 202-741-
6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Availability

    All SIAPs and Takeoff Minimums and ODPs are available online free
of charge. Visit the National Flight Data Center online at nfdc.faa.gov
to register. Additionally, individual SIAP and Takeoff Minimums and ODP
copies may be obtained from the FAA Air Traffic Organization Service
Area in which the affected airport is located.

FOR FURTHER INFORMATION CONTACT: Thomas J. Nichols, Flight Procedure
Standards Branch (AFS-420)Flight Technologies and Procedures 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 (NFDC)/Permanent Notice to
Airmen (P-NOTAM), and is incorporated by reference under 5 U.S.C.
552(a), 1 CFR part 51, and 14 CFR 97.20. 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 on FAA form documents is unnecessary.
    This amendment provides the affected CFR sections, and specifies
the SIAPs and Takeoff Minimums and ODPs with their applicable effective
dates. This amendment also identifies the airport and its location, the
procedure and the amendment number.

Availability and Summary of Material Incorporated by Reference

    The material incorporated by reference is publicly available as
listed in the ADDRESSES section.
    The material incorporated by reference describes SIAPs, Takeoff
Minimums and ODPs as identified in the amendatory language for part 97
of this final rule.

The Rule

    This amendment to 14 CFR part 97 is effective upon publication of
each separate SIAP and Takeoff Minimums and ODP as amended in the
transmittal. For safety and timeliness of change considerations, this
amendment incorporates only specific changes contained for each SIAP
and Takeoff Minimums and ODP as modified by FDC permanent NOTAMs.
    The SIAPs and Takeoff Minimums and ODPs, as modified by FDC
permanent 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 and Takeoff
Minimums and ODPs, 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 that created the need for these SIAP and Takeoff
Minimums and ODP amendments require making them effective in less than
30 days.
    Because of the close and immediate relationship between these
SIAPs, Takeoff Minimums and ODPs, and safety in air commerce, I find
that notice and public procedure under 5 U.S.C. 553(b) are
impracticable and contrary to the public interest and, where
applicable, under 5 U.S.C. 553(d), good cause exists for making these
SIAPs effective in less than 30 days.
    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,
Navigation (Air).

    Issued in Washington, DC on April 20, 2018.
John S. Duncan,
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 and Takeoff Minimums
and ODPs, 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(f), 106(g), 40103, 40106, 40113,
40114, 40120, 44502, 44514, 44701, 44719, 44721-44722.

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

Sec. Sec.  97.23, 97.25, 97.27, 97.29, 97.31, 97.33, 97.35  [AMENDED]

