[Federal Register Volume 78, Number 64 (Wednesday, April 3, 2013)]
[Notices]
[Page 20101]
[FR Doc No: 2013-07677]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. RP12-514-000]

Tennessee Gas Pipeline Company, LLC; Notice of Technical
Conference

    The Commission's January 17, 2013 Order in the above-captioned
proceeding \1\ directed that a technical conference be held to address
issues raised by Tennessee Gas Pipeline Company, LLC's filing to modify
the secondary in-the-path scheduling priority provisions of its FERC
Gas Tariff.
---------------------------------------------------------------------------

    \1\ Texas Eastern Transmission, LP, 129 FERC ] 61,088 (2009).
---------------------------------------------------------------------------

    Take notice that a technical conference will be held on Wednesday,
April 10, 2013 at 10:00 a.m., in a room to be designated at the offices
of the Federal Energy Regulatory Commission, 888 First Street, NE.,
Washington, DC 20426.
    FERC conferences are accessible under section 508 of the
Rehabilitation Act of 1973. For accessibility accommodations please
send an email to<EMAIL_ADDRESS>or call toll free (866) 208-
3372 (voice) or<PHONE_NUMBER> (TTY), or send a fax to<PHONE_NUMBER> with
the required accommodations.
    All interested persons and staff are permitted to attend. For
further information please contact David Maranville at<PHONE_NUMBER>
or email<EMAIL_ADDRESS>
    Dated: March 27, 2013.
Kimberly D. Bose,
Secretary.
[FR Doc. 2013-07677 Filed 4-2-13; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 83, Number 89 (Tuesday, May 8, 2018)]
[Proposed Rules]
[Pages 20748-20751]
[FR Doc No: 2018-09731]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0366; Product Identifier 2017-NM-166-AD]
RIN 2120-AA64

Airworthiness Directives; ATR-GIE Avions de Transport
R[eacute]gional Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500 airplanes.
This proposed AD was prompted by a determination that more restrictive
maintenance requirements and airworthiness limitations are necessary.
This proposed AD would require revising the maintenance or inspection
program, as applicable, to incorporate new and/or more restrictive
maintenance requirements and airworthiness limitations. We are
proposing this AD to address the unsafe condition on these products.

DATES: We must receive comments on this proposed AD by June 22, 2018.

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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this NPRM, contact ATR-GIE
Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email aircraft.com">[email protected]aircraft.com;
internet http://www.atr-aircraft.com. You may view this service
information at the FAA, Transport Standards Branch, 2200 South 216th
St., Des Moines, WA. For information on the availability of this
material at the FAA, call<PHONE_NUMBER>.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0366; 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 NPRM, 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 Section, Transport Standards Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone and fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2018-0366;
Product Identifier 2017-NM-166-AD'' at the beginning of your comments.
We specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this NPRM. We will consider all
comments received by the closing date and may amend this NPRM 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 NPRM.

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 2017-0222R1, dated December 15, 2017 (referred
to after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for ATR-GIE Avions de
Transport R[eacute]gional Model ATR42-500 airplanes. The MCAI states:

    The airworthiness limitations and certification maintenance
requirements (CMR) for ATR aeroplanes, which are approved by EASA,
are currently defined and published in the ATR42-400/-500 Time
Limits (TL) document. These instructions have been identified as
mandatory for continued airworthiness.
    Failure to accomplish these instructions could result in an
unsafe condition [i.e., reduced structural integrity of the
airplane].
    Consequently, ATR published Revision 11 Temporary revision 01 of
the ATR42-400/-500 TL document, which contains new and/or more
restrictive CMRs and airworthiness limitations tasks.
    For the reasons described above, this [EASA] AD requires
accomplishment of the actions specified in the ATR42-400/-500 TL
document Revision 11 Temporary revision 01, hereafter referred to as
`the TLD' in this [EASA] AD.
    This [EASA] AD, in conjunction with two other [EASA] ADs related
to ATR42-200/-300/-320 (EASA AD 2017-0221) and ATR72-101/-102/-201/-
202/-211/-212/-212A (EASA AD 2017-0223) aeroplanes, retains the
requirements of EASA AD 2009-0242 [which corresponds to FAA AD 2008-
04-19 R1, Amendment 39-16069 (74 FR 56713, November 3, 2009)] and
EASA AD 2012-0193 [which corresponds to FAA AD 2015-26-09, Amendment
39-18357 (81 FR 1483, January 13, 2016)]. Once all these three
[EASA] ADs are effective, EASA will cancel EASA AD 2009-0242 and
EASA AD 2012-0193.
    This [EASA] AD is revised to provide the correct issue date (03
May 2017) of the TLD. The original [EASA] AD inadvertently
referenced the EASA approval date for that document.

    The required actions include revising the maintenance or inspection
program, as applicable, to incorporate new and/or more restrictive
maintenance requirements and airworthiness limitations. The unsafe
condition is reduced structural integrity of the airplane.
    You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0366.

Relationship Between Proposed AD and Certain Other ADs

    This NPRM would not supersede AD 2008-04-19 R1 and AD 2015-26-09.
Rather, we have determined that a stand-alone AD would be more
appropriate to address the changes in the MCAI. This NPRM would require
revising the maintenance or inspection program, as applicable.
Accomplishment of the proposed actions would then terminate all
requirements of AD 2008-04-19 R1 and AD 2015-26-09 for ATR-GIE Avions
de Transport R[eacute]gional Model ATR42-500 airplanes only.
    In addition, we have determined that accomplishment of the proposed
actions terminates all requirements of AD 2000-23-04 R1, Amendment 39-
12174 (66 FR 19381, April 16, 2001).

Related Service Information Under 1 CFR Part 51

    ATR-GIE Avions de Transport R[eacute]gional has issued ATR42-400/-
500, Time Limits Document (TL), Revision 11, dated May 5, 2015. This
service information describes life limits and maintenance requirements
for the affected airplanes.
    ATR-GIE Avions de Transport R[eacute]gional has issued ATR42-400/-
500 Temporary Revision TR01/17, dated May 3, 2017, to the ATR42-400/-
500 Time Limits Document (TL). This service information describes
changes to life limits and maintenance requirements of certain tasks
for the affected airplanes.
    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 Proposed AD

    This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
    This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(k)(1) of this proposed AD. The request should include a description of
changes to the required actions that will ensure the continued
operational safety of the airplane.

Differences Between This Proposed AD and the MCAI or Service
Information

    The MCAI specifies that if there are findings from the
airworthiness limitations section (ALS) inspection tasks, corrective
actions must be accomplished in accordance with Airbus maintenance
documentation. However, this proposed AD does not include that
requirement. Operators of U.S.-registered airplanes are required by
general airworthiness and operational regulations to perform
maintenance using methods that are acceptable to the FAA. We consider
those methods to be adequate to address any corrective actions
necessitated by the findings of ALS inspections required by this
proposed AD.

