follows:

Sec.  391.23  Investigation and inquiries.

    (a) * * *
    (1) An inquiry, within 30 days of the date the driver's employment
begins, to each driver's licensing authority where the driver held or
holds a motor vehicle operator's license or permit during the preceding
3 years to obtain that driver's motor vehicle record.
* * * * *
    (b) A copy of the motor vehicle record(s) obtained in response to
the inquiry or inquiries to each driver's licensing authority required
by paragraph (a)(1) of this section must be placed in the driver
qualification file within 30 days of the date the driver's employment
begins and be retained in compliance with Sec.  391.51. If no motor
vehicle record is received from a driver's licensing authority required
to submit this response, the motor carrier must document a good faith
effort to obtain such information. The inquiry to a driver's licensing
authority must be made in the form and manner each authority
prescribes.
* * * * *

0
10. Amend Sec.  391.25 by revising paragraph (a) to read as follows:

Sec.  391.25  Annual inquiry and review of driving record.

    (a) Except as provided in subpart G of this part, each motor
carrier shall, at least once every 12 months, make an inquiry to obtain
the motor vehicle record of each driver it employs, covering at least
the preceding 12 months, to each driver's licensing authority where the
driver held a commercial motor vehicle operator's license or permit
during the time period.
* * * * *

Sec.  391.27  [Removed and Reserved]

0
11. Remove and reserve Sec.  391.27.

0
12. Amend Sec.  391.51 as follows:
0
a. Revise paragraphs (b)(2) and (4);
0
b. Remove paragraph (b)(6) and redesignate paragraphs (b)(7) through
(9) as paragraphs (b)(6) through (8), respectively;
0
c. Revise newly redesignated paragraph (b)(6)(iii);
0
d. Revise paragraph (d)(1);
0
e. Remove paragraph (d)(3) and redesignate paragraphs (d)(4) through
(6) as paragraphs (d)(3) through (5), respectively; and
0
f. Revise newly redesignated paragraph (d)(3).
    The revisions to read as follows:

Sec.  391.51  General requirements for driver qualification files.

* * * * *
    (b) * * *
    (2) A copy of the motor vehicle record received from each driver's
licensing authority pursuant to Sec.  391.23(a)(1);
* * * * *
    (4) The motor vehicle record received from each driver's licensing
authority to the annual driver record inquiry required by Sec.
391.25(a);
* * * * *
    (6) * * *
    (iii) If that driver obtained the medical certification based on
having obtained a medical variance from FMCSA, the motor carrier must
also include a copy of the medical variance documentation in the driver
qualification file in accordance with paragraph (b)(7) of this section;
* * * * *
    (d) * * *
    (1) The motor vehicle record received from each driver's licensing
authority to the annual driver record inquiry required by Sec.
391.25(a);
* * * * *
    (3) The medical examiner's certificate required by Sec.  391.43(g),
a legible copy of the certificate, or, for CDL drivers, any CDLIS MVR
obtained as required by paragraph (b)(6)(ii) of this section;
* * * * *

0
13. Amend Sec.  391.63 as follows:
0
a. Revise paragraphs (a)(3) and (4);
0
b. Remove paragraph (a)(5); and
0
c. Revise the first sentence of paragraph (b).
    The revisions to read as follows:

Sec.  391.63  Multiple-employer drivers.

    (a) * * *
    (3) Perform the annual driving record inquiry required by Sec.
391.25(a); or
    (4) Perform the annual review of the person's driving record
required by Sec.  391.25(b).
    (b) Before a motor carrier permits a multiple-employer driver to
drive a commercial motor vehicle, the motor carrier must obtain the
driver's name, the driver's social security number, and the
identification number, type, and issuing driver's licensing authority
of the driver's commercial motor vehicle operator's license. * * *

0
14. Amend Sec.  391.67 by revising paragraph (a) to read as follows:

Sec.  391.67  Farm vehicle drivers of articulated commercial motor
vehicles.

* * * * *
    (a) Section 391.11(b)(1) and (7) (relating to general
qualifications of drivers);
* * * * *

0
15. Amend Sec.  391.68 by revising paragraph (a) to read as follows:

Sec.  391.68  Private motor carrier of passengers (nonbusiness).

* * * * *
    (a) Section 391.11(b)(1) and (7) (relating to general
qualifications of drivers);
* * * * *

    Issued under authority delegated in 49 CFR 1.87.
Robin Hutcheson,
Acting Administrator.
[FR Doc. 2022-04930 Filed 3-8-22; 8:45 am]
BILLING CODE 4910-EX-P


[Federal Register Volume 87, Number 44 (Monday, March 7, 2022)]
[Rules and Regulations]
[Pages 12571-12574]
[FR Doc No: 2022-04694]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0699; Project Identifier AD-2020-01685-E;
Amendment 39-21959; AD 2022-05-08]
RIN 2120-AA64

Airworthiness Directives; General Electric Company Turbofan
Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain General Electric Company (GE) CF34-10E model turbofan engines.
This AD was prompted by a manufacturer investigation that revealed
Teflon material in the A-sump oil strainer (strainer assembly) screen
after several reports of in-flight shutdowns (IFSDs) and unscheduled
engine removals (UERs). This AD requires initial and repetitive visual
inspections of the strainer assembly screen. As a terminating action to
the initial and repetitive visual inspections, this AD requires the
replacement of the stationary oil seal at the No. 1 forward bearing.
The FAA is issuing this AD to address the unsafe condition on these
products.

DATES: This AD is effective April 11, 2022.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 11,
2022.

ADDRESSES: For service information identified in this final rule,
contact General Electric Company, GE Aviation, Room 285, 1 Neumann Way,
Cincinnati, OH 45215; phone:<PHONE_NUMBER>; email:
[email protected]; website: https://www.ge.com. You may view
this service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803.
For information on the availability of this material at the FAA, call
(817) 222-5110. It is also available at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0699.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0699; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this final rule, any
comments received, and other information. The address for Docket
Operations is U.S. Department of Transportation, Docket Operations, M-
30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue
SE, Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Scott Stevenson, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803;
phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
[email protected].

SUPPLEMENTARY INFORMATION:

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain GE CF34-10E2A1,
CF34-10E5, CF34-10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-
10E7-B (CF34-10E) model turbofan engines. The NPRM published in the
Federal Register on August 24, 2021 (86 FR 47264). The NPRM was
prompted by a manufacturer investigation that revealed Teflon material
in the strainer assembly screen after several reports of IFSDs and UERs
on airplanes operating with GE CF34-10E5, CF34-10E5A1, CF34-10E6, and
CF34-10E7 model turbofan engines. After investigation, the manufacturer
determined that the failures were the result of Teflon oil seals
disbonding from the aluminum housing when used with either high thermal
stability (HTS) or high performance capability (HPC) oils. The
stationary oil seal deterioration resulted from the failure of the
bonding adhesive, known as EA9658, which does not have the high
temperature capabilities as designed and is negatively impacted by the
use of HTS or HPC oils. This deterioration results in Teflon particles
collecting in the strainer assembly. The manufacturer determined that
CF34-10E2A1, CF34-10E6A1, and CF34-10E7-B model turbofan engines are
subject to the same unsafe condition. In the NPRM, the FAA proposed to
require initial and repetitive visual inspections of the strainer
assembly screen. As a terminating action to the initial and repetitive
visual inspections, the FAA proposed to require the replacement of the
stationary oil seal, part number (P/N) B1316-00453 or P/N B1316-01274,
installed at the No. 1 forward bearing. The FAA is issuing this AD to
address the unsafe condition on these products.