    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
--------------------------------------------------------------------------------------------------------------------------------------------------------
24-May-18........................  RI               Newport.............  Newport State.......          8/4781         3/29/18  This NOTAM, published in
                                                                                TL 18-11, is hereby
                                                                                rescinded in its
                                                                                entirety.
24-May-18........................  AZ               Phoenix.............  Phoenix-Mesa Gateway          7/3135          4/6/18  RNAV (GPS) RWY 12R, Amdt
                                                                                1B
24-May-18........................  AZ               Phoenix.............  Phoenix-Mesa Gateway          7/3136          4/6/18  RNAV (GPS) RWY 30L, Amdt
                                                                                1B
24-May-18........................  OK               Norman..............  University of                 7/4912         4/11/18  LOC RWY 3, Amdt 4
                                                                           Oklahoma Westheimer.
24-May-18........................  OK               Norman..............  University of                 7/4913         4/11/18  RNAV (GPS) RWY 18, Amdt
                                                                           Oklahoma Westheimer.                                  2
24-May-18........................  OK               Ardmore.............  Ardmore Muni........          7/5209          4/6/18  ILS OR LOC RWY 31, Amdt
                                                                                5B
24-May-18........................  OK               Ardmore.............  Ardmore Muni........          7/5213          4/6/18  RNAV (GPS) RWY 31, Amdt
                                                                                1B
24-May-18........................  PA               Franklin............  Venango Rgnl........          7/6969         4/11/18  VOR RWY 21, Amdt 8A
24-May-18........................  CO               Rifle...............  Rifle Garfield                7/7921         4/11/18  RNAV (RNP) Z RWY 26,
                                                                           County.                                               Amdt 1B
24-May-18........................  MI               Allegan.............  Padgham Field.......          8/0101          4/6/18  RNAV (GPS) RWY 29, Orig
24-May-18........................  MI               Allegan.............  Padgham Field.......          8/0117          4/6/18  RNAV (GPS) RWY 11, Orig-
                                                                                A
24-May-18........................  MI               Allegan.............  Padgham Field.......          8/0119          4/6/18  VOR RWY 29, Amdt 14
24-May-18........................  MO               Fulton..............  Elton Hensley                 8/0231          4/6/18  Takeoff Minimums and
                                                                           Memorial.                                             Obstacle DP, Amdt 1
24-May-18........................  IN               Goshen..............  Goshen Muni.........          8/0233          4/6/18  Takeoff Minimums and
                                                                                Obstacle DP, Orig
24-May-18........................  TX               Longview............  East Texas Rgnl.....          8/0245          4/6/18  ILS OR LOC RWY 13, Amdt
                                                                                13A
24-May-18........................  NE               Grand Island........  Central Nebraska              8/0251          4/6/18  ILS OR LOC RWY 35, Amdt
                                                                           Rgnl.                                                 9F
24-May-18........................  KS               Topeka..............  Topeka Rgnl.........          8/0311          4/6/18  ILS OR LOC RWY 31, Amdt
                                                                                10
24-May-18........................  CA               Upland..............  Cable...............          8/0674         4/11/18  VOR-A, Orig-A
24-May-18........................  MO               Charleston..........  Mississippi County..          8/1039          4/6/18  Takeoff Minimums and
                                                                                Obstacle DP, Orig
24-May-18........................  AK               Mountain Village....  Mountain Village....          8/1212         4/11/18  RNAV (GPS) RWY 2, Amdt
                                                                                1A
24-May-18........................  KS               Wichita.............  Wichita Dwight D              8/1316          4/6/18  RNAV (RNP) Z RWY 19L,
                                                                           Eisenhower National.                                  Amdt 1