Airworthiness Limitations Based on Type Design

    The FAA recently became aware of an issue related to the
applicability of ADs that require incorporation of an ALS revision into
an operator's maintenance or inspection program.
    Typically, when these types of ADs are issued by civil aviation
authorities of other countries, they apply to all airplanes covered
under an identified type certificate (TC). The corresponding FAA AD
typically retains applicability to all of those airplanes.
    In addition, U.S. operators must operate their airplanes in an
airworthy condition, in accordance with 14 CFR 91.7(a). Included in
this obligation is the requirement to perform any maintenance or
inspections specified in the ALS, and in accordance with the ALS as
specified in 14 CFR 43.16 and 91.403(c), unless an alternative has been
approved by the FAA.
    When a type certificate is issued for a type design, the specific
ALS, including revisions, is a part of that type design, as specified
in 14 CFR 21.31(c).
    The sum effect of these operational and maintenance requirements is
an obligation to comply with the ALS defined in the type design
referenced in the manufacturer's conformity statement. This obligation
may introduce a conflict with an AD that requires a specific ALS
revision if new airplanes are delivered with a later revision as part
of their type design.
    To address this conflict, the FAA has approved alternative methods
of compliance (AMOCs) that allow operators to incorporate the most
recent ALS revision into their maintenance/

inspection programs, in lieu of the ALS revision required by the AD.
This eliminates the conflict and enables the operator to comply with
both the AD and the type design.
    However, compliance with AMOCs is normally optional, and we
recently became aware that some operators choose to retain the AD-
mandated ALS revision in their fleet-wide maintenance/inspection
programs, including those for new airplanes delivered with later ALS
revisions, to help standardize the maintenance of the fleet. To ensure
that operators comply with the applicable ALS revision for newly
delivered airplanes containing a later revision than that specified in
an AD, we plan to limit the applicability of ADs that mandate ALS
revisions to those airplanes that are subject to an earlier revision of
the ALS, either as part of the type design or as mandated by an earlier
AD.
    This proposed AD therefore would apply to ATR-GIE Avions de
Transport R[eacute]gional Model ATR42-500 airplanes with an original
certificate of airworthiness or original export certificate of
airworthiness that was issued on or before the date of approval of the
ALS temporary revision identified in this proposed AD. Operators of
airplanes with an original certificate of airworthiness or original
export certificate of airworthiness issued after that date must comply
with the airworthiness limitations specified as part of the approved
type design and referenced on the type certificate data sheet.

Costs of Compliance

    We estimate that this proposed AD affects 4 airplanes of U.S.
registry.
    We estimate the following costs to comply with this proposed AD:
    We have determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although this
figure may vary from operator to operator. In the past, we have
estimated that this action takes 1 work-hour per airplane. Since
operators incorporate maintenance or inspection program changes for
their affected fleet(s), we have determined that a per-operator
estimate is more accurate than a per-airplane estimate. Therefore, we
estimate the total cost per operator to be $7,650 (90 work-hours x $85
per work-hour).

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.
    This proposed AD is issued in accordance with authority delegated
by the Executive Director, Aircraft Certification Service, as
authorized by FAA Order 8000.51C. In accordance with that order,
issuance of ADs is normally a function of the Compliance and
Airworthiness Division, but during this transition period, the
Executive Director has delegated the authority to issue ADs applicable
to transport category airplanes to the Director of the System Oversight
Division.

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec.  39.13   [Amended]

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

ATR-GIE Avions de Transport R[eacute]gional: Docket No. FAA-2018-
0366; Product Identifier 2017-NM-166-AD.

(a) Comments Due Date

    We must receive comments by June 22, 2018.

(b) Affected ADs

    This AD affects the ADs specified in paragraphs (b)(1), (b)(2),
and (b)(3) of this AD.
    (1) AD 2000-23-04 R1, Amendment 39-12174 (66 FR 19381, April 16,
2001) (``AD 2000-23-04 R1'').
    (2) AD 2008-04-19 R1, Amendment 39-16069 (74 FR 56713, November
3, 2009) (``AD 2008-04-19 R1'').
    (3) AD 2015-26-09, Amendment 39-18357 (81 FR 1483, January 13,
2016) (``AD 2015-26-09'').

(c) Applicability

    This AD applies to ATR-GIE Avions de Transport R[eacute]gional
Model ATR42-500 airplanes, certificated in any category, with an
original airworthiness certificate or original export certificate of
airworthiness dated on or before May 3, 2017.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time limits/
maintenance checks.

(e) Reason

    This AD was prompted by a determination that more restrictive
maintenance requirements and airworthiness limitations are
necessary. We are issuing this AD to prevent reduced structural
integrity of the airplane.

(f) Compliance

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

(g) Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the
maintenance or inspection program, as applicable, to incorporate the
information specified in ATR42-400/-500, Time Limits Document (TL),
Revision 11, dated May 5, 2015; and ATR42-400/-500 Temporary
Revision TR01/17, dated May 3, 2017, to the ATR42-400/-500 Time
Limits Document (TL). The initial compliance time for accomplishing
the tasks is at the applicable times specified in ATR42-400/ -500,
Time Limits Document (TL), Revision 11, dated May 5, 2015; and
ATR42-400/-500 Temporary Revision TR01/17, dated May 3, 2017, to the
ATR42-400/-500, Time Limits

Document (TL); or within 90 days after the effective date of this
AD; whichever occurs later, except for those certification
maintenance requirements (CMRs) tasks identified in figure 1 to
paragraphs (g) and (h) of this AD.

   Figure 1 to Paragraphs (g) and (h) of This AD--Grace Period for CMR
                                  Tasks
------------------------------------------------------------------------
  CMR/ maintenance significant item
              (MSI) task                        Compliance time
------------------------------------------------------------------------
213100-2A                              Within 550 flight hours or 90
213100-2B                               days, whichever occurs first,
213100-3A                               after the effective date of this
213100-3B                               AD.
------------------------------------------------------------------------

(h) Initial Compliance Times for Certain CMR Tasks

    For the CMR tasks listed in figure 1 to paragraphs (g) and (h)
of this AD, the initial compliance time for accomplishing the tasks
is at the applicable time specified in ATR42-400/-500 Temporary
Revision TR01/17, dated May 3, 2017, to the ATR42-400/-500 Time
Limits Document (TL); or within the compliance time specified in
figure 1 to paragraphs (g) and (h) of this AD; whichever occurs
later.