Discussion of Final Airworthiness Directive

Comments

    The FAA received comments from four commenters. The commenters were
the Air Line Pilots Association, International (ALPA), GE, Helvetic
Airways AG (Helvetic Airways), and JetBlue Airways (JetBlue). The
following presents the comments received on the NPRM and the FAA's
response to each comment.

Request To Change the Applicability

    GE, Helvetic Airways, and JetBlue requested that the FAA change
paragraph (c), Applicability, of this AD to align with GE CF34-10E
Service Bulletin (SB) 72-0365 R04, dated April 27, 2021 (GE CF34-10E SB
72-0365 R04). GE specifically requested that the FAA include language
that specifies the timeframe (after September 2014) to

identify which stationary oil seals have adhesive EA9658 and are
subject to the disbonding failure mode. GE and JetBlue noted that
paragraph (c), Applicability, of the NPRM differs from GE CF34-10E SB
72-0365 R04, as it does not identify stationary oil seal, P/N B1316-
00453 or P/N B1316-01274, replaced or repaired after September 2014,
which is when the EA9658 adhesive was introduced to the field. GE and
JetBlue commented that the NPRM, as written, would apply to all
stationary oil seals, regardless of when they were manufactured or
repaired. Helvetic Airways noted that paragraph (c), Applicability, of
the NPRM does not account for the population of affected stationary oil
seals, as identified in paragraph A., Effectivity, of GE CF34-10E SB
72-0365 R04.
    In response to these comments, the FAA updated paragraph (c),
Applicability, of this AD to specify this AD applies to GE CF34-10E
model turbofan engines with a stationary oil seal, P/N B1316-00453 or
P/N B1316-01274, installed at the No. 1 forward bearing, that has been
repaired, overhauled, or entered into service after August 2014, and
used HTS oil or HPC oil for 56 flight hours or more during the life of
the stationary oil seal.

Request To Clarify the Applicability by Engine Serial Number

    GE suggested that the FAA revise paragraph (c), Applicability, of
this AD to include the list of engine serial numbers (ESNs), 424714
through 424892, as an additional but alternate approach to identify
affected CF34-10E engines.
    The FAA notes that the list of ESNs includes those engines that
were produced with the affected stationary oil seal. Those new-make
engines are included in paragraph (c), Applicability, of this AD by
referencing the stationary oil seal, P/N B1316-00453 or P/N B1316-
01274, which entered service after August 2014. The FAA did not change
this AD as a result of this comment.

Request To Update Compliance Time

    GE requested that the FAA update paragraph (g)(1)(i) of the NPRM to
remove ``at the next engine shop visit.'' GE reasoned that the intent
of GE CF34-10E SB 72-0365 R04 is to perform the inspection on-wing
without removing the engine.
    In response to GE's comment, the FAA has removed ``at the next
engine shop visit'' and combined paragraphs (g)(1)(i) and (ii) of the
NPRM into one paragraph, (g)(1) of this AD, to eliminate reference to
an engine shop visit.

Request To Update Definition

    GE requested that the FAA update paragraph (i), Definition, of this
AD to indicate that a part eligible for installation is a stationary
oil seal with a P/N other than P/N B1316-00453 or P/N B1316-001274 and
with FM57 adhesive. GE reasoned that there could be room for
interpretation as to what P/N other than B1316-00453 and P/N B1316-
01274 could be in the future, especially if the manufacturer redesigns
the stationary oil seal with a new adhesive and a new failure mode is
introduced.
    The FAA disagrees with updating the definition of a part eligible
for installation in paragraph (i) of this AD to include a reference to
FM57 adhesive. The FAA cannot define a part eligible for installation
based on future redesigns by the manufacturer. The FAA may consider
future rulemaking if a new failure mode is discovered. The FAA did not
change this AD as a result of this comment.

Request To Update Service Information or Allow for Credit

    GE requested that the FAA revise paragraph (g)(1) of this AD to
reference GE CF34-10E SB 72-0365 R04, R03, and R02. GE commented that
paragraph (g)(1) of the NPRM references GE CF34-10E SB 72-0365 R04 to
comply with the AD; however, some operators may have complied with
earlier revisions of the service bulletin. GE reasoned that paragraph
3.A.(1)(d) of GE CF34-10E SB 72-0365 R04, R03, R02 are identical.
    JetBlue requested that the FAA update this AD to allow credit for
inspections performed using previous revisions of GE CF34-10E SB 72-
0365. JetBlue commented that the NPRM specifically references GE CF34-
10E SB 72-0365 R04. JetBlue reasoned that, in addition to R04 of GE
CF34-10E SB 72-0365, they performed repetitive inspections in
accordance with R03 and R02.
    This AD does not mandate that operators use GE CF34-10E SB 72-0365
R04 to perform the visual inspections. GE CF34-10E SB 72-0365 R04 is
referenced in paragraph (g), Required Actions, of this AD as guidance
to perform the visual inspections of the strainer assembly screen.
Therefore, if operators used earlier versions of the service
information to perform the visual inspections, they would be in
compliance with the requirements in paragraph (g) of this AD. Regarding
the comment requesting that this AD include credit for pervious actions
using earlier versions of the service information, the FAA notes that
this change is unnecessary. Paragraph (f) of this AD mandates
compliance with the required actions, unless already done. The FAA did
not change this AD as a result of this comment.

Support for the AD

    ALPA expressed support for the AD as written.

Conclusion

    The FAA reviewed the relevant data, considered any comments
received, and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these products. Except for minor editorial changes, and
any other changes described previously, this AD is adopted as proposed
in the NPRM. None of the changes will increase the economic burden on
any operator.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed GE CF34-10E Service Bulletin 72-0365 R04, dated
April 27, 2021. This service information specifies procedures for
performing a visual inspection and a borescope inspection of the
strainer assembly for Teflon particles. This service information is
reasonably available because the interested parties have access to it
through their normal course of business or by the means identified in
ADDRESSES.

Costs of Compliance

    The FAA estimates that this AD affects 46 engines installed on
airplanes of U.S. registry.
    The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per      Cost on U.S.
               Action                         Labor cost            Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspect the strainer assembly        1 work-hour x $85 per hour               $0             $85          $3,910
 screen.                              = $85.
Replace the stationary oil seal....  2 work-hours x $85 per hour           8,628           8,798         404,708
                                      = $170.
----------------------------------------------------------------------------------------------------------------

Authority for This Rulemaking

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

Regulatory Findings

    This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Will not affect intrastate aviation in Alaska, and
    (3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13   [Amended]

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

2022-05-08 General Electric Company: Amendment 39-21959; Docket No.
FAA-2021-0699; Project Identifier AD-2020-01685-E.

(a) Effective Date

    This airworthiness directive (AD) is effective April 11, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to General Electric Company (GE) CF34-10E2A1,
CF34-10E5, CF34-10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-
10E7-B model turbofan engines with a stationary oil seal, part
number (P/N) B1316-00453 or P/N B1316-01274, installed at the No. 1
forward bearing, that:
    (1) Has been repaired, overhauled, or entered into service after
August 2014; and
    (2) Has used high thermal stability oil or high performance
capability oil for 56 flight hours (FHs) or more during the life of
the stationary oil seal.