24-May-18........................  KS               Wichita.............  Wichita Dwight D              8/1317          4/6/18  RNAV (GPS) Y RWY 19L,
                                                                           Eisenhower National.                                  Amdt 2
24-May-18........................  AR               De Queen............  J Lynn Helms Sevier           8/1950         4/11/18  RNAV (GPS) RWY 8, Orig-A
                                                                           County.
24-May-18........................  NM               Santa Fe............  Santa Fe Muni.......          8/2099         4/11/18  Takeoff Minimums and
                                                                                Obstacle DP, Amdt 4
24-May-18........................  AK               Homer...............  Homer...............          8/2638         4/11/18  LOC BC RWY 22, Amdt 6
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/2770          4/9/18  RNAV (GPS) RWY 13, Orig-
                                                                                A
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/2771          4/9/18  RNAV (GPS) RWY 18, Orig-
                                                                                A
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/2772          4/9/18  RNAV (GPS) RWY 31, Amdt
                                                                                1A
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/2773          4/9/18  RNAV (GPS) RWY 36, Orig-
                                                                                B
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/2774          4/9/18  LOC BC RWY 31, Amdt 21D
24-May-18........................  MI               Battle Creek........  W K Kellogg.........          8/3215         4/11/18  ILS OR LOC RWY 23R, Amdt
                                                                                19
24-May-18........................  IL               Belleville..........  Scott AFB/MidAmerica          8/3218         4/11/18  ILS OR LOC RWY 32R, Orig-
                                                                                H
24-May-18........................  CO               Grand Junction......  Grand Junction                8/3221         4/11/18  ILS OR LOC RWY 11, Amdt
                                                                           Regional.                                             16B
24-May-18........................  OH               Jackson.............  James A Rhodes......          8/3523          4/9/18  RNAV (GPS) RWY 1, Amdt
                                                                                1D
24-May-18........................  OH               Jackson.............  James A Rhodes......          8/3526          4/9/18  RNAV (GPS) RWY 19, Amdt
                                                                                1C
24-May-18........................  OH               Jackson.............  James A Rhodes......          8/3527          4/9/18  VOR/DME-A, Amdt 2B
24-May-18........................  IA               Shenandoah..........  Shenandoah Muni.....          8/3555          4/9/18  RNAV (GPS) RWY 4, Orig
24-May-18........................  IA               Shenandoah..........  Shenandoah Muni.....          8/3561          4/9/18  VOR/DME RWY 12, Amdt 4A
24-May-18........................  IA               Shenandoah..........  Shenandoah Muni.....          8/3565          4/9/18  NDB RWY 4, Orig-B
24-May-18........................  NE               Gothenburg..........  Gothenburg Muni.....          8/3991         4/11/18  Takeoff Minimums and
                                                                                Obstacle DP, Amdt 1A
24-May-18........................  MO               Joplin..............  Joplin Rgnl.........          8/4158          4/9/18  ILS OR LOC/DME RWY 18,
                                                                                Amdt 2A
24-May-18........................  NC               Charlotte...........  Charlotte/Douglas             8/4264         4/17/18  Takeoff Minimums and
                                                                           Intl.                                                 Obstacle DP, Amdt 7
24-May-18........................  AK               Bethel..............  Bethel..............          8/4455         4/11/18  ILS Z OR LOC Z RWY 19R,
                                                                                Amdt 7E
24-May-18........................  ND               Dickinson...........  Dickinson--Theodore           8/4462          4/9/18  RNAV (GPS) RWY 32, Amdt
                                                                           Roosevelt Rgnl.                                       2
24-May-18........................  ND               Dickinson...........  Dickinson--Theodore           8/4479          4/9/18  RNAV (GPS) RWY 25, Orig-
                                                                           Roosevelt Rgnl.                                       A
24-May-18........................  ND               Dickinson...........  Dickinson--Theodore           8/4480          4/9/18  ILS OR LOC RWY 32, Amdt
                                                                           Roosevelt Rgnl.                                       1B
24-May-18........................  IL               Lincoln.............  Logan County........          8/4657         4/11/18  RNAV (GPS) RWY 3, Orig
24-May-18........................  IL               Lincoln.............  Logan County........          8/4659         4/11/18  RNAV (GPS) RWY 21, Orig
24-May-18........................  IL               Lincoln.............  Logan County........          8/4660         4/11/18  VOR RWY 3, Amdt 7
24-May-18........................  IL               Lincoln.............  Logan County........          8/4661         4/11/18  NDB RWY 21, Amdt 2
24-May-18........................  TX               Amarillo............  Rick Husband                  8/4668         4/13/18  LDA/DME RWY 22, Amdt 1
                                                                           Amarillo Intl.
24-May-18........................  AR               Clinton.............  Holley Mountain               8/4720         4/11/18  RNAV (GPS) RWY 23, Amdt
                                                                           Airpark.                                              1A
24-May-18........................  AR               Clinton.............  Holley Mountain               8/4721         4/11/18  RNAV (GPS) RWY 5, Amdt
                                                                           Airpark.                                              1B
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4775          4/6/18  ILS OR LOC RWY 15, Amdt
                                                                                1B
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4777          4/6/18  RNAV (GPS) RWY 3, Amdt
                                                                                1C
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4780          4/6/18  RNAV (GPS) RWY 15, Amdt
                                                                                2B
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4783          4/6/18  RNAV (GPS) RWY 21, Amdt
                                                                                1D
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4784          4/6/18  RNAV (GPS) RWY 33, Amdt
                                                                                1C
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4791          4/6/18  VOR RWY 3, Amdt 9A
24-May-18........................  IA               Davenport...........  Davenport Muni......          8/4792          4/6/18  VOR RWY 21, Amdt 8B
24-May-18........................  MN               Austin..............  Austin Muni.........          8/4821         4/11/18  RNAV (GPS) RWY 17, Amdt
                                                                                1B
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5371          4/9/18  ILS OR LOC RWY 6, Amdt
                                                                                23A
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5372          4/9/18  ILS OR LOC/DME RWY 24,
                                                                                Amdt 1A
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5373         4/13/18  RNAV (GPS) RWY 6, Amdt
                                                                                1B
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5374          4/9/18  RNAV (GPS) RWY 24, Amdt
                                                                                1A
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5375          4/9/18  RNAV (GPS) RWY 31, Amdt
                                                                                2A
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5376          4/9/18  VOR-A, Amdt 10
24-May-18........................  PA               Allentown...........  Lehigh Valley Intl..          8/5390          4/9/18  TACAN-C, Orig
24-May-18........................  RI               Newport.............  Newport State.......          8/6556         4/11/18  VOR/DME RWY 16, Amdt 1B
24-May-18........................  ND               Casselton...........  Casselton Robert              8/7299         4/11/18  RNAV (GPS) RWY 31, Amdt
                                                                           Miller Rgnl.                                          1
24-May-18........................  ND               Casselton...........  Casselton Robert              8/7300         4/11/18  VOR/DME RWY 31, Amdt 1A
                                                                           Miller Rgnl.
24-May-18........................  SD               Huron...............  Huron Rgnl..........          8/7324         4/11/18  ILS OR LOC RWY 12, Amdt
                                                                                10
24-May-18........................  SD               Huron...............  Huron Rgnl..........          8/7325         4/11/18  LOC/DME BC RWY 30, Amdt
                                                                                13
24-May-18........................  SD               Huron...............  Huron Rgnl..........          8/7326         4/11/18  VOR RWY 12, Amdt 22
24-May-18........................  SD               Huron...............  Huron Rgnl..........          8/7327         4/11/18  RNAV (GPS) RWY 30, Amdt
                                                                                1A
24-May-18........................  SD               Huron...............  Huron Rgnl..........          8/7328         4/11/18  RNAV (GPS) RWY 12, Orig
24-May-18........................  PA               New Castle..........  New Castle Muni.....          8/7350          4/6/18  NDB RWY 23, Amdt 3B
24-May-18........................  NE               Pender..............  Pender Muni.........          8/7569         4/11/18  Takeoff Minimums and
                                                                                Obstacle DP, Orig