(i) No Alternative Actions, Intervals, and/or Critical Design
Configuration Control Limitations (CDCCLs)

    After the maintenance or inspection program, as applicable, has
been revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections), intervals, and/or CDCCLs may be used
unless the actions, intervals, and/or CDCCLs are approved as an
alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (k)(1) of this AD.

(j) Terminating Action for Certain ADs

    Accomplishing the actions required by paragraph (g) of this AD
terminates all requirements of AD 2000-23-04 R1 and all requirements
of the ADs specified in paragraphs (j)(1) and (j)(2) of this AD for
ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500
airplanes only.
    (1) AD 2008-04-19 R1.
    (2) AD 2015-26-09.

(k) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards 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 International Section, send it to the attention of
the person identified in paragraph (l)(2) of this AD. Information
may be emailed to: [email protected]. 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.
    (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
Section, Transport Standards Branch, FAA; or the European Aviation
Safety Agency (EASA); or ATR-GIE Avions de Transport
R[eacute]gional's EASA Design Organization Approval (DOA). If
approved by the DOA, the approval must include the DOA-authorized
signature.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2017-0222R1, dated December 15, 2017, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2018-0366.
    (2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax<PHONE_NUMBER>.
    (3) For service information identified in this AD, contact ATR-
GIE Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21;
fax +33 (0) 5 62 21 67 18; email aircraft.com">[email protected]aircraft.com; internet http://www.atr-aircraft.com. You may view
this service information at the FAA, Transport Standards Branch,
2200 South 216th St., Des Moines, WA. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>.

    Issued in Des Moines, Washington, on April 27, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-09731 Filed 5-7-18; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 83, Number 206 (Wednesday, October 24, 2018)]
[Proposed Rules]
[Pages 53594-53595]
[FR Doc No: 2018-23251]

=======================================================================
-----------------------------------------------------------------------

ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 180

[EPA-HQ-OPP-2014-0008; FRL-9983-46]

Receipt of Several Pesticide Petitions Filed for Residues of
Pesticide Chemicals in or on Various Commodities

AGENCY: Environmental Protection Agency (EPA).

ACTION: Notice of filing of petitions and request for comment.

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

SUMMARY: This document announces the Agency's receipt of several
initial filings of pesticide petitions requesting the establishment or
modification of regulations for residues of pesticide chemicals in or
on various commodities.

DATES: Comments must be received on or before November 23, 2018.

ADDRESSES: Submit your comments, identified by docket identification
(ID) number and the pesticide petition number (PP) of interest as shown
in the body of this document, by one of the following methods:
     Federal eRulemaking Portal: http://www.regulations.gov.
Follow the online instructions for submitting comments. Do not submit
electronically any information you consider to be Confidential Business
Information (CBI) or other information whose disclosure is restricted
by statute.
     Mail: OPP Docket, Environmental Protection Agency Docket
Center (EPA/DC), (28221T), 1200 Pennsylvania Ave. NW, Washington, DC
20460-0001.
     Hand Delivery: To make special arrangements for hand
delivery or delivery of boxed information, please follow the
instructions at http://www.epa.gov/dockets/contacts.html.
    Additional instructions on commenting or visiting the docket, along
with more information about dockets generally, is available at http://www.epa.gov/dockets.

FOR FURTHER INFORMATION CONTACT: Michael L. Goodis, Registration
Division (7505P), Office of Pesticide Programs, Environmental
Protection Agency, 1200 Pennsylvania Ave. NW, Washington, DC 20460-
0001; main telephone number:<PHONE_NUMBER>; email address:
[email protected].

SUPPLEMENTARY INFORMATION:

I. General Information

A. Does this action apply to me?

    You may be potentially affected by this action if you are an
agricultural producer, food manufacturer, or pesticide manufacturer.
The following list of North American Industrial Classification System
(NAICS) codes is not intended to be exhaustive, but rather provides a
guide to help readers determine whether this document applies to them.
Potentially affected entities may include:
     Crop production (NAICS code 111).
     Animal production (NAICS code 112).
     Food manufacturing (NAICS code 311).
     Pesticide manufacturing (NAICS code 32532).
    If you have any questions regarding the applicability of this
action to a particular entity, consult the person listed under FOR
FURTHER INFORMATION CONTACT for the division listed at the end of the
pesticide petition summary of interest.

B. What should I consider as I prepare my comments for EPA?

    1. Submitting CBI. Do not submit this information to EPA through
regulations.gov or email. Clearly mark the part or all of the
information that you claim to be CBI. For CBI information in a disk or
CD-ROM that you mail to EPA, mark the outside of the disk or CD-ROM as
CBI and then identify electronically within the disk or CD-ROM the
specific information that is claimed as CBI. In addition to one
complete version of the comment that includes information claimed as
CBI, a copy of the comment that does not contain the information
claimed as CBI must be submitted for inclusion in the public docket.
Information so marked will not be disclosed except in accordance with
procedures set forth in 40 CFR part 2.
    2. Tips for preparing your comments. When preparing and submitting
your comments, see the commenting tips at http://www.epa.gov/dockets/comments.html.
    3. Environmental justice. EPA seeks to achieve environmental
justice, the fair treatment and meaningful involvement of any group,
including minority and/or low-income populations, in the development,
implementation, and enforcement of environmental laws, regulations, and
policies. To help address potential environmental justice issues, the
Agency seeks information on any groups or segments of the population
who, as a result of their location, cultural practices, or other
factors, may have atypical or disproportionately high and adverse human
health impacts or environmental effects from exposure to the pesticides
discussed in this document, compared to the general population.

II. What action is the Agency taking?

    EPA is announcing its receipt of several pesticide petitions filed
under section 408 of the Federal Food, Drug, and Cosmetic Act (FFDCA),
21 U.S.C. 346a, requesting the establishment or modification of
regulations in 40 CFR part 180 for residues of pesticide chemicals in
or on various food commodities. The Agency is taking public comment on
the requests before responding to the petitioners. EPA is not proposing
any particular action at this time. EPA has determined that the
pesticide petitions described in this document contain the data or
information prescribed in FFDCA section 408(d)(2), 21 U.S.C.
346a(d)(2); however, EPA has not fully evaluated the sufficiency of the
submitted data at this time or whether the data support granting of the
pesticide petitions. After considering the public comments, EPA intends
to evaluate whether and what action may be warranted. Additional data
may be needed before EPA can make a final determination on these
pesticide petitions.
    Pursuant to 40 CFR 180.7(f), a summary of each of the petitions
that are the subject of this document, prepared by the petitioner, is
included in a docket EPA has created for each rulemaking. The docket
for each of the petitions is available at http://www.regulations.gov.
    As specified in FFDCA section 408(d)(3), 21 U.S.C. 346a(d)(3), EPA
is publishing notice of the petition so that the public has an
opportunity to comment on this request for the establishment or
modification of regulations for residues of pesticides in or on food
commodities. Further information on the petition may be obtained
through the petition summary referenced in this unit.