(d) Subject

    Joint Aircraft System Component (JASC) Code 7261, Turbine Engine
Oil System.

(e) Unsafe Condition

    This AD was prompted by investigation by the manufacturer that
revealed Teflon material in the A-sump oil strainer (strainer
assembly) screen after several reports of in-flight shutdowns and
unscheduled engine removals. The FAA is issuing this AD to prevent
failure of the stationary oil seal at the No. 1 forward bearing. The
unsafe condition, if not addressed, could result in failure of the
engine, in-flight shutdown, and loss of control of the airplane.

(f) Compliance

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

(g) Required Actions

    (1) Before the stationary oil seal accumulates 100 FHs after the
effective date of this AD, or within 100 FHs of the stationary oil
seal accumulating 2,250 FHs since new, whichever occurs later,
perform an initial visual inspection of the strainer assembly screen
for Teflon material. Guidance on performing the visual inspection of
the strainer assembly screen can be found in the Accomplishment
Instructions, paragraph 3.A.(1)(d), of GE CF34-10E Service Bulletin
(SB) 72-0365 R04, dated April 27, 2021.
    (2) Thereafter, within the following compliance times, repeat
the visual inspection of the strainer assembly screen required by
paragraph (g)(1) of this AD:
    (i) For an affected stationary oil seal having accumulated 2,250
to 7,000 FHs since new at the time of the last inspection, repeat
the visual inspection every 750 FHs.
    (ii) For an affected stationary oil seal having accumulated
7,001 to 10,000 FHs since new at the time of the last inspection,
repeat the visual inspection every 375 FHs.
    (iii) For an affected stationary oil seal having accumulated
more than 10,000 FHs since new at the time of the last inspection,
repeat the visual inspection every 100 FHs.
    (3) If, based on any inspection required by paragraph (g)(1) or
(2) of this AD, Teflon material is found in the strainer assembly
screen, before further flight, remove the stationary oil seal at the
No. 1 forward bearing from service and replace it with a part
eligible for installation.
    (4) Before an affected stationary oil seal accumulates 10,000
FHs since new or within 500 FHs after the effective date of this AD,
whichever occurs later, remove the stationary oil seal at the No. 1
forward bearing from service and replace it with a part eligible for
installation.

(h) Terminating Action

    Removal of the stationary oil seal, P/N B1316-00453 or P/N
B1316-01274, installed at the No. 1 forward bearing, and replacement
with a part eligible for installation, constitutes terminating
action for the initial and repetitive inspections required by
paragraphs (g)(1) and (2) of this AD.

(i) Definition

    For the purpose of this AD, a ``part eligible for installation''
is a stationary oil seal that has a P/N other than P/N B1316-00453
or P/N B1316-01274.

(j) Special Flight Permit

    A special flight permit may be issued in accordance with 14 CFR
21.197 and 21.199 to permit a non-revenue ferry flight, consisting
of no more than five cycles, to a location where the engine can be
removed from service for operators who are prohibited from further
flight due to Teflon material found in the strainer assembly screen
if operators perform the actions in Appendix--A, paragraph 4.A., of
GE CF34-10E SB 72-0365 R04, dated April 27, 2021, and the engine
still meets the criteria in paragraph 4.A. for flying an additional
five cycles. This ferry flight must be performed with only essential
flight crew, without passengers, and involve non-ETOPS operations.

(k) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, ECO Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or local Flight Standards District Office, as
appropriate. If sending information directly to the manager of the
certification office, send it to the attention of the person
identified in paragraph (l) of this AD. You may email your request
to [email protected].
    (2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.

(l) Related Information

    For more information about this AD, contact Scott Stevenson,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: (781)

238-7132; fax:<PHONE_NUMBER>; email: [email protected].

(m) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
    (i) GE CF34-10E Service Bulletin 72-0365 R04, dated April 27,
2021.
    (ii) [Reserved]
    (3) For service information identified in this AD, contact
General Electric Company, GE Aviation, Room 285, 1 Neumann Way,
Cincinnati, OH 45215; phone:<PHONE_NUMBER>; email:
[email protected]; website: https://www.ge.com.
    (4) You may view this service information at FAA, Airworthiness
Products Section, Operational Safety Branch, 1200 District Avenue,
Burlington, MA 01803. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>.
    (5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on February 18, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-04694 Filed 3-4-22; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 82, Number 164 (Friday, August 25, 2017)]
[Notices]
[Pages 40604-40606]
[FR Doc No: 2017-17999]

=======================================================================
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SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-81446; File No. SR-NASDAQ-2017-084]

Self-Regulatory Organizations; The NASDAQ Stock Market LLC;
Notice of Filing and Immediate Effectiveness of Proposed Rule Change To
Address the Application of Rule 11140 in Connection With the
Implementation of the Shortened Settlement Cycle (T+2) on September 5,
2017

August 21, 2017.
    Pursuant to Section 19(b)(1) of the Securities Exchange Act of 1934
(``Act''),\1\ and Rule 19b-4 thereunder,\2\ notice is hereby given that
on August 18, 2017, The NASDAQ Stock Market LLC (``Nasdaq'' or
``Exchange'') filed with the Securities and Exchange Commission
(``SEC'' or ``Commission'') the proposed rule change as described in
Items I and II, below, which Items have been prepared by the Exchange.
The Commission is publishing this notice to solicit comments on the
proposed rule change from interested persons.
---------------------------------------------------------------------------

    \1\ 15 U.S.C. 78s(b)(1).
    \2\ 17 CFR 240.19b-4.
---------------------------------------------------------------------------

I. Self-Regulatory Organization's Statement of the Terms of Substance
of the Proposed Rule Change

    The Exchange proposes to address the application of Rule 11140 as
it relates to

the ex-dividend date in connection with the implementation of the T+2
settlement cycle on September 5, 2017.
    No change to the text of Rule 11140 is required by this proposal.

II. Self-Regulatory Organization's Statement of the Purpose of, and
Statutory Basis for, the Proposed Rule Change

    In its filing with the Commission, the Exchange included statements
concerning the purpose of and basis for the proposed rule change and
discussed any comments it received on the proposed rule change. The
text of these statements may be examined at the places specified in
Item IV below. The Exchange has prepared summaries, set forth in
sections A, B, and C below, of the most significant aspects of such
statements.