24-May-18........................  TX               Mexia...............  Mexia-Limestone Co..          8/7712          4/6/18  NDB-A, Amdt 4
24-May-18........................  TX               Mexia...............  Mexia-Limestone Co..          8/7713          4/6/18  RNAV (GPS) RWY 36, Orig-
                                                                                A
24-May-18........................  OH               New Lexington.......  Perry County........          8/7718          4/6/18  VOR/DME RWY 26, Amdt 2
24-May-18........................  OH               New Lexington.......  Perry County........          8/7719          4/6/18  RNAV (GPS) RWY 26, Orig-
                                                                                A
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8099         4/11/18  ILS OR LOC RWY 6, Amdt
                                                                                29G
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8101         4/11/18  COPTER ILS OR LOC RWY 6,
                                                                                Amdt 1F
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8102         4/11/18  ILS OR LOC RWY 19, Orig-
                                                                                A
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8105         4/11/18  RNAV (GPS) X RWY 6, Amdt
                                                                                2
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8106         4/11/18  RNAV (GPS) Y RWY 6, Amdt
                                                                                2B
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8121         4/11/18  VOR/DME RWY 6, Orig-D
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/8122         4/11/18  VOR RWY 24, Orig-D
24-May-18........................  LA               Ruston..............  Ruston Rgnl.........          8/8418          4/6/18  NDB RWY 18, Orig-D
24-May-18........................  LA               Ruston..............  Ruston Rgnl.........          8/8420          4/6/18  RNAV (GPS) RWY 18, Orig-
                                                                                A
24-May-18........................  LA               Ruston..............  Ruston Rgnl.........          8/8424          4/6/18  RNAV (GPS) RWY 36, Orig-
                                                                                A
24-May-18........................  MA               Hyannis.............  Barnstable Muni-              8/8563         4/11/18  ILS OR LOC RWY 15, Amdt
                                                                           Boardman/Polando                                      5
                                                                           Field.
24-May-18........................  MA               Hyannis.............  Barnstable Muni-              8/8564         4/11/18  RNAV (GPS) RWY 15, Orig-
                                                                           Boardman/Polando                                      A
                                                                           Field.
24-May-18........................  WI               Milwaukee...........  Lawrence J Timmerman          8/9042          4/9/18  RNAV (GPS) RWY 4L, Orig-
                                                                                B
24-May-18........................  WI               Milwaukee...........  Lawrence J Timmerman          8/9044          4/9/18  RNAV (GPS) RWY 15L, Orig-
                                                                                B
24-May-18........................  WI               Milwaukee...........  Lawrence J Timmerman          8/9051          4/9/18  RNAV (GPS) RWY 22R, Orig-
                                                                                C
24-May-18........................  NJ               Teterboro...........  Teterboro...........          8/9174         4/13/18  VOR/DME-B, Amdt 2D
24-May-18........................  WI               Milwaukee...........  Lawrence J Timmerman          8/9495          4/9/18  VOR RWY 4L, Amdt 9B
24-May-18........................  WI               Milwaukee...........  Lawrence J Timmerman          8/9497          4/9/18  LOC RWY 15L, Amdt 6B
24-May-18........................  MN               Mora................  Mora Muni...........          8/9655          4/6/18  NDB RWY 35, Orig
24-May-18........................  MN               Mora................  Mora Muni...........          8/9656          4/6/18  RNAV (GPS) RWY 35, Orig-
                                                                                A
24-May-18........................  MN               Mora................  Mora Muni...........          8/9657          4/6/18  Takeoff Minimums and
                                                                                Obstacle DP, Orig
24-May-18........................  IA               Decorah.............  Decorah Muni........          8/9849          4/6/18  RNAV (GPS) RWY 11, Orig-
                                                                                C
--------------------------------------------------------------------------------------------------------------------------------------------------------