New Tolerances

    1. PP 7E8586. EPA-HQ-OPP-2009-0493. Bayer CropScience LP, 2 T.W.
Alexander Dr., Research Triangle Park, NC 27709-2014, requests to
establish an import tolerance without U.S. registration in 40 CFR part
180.652 for residues of the insecticide ethiprole, and its metabolites
and degradates, in or on coffee, green bean at 0.10 parts per million
(ppm). The high performance liquid chromatography/mass spectrometry
(HPLC/MS-MS) enforcement method, Method 01128, is acceptable for
determination of residues of ethiprole and its sulfone metabolite RPA
097973 for data collection in plant commodities. The gas
chromatography-electron capture detector (GC-ECD) method (Report No.
B003572) is suitable for determining residues of parent ethiprole and
RPA in milk, eggs and tissues. The Food and Drug Administration (FDA)
multiresidue method testing study for ethiprole is adequate and
indicates that Pesticide Analytical Manual (PAM) multiresidue methods
are not suitable for enforcing tolerances for residues of ethiprole.
Contact: RD.
    2. PP 8E8693. EPA-HQ-OPP-2018-0636. OAT Agrio Co., Ltd. c/o Landis
International, Inc., 3185 Madison Highway, P.O. Box 5126, Valdosta, GA
31603-5126, requests to establish an import tolerance without U.S.
registration in 40 CFR part 180.677 for residues of the insecticide
cyflumetofen in or on coffee bean at 0.08 ppm. The method performance
was verified before and during sample analysis by determining the
recoveries from control samples fortified with cyflumetofen/ B-1 at
0.01/0.01 ppm (Limit of Quantitation (LOQ) and 0.1/0.1ppm (10x LOQ) for
green coffee bean, roasted coffee bean and instant coffee. The LOD
(Limit of Detection) for cyflumetofen and B-1 was calculated as 0.0029
ppm and 0.0017 ppm for green coffee bean, 0.0025 ppm and 0.0017 ppm for
roasted coffee bean, and 0.0019 ppm and 0.0011 ppm for instant coffee.
Contact: RD.

    Authority: 21 U.S.C. 346a.

    Dated: October 2, 2018.
Michael L. Goodis,
Director, Registration Division, Office of Pesticide Programs.
[FR Doc. 2018-23251 Filed 10-23-18; 8:45 am]
 BILLING CODE 6560-50-P


[Federal Register: August 10, 2006 (Volume 71, Number 154)]
[Notices]
[Page 45816]
[DOCID:fr10au06-65]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[ Project No. 2107-016]

Pacific Gas and Electric Company California; Notice of
Availability of Draft Environmental Assessment

August 2, 2006.
    In accordance with the National Environmental Policy Act of 1969
and the Federal Energy Regulatory Commission's (Commission)
regulations, 18 CFR part 380 (Order No. 486, 52 FR 47897), the Office
of Energy Projects has reviewed the application for license for the Poe
Hydroelectric Project, located on the North Fork Feather River in Butte
County, California, and has prepared a Draft Environmental Assessment
(DEA) for the project. The Project occupies 144 acres of lands of the
United States, which are administered by the Forest Supervisor of the
Plumas National Forest.
    The DEA contains the staff's analysis of the potential
environmental impacts of the project and concludes that licensing the
project, with appropriate environmental protective measures, would not
constitute a major Federal action that would significantly affect the
quality of the human environment.
    A copy of the DEA is available for review at the Commission in the
Public Reference Room or may be viewed on the Commission's Web site at
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,

(202) 502-8659.
    You may also register online at http://www.ferc.gov/docs-filing/esubscription.asp
 to be notified via e-mail of new filings and

issuances related to this or other pending projects. For assistance,
contact FERC Online Support.
    Any comments should be filed within 45 days from the date of this
notice and should be addressed to Magalie R. Salas, Secretary, Federal
Energy Regulatory Commission, 888 First Street, NE., Washington, DC
20426. Please affix Project No. 2107-016 to all comments. Comments may
be filed electronically via the Internet in lieu of paper. The
Commission strongly encourages electronic filings. See 18 CFR
385.2001(a)(1)(iii) and the instructions on the Commission's Web site
(http://www.ferc.gov) under the ``e-Filing'' link.

    For further information, contact John Mudre at<PHONE_NUMBER>.

Magalie R. Salas,
Secretary.
 [FR Doc. E6-13048 Filed 8-9-06; 8:45 am]

BILLING CODE 6717-01-P


[Federal Register Volume 86, Number 106 (Friday, June 4, 2021)]
[Notices]
[Pages 30037-30038]
[FR Doc No: 2021-11778]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 2146-259]

Alabama Power Company; Notice of Application Accepted for Filing
and Soliciting Comments, Motions To Intervene, and Protests