A. Self-Regulatory Organization's Statement of the Purpose of, and the
Statutory Basis for, the Proposed Rule Change

1. Purpose
    The Exchange is proposing to address the application of Rule 11140
(Transactions in Securities ``Ex-Dividend,'' ``Ex-Rights'' or ``Ex-
Warrants'') as it relates to the ex-dividend date in connection with
the implementation of the trade date plus two business days (T+2)
settlement cycle on September 5, 2017.
    On September 28, 2016, following a recommendation by the securities
industry, the Commission proposed amending Exchange Act Rule 15c6-1(a)
\3\ to shorten the standard settlement cycle for most broker-dealer
transactions from trade date plus three business days (T+3) to T+2.\4\
The rationale for this proposal was that the shorter settlement cycle
would reduce the risks that arise from the value and number of
unsettled securities transactions prior to the completion of
settlement, including credit, market, and liquidity risk directly faced
by U.S. market participants.\5\ The SEC adopted the proposed changes to
Rule 15c6-1(a) on March 22, 2017.\6\
---------------------------------------------------------------------------

    \3\ 17 CFR 240.15c6-1(a).
    \4\ See Securities Exchange Act Release No. 78962 (September 28,
2016), 81 FR 69240 (October 5, 2016) (Amendment to Securities
Transaction Settlement Cycle) (File No. S7-22-16).
    \5\ Id.
    \6\ See Securities Exchange Act Release No. 80295 (March 22,
2017), 82 FR 15564 (March 29, 2017) (File No. S7-22-16).
---------------------------------------------------------------------------

    In connection with the amendments to Rule 15c6-1(a) and the
adoption of the shortened settlement cycle, Nasdaq submitted a proposed
rule change implementing the new settlement cycle and making
corresponding changes to its applicable rules, including Rule
11140(b).\7\
---------------------------------------------------------------------------

    \7\ See Securities Exchange Act Release No. 79687 (December 23,
2016), 81 FR 96545 (December 30, 2016) (Order approving SR-NASDAQ-
2016-183).
---------------------------------------------------------------------------

    The industry and self-regulatory organizations (``SROs''),
including The Depository Trust Company (``DTC''), which processes
corporate action events, have raised concern that the September 5, 2017
industry-wide transition date from T+3 to T+2 will result in September
7, 2017 being a ``double'' settlement date for trades that occur on
September 1, 2017 (under T+3 and reflecting the Labor Day holiday on
September 4, 2017) and trades that occur on September 5, 2017 (under
T+2), which generally will result in investors who trade on either date
being deemed a record holder of September 7, 2017. In order to avoid
confusion about the proper settlement date and to coordinate with other
SROs, Nasdaq and the other SROs have agreed that no securities will be
ex-dividend on September 5, 2017.
    The Exchange is therefore now proposing to address the application
of Rule 11140(b) as it relates to the ex-dividend date in connection
with the implementation of the T+2 settlement cycle on September 5,
2017.
    The ex-dividend date is the date on which a security is first
traded without the right to receive a distribution of cash, stock or
warrants. Rule 11140(b)(1) establishes the ``ex-dividend date'' for
``normal'' distributions of cash, stock or warrants. The rule provides
that, in respect to cash dividends or distributions, or stock
dividends, and the issuance or distribution of warrants, which are less
than 25% of the value of the subject security, if the definitive
information is received sufficiently in advance of the record date,\8\
the date designated as the ``ex-dividend date'' shall be the second
business day preceding the record date if the record date falls on a
business day, or the third business day preceding the record date if
the record date falls on a day designated by Nasdaq Regulation as a
non-delivery date.
---------------------------------------------------------------------------

    \8\ The record date is ``the date fixed by the trustee,
registrar, paying agent or issuer for the purpose of determining the
holders of equity securities, bonds, similar evidences of
indebtedness or unit investment trust securities entitled to receive
dividends, interest or principal payments or any other
distributions.'' See Rule 11120(e).
---------------------------------------------------------------------------

    Rule 11140(b)(2) establishes the ex-dividend date with respect to
``large'' distributions, e.g., cash dividends or distributions, stock
dividends and/or splits, and the distribution of warrants, which are
25% or greater of the value of the subject security. In this case, the
ex-dividend date is the first business day following the payable
date.\9\
---------------------------------------------------------------------------

    \9\ The payable date is the date on which a declared stock
dividend is scheduled to be paid.
---------------------------------------------------------------------------

    Consistent with the compliance date of the amendments to Rule 15c6-
1(a), the securities industry has adopted Tuesday, September 5, 2017 as
the implementation date of the T+2 settlement cycle.\10\ With the
implementation of the T+2 settlement cycle, the ex-dividend date for
``normal'' distributions pursuant to Rule 11140(b)(1) will be the first
business day before the record date.\11\ Accordingly, Nasdaq proposes
to interpret Rule 11140(b)(1) so that the first record date to which
this new ex-dividend date rationale will be applied will be Thursday,
September 7, 2017. During the implementation of the T+2 settlement
cycle, the ``regular'' ex-dividend dates will be as follows:
---------------------------------------------------------------------------

    \10\ See Securities Exchange Act Release No. 80295 (March 22,
2017), 82 FR 15564 (March 29, 2017) (File No. S7-22-16).
    \11\ See Securities Exchange Act Release No. 79687 (December 23,
2016), 81 FR 96545 (December 30, 2016).

Record Date 9/1/2017 Ex date 8/30/2017
Record Date 9/5/2017 Ex date 8/31/2017
Record Date 9/6/2017 Ex date 9/1/2017
Record Date 9/7/2017 Ex date 9/6/2017 \12\
---------------------------------------------------------------------------

    \12\ September 4, 2017 is Labor Day and not a business day.

    As described above, the ex-dividend date for ``large''
distributions under Rule 11140(b) is the first business day following
the payable date. This provision was not amended in connection with the
adoption of the T+2 settlement cycle. In order to ensure that no
securities will be ex-dividend on September 5, 2017 for purposes of
``large'' distributions, Nasdaq similarly proposes to interpret Rule
11140(b) so that, if an issuer sets September 1, 2017 as the payment
date for a large distribution, the ex-dividend date would be September
6, 2017, not September 5, 2017.
    Nasdaq notes that it previously issued an Issuer Alert addressing
the application of the T+2 implementation date on Rule 11140(b).\13\
---------------------------------------------------------------------------

    \13\ See Nasdaq Issuer Alert 2017-001 (Changes to Ex-dividend
Procedures Effective September 5, 2017 to Accommodate T+2
Settlement), available at http://nasdaq.cchwallstreet.com/nasdaq/pdf/nasdaq-issalerts/2017/2017-001.pdf.
---------------------------------------------------------------------------

2. Statutory Basis
    The Exchange believes that its proposal is consistent with Section
6(b) of the Act,\14\ in general, and furthers the objectives of Section
6(b)(5) of the Act,\15\

in particular, in that it is designed to promote just and equitable
principles of trade, to remove impediments to and perfect the mechanism
of a free and open market and a national market system, and, in general
to protect investors and the public interest. In the interest of
minimizing potential confusion about proper settlement in connection
with the implementation of the T+2 settlement cycle on September 5,
2017, the SROs have agreed that no securities will be ex-dividend on
September 5, 2017. This proposal is consistent with the Act because it
interprets the application of Rule 11140(b) on September 5, 2017 so
that neither ``normal'' nor ``large'' distributions will be ex-divided
on that date, thereby interpreting the application of the Rule on that
date while minimizing the possibility of additional operational
complexity and potential confusion about settlement that could occur if
the rule were interpreted differently.
---------------------------------------------------------------------------

    \14\ 15 U.S.C. 78f(b).
    \15\ 15 U.S.C. 78f(b)(5).
---------------------------------------------------------------------------

B. Self-Regulatory Organization's Statement on Burden on Competition

    The Exchange does not believe that the proposed rule change will
impose any burden on competition not necessary or appropriate in
furtherance of the purposes of the Act. As noted above, the SROs,
including DTC, have collectively agreed that no securities will be ex-
dividend on September 5, 2017 in order to minimize confusion about
proper settlement. Accordingly, the proposed rule change interprets the
application of Rule 11140(b) on September 5, 2017 so that neither
``normal'' nor ``large'' distributions will be ex-divided on that date.

C. Self-Regulatory Organization's Statement on Comments on the Proposed
Rule Change Received From Members, Participants, or Others

    No written comments were either solicited or received.