[FR Doc. 2018-09565 Filed 5-7-18; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 79, Number 165 (Tuesday, August 26, 2014)]
[Notices]
[Page 50986]
[FR Doc No: 2014-20071]

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DEPARTMENT OF TRANSPORTATION

Pipeline and Hazardous Materials Safety Administration

Office of Hazardous Materials Safety; Notice of Applications for
Modification of Special Permit

AGENCY: Pipeline and Hazardous Materials Safety Administration (PHMSA),
DOT.

ACTION: List of Applications for Modification of Special Permits.

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

SUMMARY: In accordance with the procedures governing the application
for, and the processing of, special permits from the Department of
Transportation's Hazardous Material Regulations (49 CFR Part 107,
Subpart B), notice is hereby given that the Office of Hazardous
Materials Safety has received the applications described herein. This
notice is abbreviated to expedite docketing and public notice. Because
the sections affected, modes of transportation, and the nature of
application have been shown in earlier Federal Register publications,
they are not repeated here. Requests for modification of special
permits (e.g. to provide for additional hazardous materials, packaging
design changes, additional mode of transportation, etc.) are described
in footnotes to the application number. Application numbers with the
suffix ``M'' denote a modification request. These appEcations have been
separated from the new application for special permits to facilitate
processing.

DATES: Comments must be received on or before September 10, 2014.
    Address Comments To: Record Center, Pipeline and Hazardous
Materials Safety Administration, U.S. Department of Transportation,
Washington, DC 20590.
    Comments should refer to the application number and be submitted in
triplicate. If confirmation of receipt of comments is desired, include
a self-addressed stamped postcard showing the special permit number.

FOR FURTHER INFORMATION CONTACT: Copies of the applications are
available for inspection in the Records Center, East Building, PHH-30,
1200 New Jersey Avenue Southeast, Washington DC or at http://regulations.gov.
    This notice of receipt of applications for modification of special
permit is published in accordance with Part 107 of the Federal
hazardous materials transportation law (49 U.S.C. 5117(b); 49 CFR
1.53(b)).

    Issued in Washington, DC, on August 18, 2014.
Donald Burger,
Chief, General Approvals and Permits.