    Take notice that the following hydroelectric application has been
filed with the Commission and is available for public inspection:
    a. Application Type: Non-Project Use of Project Lands and Waters.
    b. Project No: 2146-259.
    c. Date Filed: May 19, 2021.
    d. Applicant: Alabama Power Company.
    e. Name of Project: Coosa River Hydroelectric Project.
    f. Location: The Lay Development of the Coosa River Hydroelectric
Project is in Chilton, Coosa, Shelby, and Talledega counties, Alabama;
the proposed non-project use of project lands and waters would be
located in Shelby County.
    g. Filed Pursuant to: Federal Power Act, 16 U.S.C. 791a-825r.
    h. Applicant Contact: Shelia Smith, Alabama Power Company at (256)
396-5093, or<EMAIL_ADDRESS>    i. FERC Contact: Shawn Halerz at<PHONE_NUMBER> or
<EMAIL_ADDRESS>    j. Deadline for Filing Comments, Motions to Intervene, and
Protests: June 28, 2021.
    The Commission strongly encourages electronic filing. Please file
comments, motions to intervene, and protests using the Commission's
eFiling system at http://www.ferc.gov/docs-filing/efiling.asp.
Commenters can submit brief comments up to 6,000 characters, without
prior registration, using the eComment system at http://www.ferc.gov/docs-filing/ecomment.asp. You must include your name and contact
information at the end of your comments. For assistance, please contact
FERC Online Support at<EMAIL_ADDRESS>(866) 208-3676 (toll
free), or<PHONE_NUMBER> (TTY). In lieu of electronic filing, you may
submit a paper copy. Submissions sent via the U.S. Postal Service must
be addressed to: Kimberly D. Bose, Secretary, Federal Energy Regulatory
Commission, 888 First Street NE, Room 1A, Washington, DC 20426.
Submissions sent via any other carrier must be addressed to: Kimberly
D. Bose, Secretary, Federal Energy Regulatory Commission, 12225 Wilkins
Avenue, Rockville, Maryland 20852. The first page of any filing should
include the docket number P-2146-259. Comments emailed to Commission
staff are not considered part of the Commission record.
    The Commission's Rules of Practice and Procedure require all
intervenors filing documents with the Commission to serve a copy of
that document on each person whose name appears on the official service
list for the project. Further, if an intervenor files comments or
documents with the Commission relating to the merits of an issue that
may affect the responsibilities of a particular resource agency, they
must also serve a copy of the document on that resource agency.
    k. Description of Request: Alabama Power Company is requesting
Commission approval to permit James and Tracey Etheridge to provide
wet-slips, a boat ramp, a courtesy pier, and a seawall that will be
associated with an RV park and campground (Lay Lake Campground) located
outside of the project boundary. An existing boathouse structure within
the project boundary is included in this request as well and was
previously permitted through Alabama Power Company's residential
permitting program.
    l. Locations of the Application: This filing may be viewed on the
Commission's website at 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. You may also register
online at http://www.ferc.gov/docs-filing/esubscription.asp to be
notified via email of new filings and issuances related to this or
other pending projects. For assistance, call 1-866-208-3676 or email
<EMAIL_ADDRESS>for TTY, call<PHONE_NUMBER>. Agencies may
obtain copies of the application directly from the applicant.
    m. Individuals desiring to be included on the Commission's mailing
list should so indicate by writing to the Secretary of the Commission.
    n. Comments, Protests, or Motions to Intervene: Anyone may submit
comments, a protest, or a motion to intervene in accordance with the
requirements of Rules of Practice and Procedure, 18 CFR 385.210, .211,
.214, respectively. In determining the appropriate action to take, the
Commission will consider all protests or other comments filed, but only
those who file a motion to intervene in accordance with the
Commission's Rules may become a party to the proceeding. Any comments,
protests, or motions to intervene must be received on or before the
specified comment date for the particular application.

    o. Filing and Service of Documents: Any filing must (1) bear in all
capital letters the title ``COMMENTS'', ``PROTEST'', or ``MOTION TO
INTERVENE'' as applicable; (2) set forth in the heading the name of the
applicant and the project number of the application to which the filing
responds; (3) furnish the name, address, and telephone number of the
person commenting, protesting or intervening; and (4) otherwise comply
with the requirements of 18 CFR 385.2001 through 385.2005. All
comments, motions to intervene, or protests must set forth their
evidentiary basis. Any filing made by an intervenor must be accompanied
by proof of service on all persons listed in the service list prepared
by the Commission in this proceeding, in accordance with 18 CFR
385.2010.

    Dated: May 28, 2021.
Kimberly D. Bose,
Secretary.
[FR Doc. 2021-11778 Filed 6-3-21; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 77, Number 120 (Thursday, June 21, 2012)]
[Proposed Rules]
[Pages 37337-37340]
[FR Doc No: 2012-15166]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0643; Directorate Identifier 2011-NM-190-AD]
RIN 2120-AA64

Airworthiness Directives; Fokker Services B.V. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to supersede an existing airworthiness directive
(AD) that applies to certain Fokker Services B.V. Model F.28 Mark 0070
and 0100 airplanes. The existing AD currently requires performing a
detailed visual inspection for cracks of the pistons on the main
landing gear (MLG), and replacing the affected pistons if necessary.
Since we issued that AD, a new modification has been developed to
safeguard the integrity of the MLG assembly and improve surface
protection of the affected area of the MLG piston. This proposed AD
would also require modifying the MLG by installing a piston containing
a certain part number, and revising the aircraft maintenance program.
We are proposing this AD to prevent MLG failure, possibly resulting in
loss of control of the airplane during the landing roll-out.

DATES: We must receive comments on this proposed AD by August 6, 2012.

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, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
    For Fokker service information identified in this proposed AD,
contact Fokker Services B.V., Technical Services Dept., P.O. Box 231,
2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252-627-350;
fax +31 (0)252-627-211; email
<EMAIL_ADDRESS>Internet http://www.myfokkerfleet.com. For Goodrich service information identified in
this proposed AD, contact Goodrich, 1400 South Service Road, West
Oakville, L6L 5Y7, Ontario, Canada, telephone +1-905-827-7777; fax +1-
905-825-1583; Internet http://www.goodrich.com/TechPubs. You may review
copies of the referenced 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 425-
227-1221.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this proposed 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: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 425-227-
1137; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-0643;
Directorate Identifier 2011-NM-190-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD 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 proposed AD.

Discussion

    On January 31, 2011, we issued AD 2011-04-01, Amendment 39-16601
(76 FR 8618, February 15, 2011). That AD required actions intended to
address an unsafe condition on the products listed above.
    Since we issued AD 2011-04-01, Amendment 39-16601 (76 FR 8618,
February 15, 2011), a new modification has been developed to safeguard
the integrity of the MLG assembly and improve surface protection of the
affected area of the MLG piston. The European Aviation Safety Agency
(EASA), which is the Technical Agent for the Member States of the
European Community, has issued EASA Airworthiness Directive 2011-0159,
dated August 26, 2011 (referred to after this as ``the MCAI''), to
correct an unsafe condition for the specified products. The MCAI
states:

    During a normal walk around check on a F28 Mark 0100 aeroplane,
a large crack was discovered in the lower portion of the right (RH)
MLG piston. The affected MLG unit had accumulated 7,909 flight
cycles (FC) at the time of detection. The piston was sent to
Goodrich, the landing gear manufacturer, for detailed investigation,
which revealed that the crack had been initiated by corrosion pits.
The extent of the corrosion indicates that the initial crack existed
for a substantial period before a high loading event caused the
crack to grow further by ductile overload.
    This condition, if not detected and corrected, could lead to MLG
failure during the landing roll-out, possibly resulting in damage to
the aeroplane and injury to occupants.
    To address this potential unsafe condition, EASA issued AD 2009-
0221 [which corresponds with FAA AD 2011-04-01, Amendment 39-16601
(76 FR 8618, February 15, 2011)] to require a one-time detailed
visual inspection of the MLG pistons, the replacement of any MLG
pistons on which cracks are detected, and the reporting of all
findings to the aeroplane TC [type certificate] holder. No cracks
were reported as a result of this inspection.
    Subsequently, a repetitive inspection was introduced in the
Airworthiness Limitations Section (Fokker Services report SE-623
Issue 8) in Appendix 1 of the Maintenance Review Board (MRB)
document to safeguard the integrity of the MLG assembly, pending the
accomplishment of a terminating action.
    Goodrich issued Service Bulletin (SB) 41000-32-29 to introduce
an improved surface protection (nickel plate) of the affected area
of the MLG piston P/N [part number] 41141-3 and re-identification as
P/N 41141-5, which is considered as a terminating action for the
repetitive inspections.
    For the reasons described above, this [EASA] AD requires
repetitive visual inspections of the P/N 41141-3 MLG piston for
cracks and, depending on findings, replacement or modification of
the MLG piston. This [EASA] AD also requires modification of the
affected MLG by installing a piston P/N 41141-5.