III. Date of Effectiveness of the Proposed Rule Change and Timing for
Commission Action

    Because the proposed rule change does not (i) significantly affect
the protection of investors or the public interest; (ii) impose any
significant burden on competition; and (iii) become operative for 30
days from the date on which it was filed, or such shorter time as the
Commission may designate, the proposed rule change has become effective
pursuant to Section 19(b)(3)(A) of the Act \16\ and Rule 19b-4(f)(6)
thereunder.\17\
---------------------------------------------------------------------------

    \16\ 15 U.S.C. 78s(b)(3)(A).
    \17\ 17 CFR 240.19b-4(f)(6). In addition, Rule 19b-4(f)(6)(iii)
requires the Exchange to give the Commission written notice of the
Exchange's intent to file the proposed rule change, along with a
brief description and text of the proposed rule change, at least
five business days prior to the date of filing of the proposed rule
change, or such shorter time as designated by the Commission. The
Exchange has satisfied this requirement.
---------------------------------------------------------------------------

    A proposed rule change filed under Rule 19b-4(f)(6) \18\ normally
does not become operative for 30 days after the date of filing.
However, pursuant to Rule 19b-4(f)(6)(iii),\19\ the Commission may
designate a shorter time if such action is consistent with the
protection of investors and the public interest. The Exchange has asked
the Commission to waive the 30-day operative delay so that the proposal
may become operative upon filing. The Exchange has stated that the
purpose of the proposed rule change is to minimize confusion about
proper settlement that may arise during the transition to the T+2
settlement cycle on September 5, 2017. The Commission believes that
waiving the 30-day operative delay is consistent with the protection of
investors and the public interest to avoid the confusion that could
arise in connection with the transition to the T+2 settlement cycle on
September 5, 2017, if normal or large distributions were to be ex-
dividend on that date. Accordingly, the Commission hereby waives the
30-day operative delay requirement and designates the proposed rule
change as operative upon filing.\20\
---------------------------------------------------------------------------

    \18\ 17 CFR 240.19b-4(f)(6).
    \19\ 17 CFR 240.19b-4(f)(6)(iii).
    \20\ For purposes only of waiving the 30-day operative delay,
the Commission has also considered the proposed rule's impact on
efficiency, competition, and capital formation. See 15 U.S.C.
78c(f).
---------------------------------------------------------------------------

    At any time within 60 days of the filing of the proposed rule
change, the Commission summarily may temporarily suspend such rule
change if it appears to the Commission that such action is necessary or
appropriate in the public interest, for the protection of investors, or
otherwise in furtherance of the purposes of the Act. If the Commission
takes such action, the Commission shall institute proceedings to
determine whether the proposed rule should be approved or disapproved.

IV. Solicitation of Comments

    Interested persons are invited to submit written data, views, and
arguments concerning the foregoing, including whether the proposed rule
change is consistent with the Act. Comments may be submitted by any of
the following methods:

Electronic Comments

     Use the Commission's Internet comment form (http://www.sec.gov/rules/sro.shtml); or
     Send an email to<EMAIL_ADDRESS>Please include
File Number SR-NASDAQ-2017-084 on the subject line.

Paper Comments

     Send paper comments in triplicate to Secretary, Securities
and Exchange Commission, 100 F Street NE., Washington, DC 20549-1090.

All submissions should refer to File Number SR-NASDAQ-2017-084. This
file number should be included on the subject line if email is used. To
help the Commission process and review your comments more efficiently,
please use only one method. The Commission will post all comments on
the Commission's Internet Web site (http://www.sec.gov/rules/sro.shtml). Copies of the submission, all subsequent amendments, all
written statements with respect to the proposed rule change that are
filed with the Commission, and all written communications relating to
the proposed rule change between the Commission and any person, other
than those that may be withheld from the public in accordance with the
provisions of 5 U.S.C. 552, will be available for Web site viewing and
printing in the Commission's Public Reference Room, 100 F Street NE.,
Washington, DC 20549, on official business days between the hours of
10:00 a.m. and 3:00 p.m. Copies of the filing also will be available
for inspection and copying at the principal office of the Exchange. All
comments received will be posted without change; the Commission does
not edit personal identifying information from submissions. You should
submit only information that you wish to make available publicly. All
submissions should refer to File Number SR-NASDAQ-2017-084, and should
be submitted on or before September 15, 2017.
---------------------------------------------------------------------------

    \21\ 17 CFR 200.30-3(a)(12).

    For the Commission, by the Division of Trading and Markets,
pursuant to delegated authority.\21\
Robert W. Errett,
Deputy Secretary.
[FR Doc. 2017-17999 Filed 8-24-17; 8:45 am]
 BILLING CODE 8011-01-P


[Federal Register Volume 83, Number 190 (Monday, October 1, 2018)]
[Rules and Regulations]
[Page 49302]
[FR Doc No: 2018-21367]

=======================================================================
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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

44 CFR Chapter I

Technical, Organizational and Conforming Amendments

CFR Correction

    In Title 44 of the Code of Federal Regulations, revised as of
October 1, 2017, make the following corrections:

0
1. On page 45, in Sec.  7.14, in paragraph (e), remove the word
``Director'' and add the word ``Administrator'' in its place.

0
2. On page 135, in Sec.  59.24, in paragraph (a), and on page 137, in
paragraph (f), remove the term ``the Administrator'' and add the term
``Federal Insurance Administrator'' in its place.

0
3. On page 285, in Sec.  151.11, in the introductory text, remove the
word ``Director'' and add the word ``Administrator'' in its place.

0
4. On page 286, in Sec.  151.12, in the last sentence of paragraph
(b)(2), remove the word ``Director'' and add the word ``Administrator''
in its place.

0
5. On page 319, in Sec.  206.2, in paragraph (a)(11), remove the word
``Director'' and add the word ``Administrator'' in its place.

0
6. On page 371, in Sec.  206.164, in paragraph (b), remove the word
``Director'' and add the word ``Administrator'' in its place.

0
7. On page 505, in Sec.  332.2, in paragraph (e)(2), remove the word
``Director'' and add the word ``Administrator'' in its place.

0
8. On page 516, in Sec.  350.9, in the last sentence of paragraph
(c)(3), remove the term ``Associate Director'' and add the term
``Deputy Administrator for the National Preparedness Directorate'' in
its place.

0
9. On page 518, in Sec.  350.12 in the introductory text of paragraph
(b), remove the term ``Regional Director's'' and add the term
``Regional Administrator's'' in its place.

[FR Doc. 2018-21367 Filed 9-28-18; 8:45 am]
 BILLING CODE 1301-00-D


[Federal Register Volume 80, Number 64 (Friday, April 3, 2015)]
[Rules and Regulations]
[Page 18144]
[FR Doc No: 2015-07472]

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ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 300

[EPA-HQ-SFUND-1991-006; FRL-9925-52-Region 8]

National Oil and Hazardous Substances Pollution Contingency Plan
National Priorities List

AGENCY: Environmental Protection Agency (EPA).

ACTION: Withdrawal of direct final rule.