------------------------------------------------------------------------
   Application                      Regulation(s)     Nature of special
   Docket No.        Applicant         affected        permits thereof
------------------------------------------------------------------------
                      Modification Special Permits
------------------------------------------------------------------------
8451-M..........  Special          49 CFR 173.320,  To modify the
                   Devices, Inc.    173.54(a),       special permit to
                   Mesa, AR.        173.56 (b),      authorize forbidden
                                    173.57,          explosives.
                                    173.58, and
                                    173.60.
11150-M.........  Maine State      49 CFR 172.101   To modify the
                   Ferry Service    and 172.301(c).  special permit to
                   Augusta, ME.                      authorize cylinders
                                                     having a water
                                                     capacity exceeding
                                                     100 pounds.
11536-M.........  Boeing Company,  49 CFR 173.102,  To modify the
                   The Los          Spec. Prov.      special permit to
                   Angeles, CA.     101,             authorize new
                                    173.24(g),       shipping and
                                    173.62,          storage containers.
                                    173.185,
                                    173.202;
                                    173.211, and
                                    173.304.
12661-M.........  UPS, Inc.        49 CFR 172.202,  To modify the
                   Atlanta, GA.     172.203(c),      special permit to
                                    (k) and (m),     authorize Division
                                    172.301,         6.2 materials.
                                    172.400, and
                                    172.302(c).
15747-M.........  UPS, Inc.        49 CFR           To modify the
                   Atlanta, GA.     177.817(a),      special permit to
                                    177.817(e),      authorize Division
                                    172.606(b),      6.2 materials.
                                    and 172.203(a).
16153-M.........  Trailers y       49 CFR 178.345-  To modify the
                   Tanques de       7(d).            special permit to
                   Aluminio S.A.                     authorize less
                   de C.V. Mexico.                   restrictive
                                                     inspection
                                                     requirements.
------------------------------------------------------------------------

[FR Doc. 2014-20071 Filed 8-25-14; 8:45 am]
BILLING CODE 4909-60-M


[Federal Register Volume 81, Number 240 (Wednesday, December 14, 2016)]
[Notices]
[Pages 90390-90391]
[FR Doc No: 2016-29932]

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SECURITIES AND EXCHANGE COMMISSION

[Investment Company Act Release No. 32384; File No. 812-14543]

ALAIA Market Linked Trust and Beech Hill Securities, Inc.; Notice
of Application

December 8, 2016.
AGENCY: Securities and Exchange Commission (``Commission'').

ACTION: Notice of an application for an order under section 12(d)(1)(J)
of the Investment Company Act of 1940 (the ``Act'') for an exemption
from sections 12(d)(1)(A), (B), and (C) of the Act and under sections
6(c) and 17(b) of the Act for an exemption from sections 17(a)(1) and
(2) of the Act. The requested order would permit certain registered
unit investment trusts (``UITs'') to acquire shares of certain
registered open-end investment companies, registered closed-end
investment companies and registered UITs (collectively, the
``Underlying Funds'') that are within and outside the same group of
investment companies as the acquiring

UITs, in excess of the limits in section 12(d)(1) of the Act.

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

Applicants:  ALAIA Market Linked Trust (the ``Trust''), a UIT that is
registered under the Act, and Beech Hill Securities, Inc. (``BHSI''), a
New York corporation registered as a broker-dealer under the Securities
Exchange Act of 1934 (the ``Exchange Act'').

DATES: Filing Dates: The application was filed on September 3, 2015 and
amended on January 15, 2016, October 17, 2016 and November 22, 2016.

Hearing or Notification of Hearing:  An order granting the requested
relief will be issued unless the Commission orders a hearing.
Interested persons may request a hearing by writing to the Commission's
Secretary and serving applicants with a copy of the request, personally
or by mail. Hearing requests should be received by the Commission by
5:30 p.m. on January 3, 2017 and should be accompanied by proof of
service on the applicants, in the form of an affidavit, or, for
lawyers, a certificate of service. Pursuant to Rule 0-5 under the Act,
hearing requests should state the nature of the writer's interest, any
facts bearing upon the desirability of a hearing on the matter, the
reason for the request, and the issues contested. Persons who wish to
be notified of a hearing may request notification by writing to the
Commission's Secretary.

ADDRESSES:  Secretary, U.S. Securities and Exchange Commission, 100 F
Street NE., Washington, DC 20549-1090. Applicants: ALAIA Market Linked
Trust, 10 Corbin Drive, Darien, CT 06820, Beech Hill Securities, Inc.,
880 3rd Avenue, 16th Floor, New York, NY 10022-4730.