You may obtain further information by examining the MCAI in the AD
docket.

Relevant Service Information

    Fokker Services B.V. has issued Fokker Service Bulletin SBF100-32-
161, dated April 7, 2011; and Fokker Engineering Report, MRB Appendix
1, SE-623, Issue 8, dated March 17, 2011. Goodrich Aerospace Canada
Ltd. has issued Goodrich Service Bulletin 41000-32-29, dated November
10, 2010. The actions described in this service information are
intended to correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of This Proposed AD

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

Costs of Compliance

    Based on the service information, we estimate that this proposed AD
would affect about 2 products of U.S. registry.
    The actions that are required by AD 2011-04-01, Amendment 39-16601
(76 FR 8618, February 15, 2011), and retained in this proposed AD take
about 3 work-hours per product, at an average labor rate of $85 per
work hour. Based on these figures, the estimated cost of the currently
required actions is $255 per product.
    We estimate that it would take about 26 work-hours per product to
comply with the new basic requirements of this proposed AD. The average
labor rate is $85 per work-hour. Based on these figures, we estimate
the cost of the proposed AD on U.S. operators to be $4,420, or $2,210
per product.

Authority for This Rulemaking

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

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

    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]

    2. The FAA amends Sec.  39.13 by removing airworthiness directive
(AD) 2011-04-01, Amendment 39-16601 (76 FR 8618, February 15, 2011),
and adding the following new AD:

Fokker Services B.V.: Docket No. FAA-2012-0643; Directorate
Identifier 2011-NM-190-AD.

(a) Comments Due Date

    We must receive comments by August 6, 2012.

(b) Affected ADs

    This AD supersedes AD 2011-04-01, Amendment 39-16601 (76 FR
8618, February 15, 2011).

(c) Applicability

    (1) This AD applies to Fokker Services B.V. Model F.28 Mark 0070
and 0100 airplanes; certificated in any category; all serial
numbers, equipped with Goodrich (formerly Menasco, Colt Industries)
main landing gear (MLG) units, part numbers (P/N) 41050-7, 41050-8,
41050-9, 41050-10, 41050-11, 41050-12, 41050-13, 41050-14, 41050-15,
41050-16, 41060-1, 41060-2, 41060-3, 41060-4, 41060-5 or 41060-6.
    (2) This AD requires revisions to certain operator maintenance
documents to include new actions (e.g., inspections). Compliance
with these inspections is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired
in the areas addressed by these actions, the operator may not be
able to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must
request approval for an alternative method of compliance according
to paragraph (n)(1) of this AD. The request should include a
description of changes to the required inspections that will ensure
the continued operational safety of the airplane.

(d) Subject

    Air Transport Association (ATA) of America Code 32: Main Landing
Gear.

(e) Reason

    This AD was prompted by a new modification developed to
safeguard the integrity of the MLG assembly and improve surface
protection of the affected area of the MLG piston. We are issuing
this AD to prevent MLG failure, possibly resulting in loss of
control of the airplane during the landing roll-out.

(f) Compliance

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

(g) Retained Initial Inspection

    This paragraph restates the initial inspection required by
paragraph (g) of AD 2011-04-01, Amendment 39-16601 (76 FR 8618,
February 15, 2011). Within 30 days after March 22, 2011 (the
effective date of AD 2011-04-01), do a detailed visual inspection
for cracks of the MLG pistons, in accordance with the Accomplishment
Instructions of Fokker Service Bulletin SBF100-32-158, dated October
2, 2009.

(h) Retained Replacement

    This paragraph restates the replacement required by paragraph
(h) of AD 2011-04-01, Amendment 39-16601 (76 FR 8618, February 15,
2011). If any cracked MLG piston is found during the inspection
required by paragraph (g) of this AD, before further flight, replace
the affected piston with a serviceable part, in accordance with the
Accomplishment Instructions of Fokker Service Bulletin SBF100-32-
158, dated October 2, 2009.

(i) New Requirement: Modification

    Within 120 months, or during a scheduled overhaul of the MLG,
whichever occurs first after the effective date of this AD: Modify
the MLG by installing a piston containing P/N 41141-5, in accordance
with the Accomplishment Instructions of Fokker Service Bulletin
SBF100-32-161, dated April 7, 2011. Re-installation of a MLG piston
which has been modified and re-identified as P/N 41141-5, in
accordance with the Accomplishment Instructions of Goodrich Service
Bulletin 41000-32-29, dated November 10, 2010, is an optional method
of

compliance for the requirements in this paragraph of this AD. It is
acceptable to operate an airplane with one MLG having a P/N 41141-5
piston installed, and the other MLG having a P/N 41141-3 piston
installed, provided all MLG P/N 41141-3 are replaced within the
compliance times specified in paragraph (i) of this AD.

(j) New Requirement: Parts Installation

    After 120 months after the effective date of this AD: No person
may install a MLG piston, P/N 41141-3, or a MLG unit equipped with a
MLG piston P/N 41141-3, on any airplane.

(k) New Requirement: Revising the Airplane Maintenance Program

    Within two months after the effective date of this AD: Revise
the airplane maintenance program by incorporating Task 321100-01-16,
inspection of the MLG piston, and associated thresholds and
intervals described in Fokker Engineering Report, MRB Appendix 1,
SE-623, Issue 8, dated March 17, 2011. The initial compliance time
for Task 321100-01-16 is within two months after the effective date
of this AD.

(l) No Alternative Actions or Intervals

    After accomplishing the revisions required by paragraph (k) of
this AD, no alternative actions (e.g., inspections) or intervals may
be used other than those specified in Fokker Engineering Report, MRB
Appendix 1, SE-623, Issue 8, dated March 17, 2011, unless the
actions and intervals are approved as an AMOC in accordance with the
procedures specified in paragraph (m)(1) of this AD.

(m) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 425-
227-1137; 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) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.