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

SUMMARY: On February 5, 2015, the Environmental Protection Agency (EPA)
published a Notice of Intent to Delete and a direct final Notice of
Deletion for the Midvale Slag from the National Priorities List. The
EPA is withdrawing the Final Notice of Deletion due to adverse comments
that were received during the public comment period. After
consideration of the comments received, if appropriate, EPA will
publish a Notice of Deletion in the Federal Register based on the
parallel Notice of Intent to Delete and place a copy of the final
deletion package, including a Responsiveness Summary, if prepared, in
the Site repositories.

DATES: This withdrawal of the direct final action published February 5,
2015 (80 FR 6458) is effective as of April 3, 2015.

ADDRESSES: Information Repositories: Comprehensive information on the
Site, as well as the comments that we received during the comment
period, are available in the docket EPA-HQ-SFUND-1991-0006 accessed
through the http://www.regulations.gov Web site. Although listed in the
index, some information is not publicly available, e.g., CBI or other
information whose disclosure is restricted by statute. Certain other
material, such as copyrighted material, will be publicly available only
in hard copy. Publicly available docket materials are available
electronically at http://www.regulations.gov or in hard copy at Ruth
Tyler Branch Library, 8041 South Wood, Midvale, UT 84047; Phone: (801-
944-7641); Hours: M-Th: 9 a.m.-9 p.m.; Fri-Sat: 9:00 a.m.-5:30 p.m.

FOR FURTHER INFORMATION CONTACT: Erna Waterman, Remedial Project
Manager, U.S. Environmental Protection Agency, Region 8, Mail code:
8EPR-SR, 1595 Wynkoop Street, Denver, CO 80202-1129; Phone: (303) 312-
6762; Email<EMAIL_ADDRESS>You may contact Erna to request a
hard copy of publicly available docket materials.

List of Subjects in 40 CFR Part 300

    Environmental protection, Air pollution control, Chemicals,
Hazardous waste, Hazardous substances, Intergovernmental relations,
Penalties, Reporting and recordkeeping requirements, Superfund, Water
pollution control, Water supply.

    Dated: March 24, 2015.
Shaun L. McGrath,
Regional Administrator, Region 8.

    For the reasons set out in this document, 40 CFR part 300 is
amended as follows:

PART 300--NATIONAL OIL AND HAZARDOUS SUBSTANCES POLLUTION
CONTINGENCY PLAN

0
1. The authority citation for part 300 continues to read as follows:

    Authority:  33 U.S.C. 1321(c)(2); 42 U.S.C. 9601-9657; E.O.
13626, 77 FR 56749, 3 CFR, 2013 Comp., p.306; E.O. 12777, 56 FR
54757, 3 CFR, 1991 Comp., p.351; E.O. 12580, 52 FR 2923, 3 CFR, 1987
Comp., p.193.

0
2. Accordingly, the amendment to Table 1 of Appendix B to CFR part 300
to remove the entry ``UT'' ``Midvale Slag'' ``Midvale'' published
February 5, 2015 (80 FR 6458) is withdrawn as of April 3, 2015.
[FR Doc. 2015-07472 Filed 4-2-15; 8:45 am]
 BILLING CODE 6560-50-P


[Federal Register Volume 81, Number 38 (Friday, February 26, 2016)]
[Rules and Regulations]
[Pages 9754-9756]
[FR Doc No: 2016-03883]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-3704; Directorate Identifier 2016-NM-005-AD;
Amendment 39-18413; AD 2016-04-19]
RIN 2120-AA64

Airworthiness Directives; Airbus Defense and Space S.A. (Formerly
Known as Construcciones Aeronauticas, S.A.) Airplanes

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

ACTION: Final rule; request for comments.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all
Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, CN-
235-300, and C-295 airplanes. This AD requires a general visual
inspection of the rudder control system to confirm correct alignment
and installation of the adjustment device, and repair if necessary.
This AD was prompted by a report of disconnection of the kinematic
chain from the co-pilot rudder pedals to the rudder control bars
located under the cockpit floor; subsequent investigation revealed that
the failure was caused by disconnection of the pedal adjustment device
from the adjustment actuator. We are issuing this AD to detect and
correct incorrect alignment and incorrect installation of the
adjustment device, which could lead to loss of the rudder control from
the affected side and possibly result in reduced control of the
airplane.

DATES: This AD becomes effective March 14, 2016.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 14,
2016.
    We must receive comments on this AD by April 11, 2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to 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, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
    For service information identified in this final rule, contact
Airbus Defense and Space S.A., Services/Engineering Support, Avenida de
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax
+34 91 585 3127; email<EMAIL_ADDRESS>For
U.S. operators, email alternatively
<EMAIL_ADDRESS>You may view this referenced
service information at the FAA, Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, WA. For information on the availability of
this material at the FAA, call<PHONE_NUMBER>. It is also available on
the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2016-3704.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
3704; or in person at the Docket Operations office between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Operations office
(telephone<PHONE_NUMBER>) is in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive 2016-0012, dated January 14, 2016 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition on all Airbus Defense and
Space S.A. Model CN-235, CN-235-100, CN-235-200, CN-235-300, and C-295
airplanes. The MCAI states:

    An occurrence was reported involving disconnection of the
kinematic chain from the co-pilot rudder pedals to the rudder
control bars located under the cockpit floor. Subsequent
investigation revealed that the failure was caused by disconnection
of the pedal adjustment device from the adjustment actuator.
    This condition, if not detected and corrected, could lead to
loss of the rudder control from the affected side, possibly
resulting in reduced control of the aeroplane.
    To address this potential unsafe condition, Airbus Defence and
Space (Airbus D&S) issued Alert Operators Transmission (AOT) AOT-
CN235-27-0002 and AOT-C295-27-0001, as applicable to aeroplane
model, to provide inspection instructions.
    For the reasons described above, this [EASA] AD requires a one-
time general visual inspection (GVI) of the rudder control system
and correctness of the installation connection between the
adjustment actuators and the adjustment devices of the rudder pedals
and, depending on findings, accomplishment of applicable corrective
action(s).

You may examine the MCAI on the Internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2016-3704.

Related Service Information Under 1 CFR Part 51

    Airbus Defence and Space has issued AOT AOT-C295-27-0001, Revision
1, dated September 29, 2015; and AOT-CN235-27-0002, Revision 1, dated
September 22, 2015. The service information describes procedures for a
general visual inspection of the rudder control system to confirm
correct alignment and installation of the adjustment device. This
service information is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in the ADDRESSES section.

FAA's Determination and Requirements of This AD

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

FAA's Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because
incorrect alignment and

incorrect installation of the adjustment device could lead to loss of
the rudder control from the affected side and possibly result in
reduced control of the airplane. Therefore, we determined that notice
and opportunity for public comment before issuing this AD are
impracticable and that good cause exists for making this amendment
effective in fewer than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2016-3704; Directorate
Identifier 2016-NM-005-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 based on
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.

Costs of Compliance

    We estimate that this AD affects 29 airplanes of U.S. registry.
    We also estimate that it will take about 1 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $0 per product.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $2,465, or $85 per product.
    In addition, we estimate that any necessary follow-on actions will
take about 8 work-hours and require parts costing $177, for a cost of
$857 per product. We have no way of determining the number of aircraft
that might need these actions.

Authority for This Rulemaking

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

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13  [Amended]

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

2016-04-19 Airbus Defense and Space S.A. (Formerly Known as
Construcciones Aeronauticas, S.A.): Amendment 39-18413. Docket No.
FAA-2016-3704; Directorate Identifier 2016-NM-005-AD.