FOR FURTHER INFORMATION CONTACT:  Deepak T. Pai, Senior Counsel, at
(202) 551-6876 or Mary Kay Frech, Branch Chief, at<PHONE_NUMBER>
(Division of Investment Management, Chief Counsel's Office).

SUPPLEMENTARY INFORMATION: The following is a summary of the
application. The complete application may be obtained via the
Commission's Web site by searching for the file number, or for an
applicant using the Company name box, at http://www.sec.gov/search/search.htm, or by calling<PHONE_NUMBER>.

Summary of the Application

    1. Applicants request an order to permit (a) a Series \1\ to
acquire shares of Underlying Funds \2\ in excess of the limits in
sections 12(d)(1)(A) and (C) of the Act and (b) the Underlying Funds
that are registered open-end investment companies, their principal
underwriters and any broker or dealer registered under the Exchange Act
to sell shares of the Underlying Funds to the Series in excess of the
limits in section 12(d)(1)(B) of the Act.\3\ Applicants also request an
order of exemption under sections 6(c) and 17(b) of the Act from the
prohibition on certain affiliated transactions in section 17(a) of the
Act to the extent necessary to permit the Underlying Funds to sell
their shares to, and redeem their shares from, the Series.\4\
Applicants state that such transactions will be consistent with the
policies of each Series and each Underlying Fund and with the general
purposes of the Act and will be based on the net asset values of the
Underlying Funds.
---------------------------------------------------------------------------

    \1\ Applicants request that the order apply to each existing and
future series of the Trust and to any future registered UIT and
series thereof sponsored by BHSI or an entity controlling,
controlled by or under common control with BHSI (the ``Series'').
    \2\ Certain of the Underlying Funds may be registered as an
open-end investment company or a UIT, but have received exemptive
relief from the Commission to permit their shares to be listed and
traded on a national securities exchange at negotiated prices and to
operate as exchange-traded funds (``ETFs'').
    \3\ Applicants do not request relief for the Series to invest in
reliance on the order in closed-end investment companies that are
not listed and traded on a national securities exchange.
    \4\ A Series generally would purchase and sell shares of an
Underlying Fund that operates as an ETF through secondary market
transactions rather than through principal transactions with the
Underlying Fund. Applicants nevertheless request relief from section
17(a) to permit a Series to purchase or redeem shares from the ETF.
A Series will purchase and sell shares of an Underlying Fund that is
a closed-end fund through secondary market transactions at market
prices rather than through principal transactions with the closed-
end fund. Accordingly, applicants are not requesting section 17(a)
relief with respect to transactions in shares of closed-end funds.
---------------------------------------------------------------------------

    2. Applicants agree that any order granting the requested relief
will be subject to the terms and conditions stated in the application.
Such terms and conditions are designed to, among other things, help
prevent any potential (i) undue influence over an Underlying Fund that
is not in the same ``group of investment companies'' as the UIT through
control or voting power, or in connection with certain services,
transactions, and underwritings, (ii) excessive layering of fees, and
(iii) overly complex fund structures, which are the concerns underlying
the limits in sections 12(d)(1)(A), (B), and (C) of the Act.
    3. Section 12(d)(1)(J) of the Act provides that the Commission may
exempt any person, security, or transaction, or any class or classes of
persons, securities, or transactions, from any provision of section
12(d)(1) if the exemption is consistent with the public interest and
the protection of investors. Section 17(b) of the Act authorizes the
Commission to grant an order permitting a transaction otherwise
prohibited by section 17(a) if it finds that (a) the terms of the
proposed transaction are fair and reasonable and do not involve
overreaching on the part of any person concerned; (b) the proposed
transaction is consistent with the policies of each registered
investment company involved; and (c) the proposed transaction is
consistent with the general purposes of the Act. Section 6(c) of the
Act permits the Commission to exempt any persons or transactions from
any provision of the Act if such exemption is necessary or appropriate
in the public interest and consistent with the protection of investors
and the purposes fairly intended by the policy and provisions of the
Act.

    For the Commission, by the Division of Investment Management,
pursuant to delegated authority.
 Robert W. Errett,
Deputy Secretary.
[FR Doc. 2016-29932 Filed 12-13-16; 8:45 am]
 BILLING CODE 8011-01-P