(n) Related Information

    (1) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2011-0159, dated August 26, 2011; and the service
information specified in paragraphs (n)(1)(i) through (n)(1)(iv) of
this AD; for related information.
    (i) Fokker Service Bulletin SBF100-32-161, dated April 7, 2011.
    (ii) Fokker Services Engineering Report, MRB Appendix 1, SE-623,
Issue 8, dated March 17, 2011.
    (iii) Goodrich Service Bulletin 41000-32-29, dated November 10,
2010.
    (iv) Fokker Service Bulletin SBF100-32-158, dated October 2,
2009.
    (2) For Fokker service information identified in this AD,
contact Fokker Services B.V., Technical Services Dept., P.O. Box
231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252-
627-350; fax +31 (0)252-627-211; email
<EMAIL_ADDRESS>Internet http://www.myfokkerfleet.com. For Goodrich service information identified
in this AD, contact Goodrich, 1400 South Service Road, West
Oakville, L6L 5Y7, Ontario, Canada, telephone +1-905-827-7777; fax
+1-905-825-1583; Internet http://www.goodrich.com/TechPubs. You may
review copies of the referenced 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>.

    Issued in Renton, Washington, on June 12, 2012.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-15166 Filed 6-20-12; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 86, Number 222 (Monday, November 22, 2021)]
[Notices]
[Pages 66318-66319]
[FR Doc No: 2021-25371]

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

DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-1978-N-0018]

Amending Over-the-Counter Monograph M020: Sunscreen Drug Products
for Over-The-Counter Human Use; Over-The-Counter Monograph Proposed
Order (OTC 000008) Extension of Comment Period

AGENCY: Food and Drug Administration, HHS.

ACTION: Proposed order; extension of comment period.

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

SUMMARY: The Food and Drug Administration (FDA or Agency) has extended
the comment period for the over-the-counter (OTC) monograph proposed
order (order ID OTC000008) entitled ``Amending Over-the-Counter (OTC)
Monograph M020: Sunscreen Drug Products for OTC Human Use'' (Proposed
Order), which was issued on September 24, 2021. A notice of
availability for the Proposed Order appeared in the Federal Register of
September 27, 2021. FDA issued the Proposed Order to amend and revise
the deemed final administrative order concerning nonprescription
sunscreen drug products (Deemed Final Order) established by the
enactment of the Coronavirus Aid, Relief, and Economic Security Act
(CARES Act). The Proposed Order, if finalized, would replace the Deemed
Final Order in its entirety with new conditions under which
nonprescription sunscreen drug products would be determined to be
generally recognized as safe and effective (GRASE) under the Federal
Food, Drug, and Cosmetic Act (FD&C Act). It would also set forth
certain characteristics that would establish that a sunscreen drug
product is not GRASE. FDA has extended the comment period for the
Proposed Order in response to a request for an extension to allow
interested persons additional time to submit comments.

DATES: FDA is extending the comment period on the Proposed Order issued
on September 24, 2021 (86 FR 53322). Submit electronic comments on the
Proposed Order by 11:59 p.m. Eastern Time at the end of December 27,
2021.

ADDRESSES: You may submit comments to Order ID OTC000008 as follows.
Please note that late, untimely filed comments will not be considered.
Comments must be submitted electronically on or before December 27,
2021. The https://www.regulations.gov will accept comments at any time
until 11:59 p.m. Eastern Time at the end of December 27, 2021.

Electronic Submissions

    Submit electronic comments in the following way:
     Federal eRulemaking Portal: https://www.regulations.gov.
Follow the instructions for submitting comments. Comments submitted
electronically, including attachments, to https://www.regulations.gov
will be posted to the docket unchanged. Because your comment will be
made public, you are solely responsible for ensuring that your comment
does not include any information that you or a third party may not wish
to be publicly posted, such as medical information or your or anyone
else's Social Security number, or confidential business information,
such as a manufacturing process. Please note that if you include your
name, contact information, or other information that identifies you in
the body of your comments, that information will be posted on https://www.regulations.gov.
     If you want to submit a comment with confidential
information that you do not wish to be made available to the public,
submit the comment electronically in the manner detailed in
Instructions.
    Instructions: All submissions received must include the Order ID
Number OTC000008 and the Docket No. FDA-1978-N-0018 for ``Amending
Over-the-Counter (OTC) Monograph M020: Sunscreen Drug Products for OTC
Human Use.'' Received comments, those filed in a timely manner (see
ADDRESSES), will be placed in the docket and, except for those
submitted as ``Confidential Submissions,'' will be publicly viewable on
https://www.regulations.gov or at the Dockets Management Staff between
9 a.m. and 4 p.m., Monday through Friday,<PHONE_NUMBER>.
     Confidential Submissions--Under section 505G(d) of the
FD&C Act (21 U.S.C. 355h(d)), FDA must make any information submitted
by any person with respect to this order available to the public upon
submission, with limited exceptions. FDA will not make public
information pertaining to pharmaceutical quality information, unless
such information is necessary to establish standards under which a drug
is generally recognized as safe and effective under section 201(p)(1)
of the FD&C Act (21 U.S.C. 321(p)(1)) (see section 505G(d)(2)(B) of the
FD&C Act). FDA will also not make public information that is of the
type contained in raw datasets (see section 505G(d)(2)(B) of the FD&C
Act). To submit a comment with this specific confidential information
that you do not wish to be made publicly available, electronically
submit two copies of the comment as an attachment to your comment
submission. One copy will include the information that you claim to be
confidential with a heading or cover note that states ``THIS DOCUMENT
CONTAINS CONFIDENTIAL INFORMATION.'' The Agency will review this copy,
including the claimed confidential information. The second copy, which
will have the claimed information redacted/blacked out, will be
available for public viewing and posted on https://www.regulations.gov.
Any information marked as ``confidential'' will not be disclosed except
in accordance with section 505G(d) of the FD&C Act, and other
applicable disclosure law.
    Docket: For access to the docket to read background documents or
the electronic comments received, go to https://www.regulations.gov and
insert the docket number, found in brackets in the heading of this
document, into the ``Search'' box and follow the prompts and/or go the
Dockets Management Staff, 5630 Fishers Lane, Rm. 1061, Rockville, MD
20852,<PHONE_NUMBER>.