(a) Effective Date

    This AD becomes effective March 14, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus Defense and Space S.A. (Formerly known
as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-
235-200, CN-235-300, and C-295 airplanes, certificated in any
category, all manufacturer serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 27, Flight
Controls.

(e) Reason

    This AD was prompted by a report of disconnection of the
kinematic chain from the co-pilot rudder pedals to the rudder
control bars located under the cockpit floor; subsequent
investigation revealed that the failure was caused by disconnection
of the pedal adjustment device from the adjustment actuator. We are
issuing this AD to detect and correct incorrect alignment and
incorrect installation of the adjustment device, which could lead to
loss of the rudder control from the affected side and possibly
result in reduced control of the airplane.

(f) Compliance

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

(g) General Visual Inspection

    Within 30 days after the effective date of this AD: Do a general
visual inspection of the rudder control system to confirm correct
alignment and installation of the adjustment device, in accordance
with the instructions of Airbus Defence and Space Alert Operators
Transmission (AOT) AOT-C295-27-0001, Revision 1, dated September 29,
2015; or Airbus Defence and Space AOT AOT-CN235-27-0002, Revision 1,
dated September 22, 2015; as applicable.

(h) Corrective Action

    If, during the general visual inspection required by paragraph
(g) of this AD, any discrepancy is found, as specified in Airbus
Defence and Space AOT AOT-C295-27-0001, Revision 1, dated September
29, 2015; or Airbus Defence and Space AOT AOT-CN235-27-0002,
Revision 1, dated September 22, 2015; as applicable: Before further
flight, repair using a method approved by the Manager, International
Branch, ANM-116, Transport Airplane Directorate, FAA; or the
European Aviation Safety Agency (EASA); or Airbus Defense and Space
S.A.'s EASA Design Organization Approval (DOA).

(i) Credit for Previous Actions

    This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using Airbus Defence and Space AOT AOT-C295-27-0001,
dated October 23, 2014; or Airbus Defence and Space AOT AOT-CN235-
27-0002, dated October 23, 2014; as applicable.

(j) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to ATTN: Shahram
Daneshmandi, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>. Information
may be emailed to<EMAIL_ADDRESS>Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the local flight
standards district office/certificate holding district office. The
AMOC approval letter must specifically reference this AD.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Branch, ANM-116, Transport Airplane Directorate, FAA; or the
European Aviation Safety Agency (EASA); or Airbus Defense and Space
S.A.'s EASA Design Organization Approval (DOA). If approved by the
DOA, the approval must include the DOA-authorized signature.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0012, dated January 14,
2016, for related information. You may examine the MCAI on the
Internet at http://www.regulations.gov by searching for and locating
Docket No. FAA-2016-3704.
    (2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (l)(3) and (l)(4) of this AD.

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
    (i) Airbus Defence and Space Alert Operators Transmission AOT-
C295-27-0001, Revision 1, dated September 29, 2015.
    (ii) Airbus Defence and Space Alert Operators Transmission AOT-
CN235-27-0002, Revision 1, dated September 22, 2015.
    (3) For service information identified in this AD, contact
Airbus Defense and Space S.A., Services/Engineering Support, Avenida
de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55
84; fax +34 91 585 3127; email
<EMAIL_ADDRESS>For U.S. operators, email
alternatively<EMAIL_ADDRESS>    (4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on February 15, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-03883 Filed 2-25-16; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 77, Number 8 (Thursday, January 12, 2012)]
[Notices]
[Pages 1924-1925]
[FR Doc No: 2012-425]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 13762-001; Project No. 13753-001]

FFP Missouri 15, LLC; FFP Missouri 16, LLC; Notice of Intent To
File License Application, Filing of Pre-Application Document, and
Approving Use of the Traditional Licensing Process

    a. Type of Filing: Notice of Intent To File License Application and
Request to Use the Traditional Licensing Process.
    b. Project Nos.: P-13762-001, P-13753-001.
    c. Date Filed: November 16, 2011.
    d. Submitted By: Free Flow Power Corporation on behalf of its
subsidiary limited liability corporations (listed above and
collectively referred to below as ``Free Flow Power'').
    e. Name of Projects: Morgantown Lock and Dam Project, P-13762-001;
and Opekiska Lock and Dam Project, P-13753-001.
    f. Location: At existing locks and dams owned and operated by the
U.S. Army Corps of Engineers on the Monongahela River in West Virginia

(see table below for specific project locations). The projects would
occupy United States lands administered by the U.S. Army Corps of
Engineers.

----------------------------------------------------------------------------------------------------------------
              Project No.                     Projects                 County                     City
----------------------------------------------------------------------------------------------------------------
P-13762...............................  Morgantown Lock and   Monongalia..............  Morgantown.
                                         Dam Hydroelectric
                                         Project.
P-13753...............................  Opekiska Lock and     Monongalia..............  Fairmont.
                                         Dam Hydroelectric
                                         Project.
----------------------------------------------------------------------------------------------------------------

    g. Filed Pursuant to: 18 CFR 5.3 of the Commission's regulations.
    h. Potential Applicant Contact: Ramya Swaminathan, Chief Operating
Officer, Free Flow Power, 239 Causeway Street, Boston, MA 02114-2130;
(978) 283-2822; or email at<EMAIL_ADDRESS>    i. FERC Contact: Monir Chowdhury at<PHONE_NUMBER>; or email at
<EMAIL_ADDRESS>    j. Free Flow Power filed its request to use the Traditional
Licensing Process on November 16, 2011. Free Flow Power provided public
notice of its request on November 16, 2011. In a letter dated January
5, 2012, the Director of the Division of Hydropower Licensing approved
Free Flow Power's request to use the Traditional Licensing Process.
    k. With this notice, we are initiating informal consultation with:
(a) The U.S. Fish and Wildlife Service and NOAA Fisheries under section
7 of the Endangered Species Act and the joint agency regulations
thereunder at 50 CFR, part 402; (b) NOAA Fisheries under section 305(b)
of the Magnuson-Stevens Fishery Conservation and Management Act and
implementing regulations at 50 CFR 600.920; and (c) the West Virginia
Historic Preservation Officer, as required by section 106, National
Historic Preservation Act, and the implementing regulations of the
Advisory Council on Historic Preservation at 36 CFR 800.2.
    l. With this notice, we are designating Free Flow Power as the
Commission's non-federal representative for carrying out informal
consultation, pursuant to section 7 of the Endangered Species Act,
section 305 of the Magnuson-Stevens Fishery Conservation and Management
Act, and section 106 of the National Historic Preservation Act.
    m. Free Flow Power filed a Pre-Application Document (PAD; including
a proposed process plan and schedule) with the Commission, pursuant to
18 CFR 5.6 of the Commission's regulations.
    n. A copy of the PAD is available for review at the Commission in
the Public Reference Room or may be viewed on the Commission's Web site
(http://www.ferc.gov), using the ``eLibrary'' link. Enter the docket
number, excluding the last three digits in the docket number field to
access the document. For assistance, contact FERC Online Support at
<EMAIL_ADDRESS>or toll free at 1-(866) 208-3676, or for
TTY,<PHONE_NUMBER>. A copy is also available for inspection and
reproduction at the address in paragraph h.
    o. Register online at http://www.ferc.gov/docs-filing/esubscription.asp to be notified via email of new filing and issuances
related to this or other pending projects. For assistance, contact FERC
Online Support.

    Dated: January 5, 2012.
Kimberly D. Bose,
Secretary.
[FR Doc. 2012-425 Filed 1-11-12; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 85, Number 71 (Monday, April 13, 2020)]
[Rules and Regulations]
[Pages 20416-20418]
[FR Doc No: 2020-07612]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 97

[Docket No. 31304; Amdt. No. 3898]

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 April 13, 2020. 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 April 13, 2020.

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, email
<EMAIL_ADDRESS>or go to: https://www.archives.gov/federal-register/cfr/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 Procedures
and Airspace Group, Flight Technologies and Procedures Division, Flight
Standards Service, Federal Aviation Administration. Mailing Address:
FAA Mike Monroney Aeronautical Center, Flight Procedures and Airspace
Group, 6500 South MacArthur Blvd., Registry Bldg 29 Room 104, Oklahoma
City, OK 73169. 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 March 20, 2020.
Rick Domingo,
Executive 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.

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

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

 * * * Effective Upon Publication

--------------------------------------------------------------------------------------------------------------------------------------------------------
      AIRAC date             State               City                 Airport         FDC No.    FDC Date                     Subject
--------------------------------------------------------------------------------------------------------------------------------------------------------
23-Apr-20.............  TX              Fort Worth...........  Fort Worth Meacham       0/1186     3/3/20  This NOTAM, published in Docket No. 31302,
                                                                Intl.                                       Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  FL              Fort Pierce..........  Treasure Coast Intl.     0/1228     3/3/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  FL              Fort Pierce..........  Treasure Coast Intl.     0/1229     3/3/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.

23-Apr-20.............  FL              Fort Pierce..........  Treasure Coast Intl.     0/1230     3/3/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  FL              Fort Pierce..........  Treasure Coast Intl.     0/1231     3/3/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  MN              Rochester............  Rochester Intl......     0/5079    2/19/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  IN              La Porte.............  La Porte Muni.......     0/7323    2/21/20  This NOTAM, published in Docket No. 31302,
                                                                                Amdt No. 3896, TL 20-09 (85 FR 16240; March
                                                                                23, 2020), is hereby rescinded in its
                                                                                entirety.
23-Apr-20.............  NE              Holdrege.............  Brewster Field......     0/2149     3/5/20  VOR-A, Amdt 3A.
23-Apr-20.............  KS              Pittsburg............  Atkinson Muni.......     0/2778     3/5/20  RNAV (GPS) RWY 4, Amdt 1E.
23-Apr-20.............  KS              Pittsburg............  Atkinson Muni.......     0/2779     3/5/20  VOR/DME RWY 4, Amdt 3E.
23-Apr-20.............  MD              Westminster..........  Clearview Airpark...     0/2781     3/5/20  RNAV (GPS) RWY 14, Amdt 1B.
23-Apr-20.............  VA              Richmond.............  Richmond Intl.......     0/2803     3/5/20  VOR RWY 20, Amdt 1B.
23-Apr-20.............  NY              Binghamton...........  Greater Binghamton/      0/2877     3/5/20  RNAV (GPS) RWY 34, Amdt 1.
                                                                Edwin A Link Field.
23-Apr-20.............  IL              Centralia............  Centralia Muni......     0/2884     3/5/20  VOR-A, Amdt 1.
23-Apr-20.............  NH              Lebanon..............  Lebanon Muni........     0/3496     3/6/20  RNAV (GPS) RWY 7, Orig-E.
23-Apr-20.............  NH              Lebanon..............  Lebanon Muni........     0/3502     3/6/20  RNAV (GPS) RWY 36, Orig-C.
23-Apr-20.............  NH              Lebanon..............  Lebanon Muni........     0/3524     3/6/20  VOR RWY 25, Amdt 1B.
23-Apr-20.............  FL              Palm Coast...........  Flagler Executive...     0/3660    2/26/20  Takeoff Minimums and Obstacle DP, Amdt 2.
23-Apr-20.............  MT              West Yellowstone.....  Yellowstone.........     0/3776    3/10/20  ILS OR LOC RWY 1, Amdt 4.
23-Apr-20.............  MT              West Yellowstone.....  Yellowstone.........     0/3780    3/10/20  RNAV (GPS) RWY 1, Orig-A.
23-Apr-20.............  MT              West Yellowstone.....  Yellowstone.........     0/3781    3/10/20  NDB RWY 1, Amdt 4.
23-Apr-20.............  LA              Lafayette............  Lafayette Rgnl/Paul      0/4521    3/10/20  RNAV (GPS) RWY 22L, Amdt 1C.
                                                                Fournet Field.
23-Apr-20.............  LA              Lafayette............  Lafayette Rgnl/Paul      0/4525    3/10/20  VOR/DME RWY 11, Amdt 1F.
                                                                Fournet Field.
23-Apr-20.............  LA              Lafayette............  Lafayette Rgnl/Paul      0/4526    3/10/20  ILS OR LOC RWY 4R, Amdt 2E.
                                                                Fournet Field.
23-Apr-20.............  LA              Lafayette............  Lafayette Rgnl/Paul      0/4534    3/10/20  ILS OR LOC RWY 22L, Amdt 5D.
                                                                Fournet Field.
23-Apr-20.............  NV              Las Vegas............  McCarran Intl.......     0/4574    3/10/20  VOR/DME-A, Orig-D.
23-Apr-20.............  TN              Nashville............  Nashville Intl......     0/4582    3/11/20  RNAV (GPS) RWY 13, Amdt 1.
23-Apr-20.............  MO              Butler...............  Butler Memorial.....     0/4635    3/11/20  VOR-A, Amdt 5.
23-Apr-20.............  MA              Vineyard Haven.......  Martha's Vineyard...     0/4638    3/10/20  ILS OR LOC RWY 24, Amdt 3B.
23-Apr-20.............  VT              Burlington...........  Burlington Intl.....     0/4648    3/11/20  ILS OR LOC/DME RWY 33, Amdt 1B.
23-Apr-20.............  VT              Burlington...........  Burlington Intl.....     0/4660    3/11/20  RNAV (GPS) RWY 1, Orig-B.
23-Apr-20.............  CA              Hawthorne............  Jack Northrop Field/     0/4671    3/11/20  VOR RWY 25, Amdt 16
                                                                Hawthorne Muni.
23-Apr-20.............  IN              Sheridan.............  Sheridan............     0/4769    3/11/20  GPS RWY 23, Orig-A.
23-Apr-20.............  IN              Sheridan.............  Sheridan............     0/4770    3/11/20  GPS RWY 5, Orig-A.
23-Apr-20.............  IA              Marshalltown.........  Marshalltown Muni...     0/4970    3/11/20  VOR RWY 13, Amdt 2.
23-Apr-20.............  IA              Marshalltown.........  Marshalltown Muni...     0/4992    3/11/20  VOR RWY 31, Amdt 2.
23-Apr-20.............  TX              Houston..............  Sugar Land Rgnl.....     0/5193    3/11/20  RNAV (GPS) RWY 17, Amdt 2A.
23-Apr-20.............  TX              Houston..............  Sugar Land Rgnl.....     0/5194    3/11/20  RNAV (GPS) RWY 35, Amdt 2A.
--------------------------------------------------------------------------------------------------------------------------------------------------------

[FR Doc. 2020-07612 Filed 4-10-20; 8:45 am]
 BILLING CODE 4910-13-P