FOR FURTHER INFORMATION CONTACT: Trang Tran, Center for Drug Evaluation
and Research, Food and Drug Administration, 10903 New Hampshire Ave.,
Silver Spring, MD 20993-0002,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: In the Federal Register of September 27,
2021 (86 FR 53322), FDA announced the availability of an OTC monograph
proposed order (order ID OTC000008), issued pursuant to section 505G(b)
of the FD&C Act (21 U.S.C. 355g(b)) and section 3854(c)(1) of the CARES
Act, entitled ``Amending Over-the-Counter (OTC) Monograph M020:
Sunscreen Drug Products for OTC Human Use.'' FDA issued this Proposed
Order to amend and revise the Deemed Final Order established by the
enactment of the CARES Act, Public Law 116-136 (March 27, 2020).\1\
This Proposed Order,

if finalized, would replace the Deemed Final Order in its entirety with
new conditions under which nonprescription sunscreen drug products
would be determined to be GRASE under section 201(p)(1) of the FD&C Act
(21 U.S.C. 321(p)(1)). It would also set forth certain characteristics
establishing that a sunscreen drug product is not GRASE under section
201(p)(1) of the FD&C Act.
---------------------------------------------------------------------------

    \1\ To address nonprescription sunscreen drug products that are
also subject to provisions in other monographs, this proposed order
also proposes to amend and revise ``OTC Monograph M016, Skin
Protectant Drug Products for Over-the-Counter Human Use,'' and to
consolidate existing and new provisions that identify sunscreens
that are not GRASE in ``Non-Monograph Conditions NM020: Sunscreen
Drug Products for Over-the-Counter Human Use.''
---------------------------------------------------------------------------

    The original close of the public comment period for this Proposed
Order was November 12, 2021. On November 2, 2021, the Agency received a
request to extend this comment period by a minimum of 45 days,
conveying concern that the original comment period did not provide
sufficient time for review of the Proposed Order or for submission of
needed updates related to sunscreen active ingredients about which FDA
had requested additional data. FDA considered the request and extended
the public comment period for the Proposed Order for an additional 45
days, until December 27, 2021.\2\ This extension will allow additional
time for the public to submit information related to these active
ingredients (and other proposed sunscreen conditions) that has become
available since the closure of the comment period on the 2019 Proposed
Rule ``Sunscreen Drug Products for Over-the-Counter Human Use'' (2019
Proposed Rule).
---------------------------------------------------------------------------

    \2\ See https://www.regulations.gov/document/FDA-1978-N-0018-15828.
---------------------------------------------------------------------------

    The Agency reiterates that, as stated in the notice of availability
of the Proposed Order published in the Federal Register on September
27, 2021, and in the Proposed Order itself, the Agency will consider
all comments that were submitted to the public docket for the 2019
Proposed Rule within its comment period to be constructively submitted
as comments on the Proposed Order. The Agency requests that commenters
do not resubmit comments on this Proposed Order previously submitted on
the 2019 Proposed Rule.

    Dated: November 16, 2021.
Lauren K. Roth,
Associate Commissioner for Policy.
[FR Doc. 2021-25371 Filed 11-19-21; 8:45 am]
BILLING CODE 4164-01-P


[Federal Register Volume 81, Number 102 (Thursday, May 26, 2016)]
[Rules and Regulations]
[Pages 33371-33374]
[FR Doc No: 2016-12157]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-6892; Directorate Identifier 2016-NM-057-AD;
Amendment 39-18529; AD 2016-11-02]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. 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
Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, &
702) airplanes; Model CL-600-2D15 (Regional Jet Series 705) airplanes;
Model CL-600-2D24 (Regional Jet Series 900) airplanes; and Model CL-
600-2E25 (Regional Jet Series 1000) airplanes. This AD requires a
detailed visual inspection of the upper and lower engine pylons for
protruding, loose, or missing fasteners; and repair, including
applicable related investigative and corrective actions, if necessary.
This AD was prompted by reports of loose or

missing Hi-Lite fasteners on the upper and lower engine pylon structure
common to the upper and lower pylon skin panels and engine thrust
fitting. We are issuing this AD to detect and correct protruding,
loose, or missing fasteners, which could result in structural failure
of the engine pylons.

DATES: This AD becomes effective June 10, 2016.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of June 10,
2016.
    We must receive comments on this AD by July 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
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec
H4S 1Y9, Canada; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>; email
<EMAIL_ADDRESS>Internet http://www.bombardier.com. You
may view this referenced service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>. It
is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2016-6892.

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-
6892; 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: Aziz Ahmed, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2016-10, dated April 27, 2016 (referred to after this as the Mandatory
Continuing Airworthiness Information, or ``the MCAI''), to correct an
unsafe condition for all Bombardier, Inc. Model CL-600-2C10 (Regional
Jet Series 700, 701, & 702) airplanes; Model CL-600-2D15 (Regional Jet
Series 705) airplanes; Model CL-600-2D24 (Regional Jet Series 900)
airplanes; and Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
The MCAI states:

    There have been several reported findings of loose or missing
Hi-Lite fasteners on the left hand (LH) and right hand (RH) upper
and lower engine pylon structure common to the upper and lower pylon
skin panels and engine thrust fitting. Missing fasteners in these
areas are shown to significantly reduce the safety margins and could
result in a structural failure of the engine pylon.
    Bombardier has issued a new Aircraft Maintenance Manual (AMM)
task for detailed inspection of the engine pylon rib and skin
fasteners to inspect for protruding, loose or missing fasteners and
rectify any discrepancies [repair including applicable related
investigative and corrective actions] noted in accordance with a
Repair Engineering Order (REO).
    This AD is issued to mandate a repeat inspection to mitigate the
risk of a structural failure of the engine pylons and repair any
loose or missing fasteners as required.

Related investigative actions include visual inspections for cracks.
Corrective actions include repair. You may examine the MCAI on the
Internet at http://www.regulations.gov by searching for and locating
Docket No. FAA-2016-6892.

Related Service Information Under 1 CFR Part 51

    We reviewed Bombardier Repair Engineering Order 670-54-51-034,
``Repair for Missing or Loose/Protruding Fasteners in Upper and Lower
Pylon Skins FS 1088-FS 1098, PBL 69.3 L & RHS,'' dated March 7, 2016.
The service information describes procedures for repair, including
applicable related investigative and corrective actions.
    We also reviewed Bombardier Temporary Revision 54-0007, dated March
8, 2016, to the CRJ700/900/1000 AMM. The service information describes
procedures for a detailed visual inspection for protruding, loose, or
missing fasteners of the left-hand and right-hand upper and lower
engine pylons.
    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 this 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 loose
or missing Hi-Lite fasteners on the upper and lower engine pylon
structure common to the upper and lower pylon skin panels and engine
thrust fitting could result in structural failure of the engine pylons.
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-2016-6892; Directorate
Identifier 2016-NM-057-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 531 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. Based on these figures, we estimate the cost of
this AD on U.S. operators to be $45,135, or $85 per product.
    In addition, we estimate that any necessary follow-on actions will
take up to 32 work-hours for a cost of $2,720 per product, plus the
cost of parts. We have received no definitive data that would enable us
to provide cost estimates for the on-condition actions specified in
this AD. We have no way of determining the number of aircraft that
might need this action.
    According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all available costs in our
cost estimate.

Authority for This Rulemaking

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

Regulatory Findings

    We 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):

2016-11-02 Bombardier, Inc.: Amendment 39-18529. Docket No. FAA-
2016-6892; Directorate Identifier 2016-NM-057-AD.

(a) Effective Date

    This AD becomes effective June 10, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all the airplanes identified in paragraphs
(c)(1), (c)(2), (c)(3), and (c)(4) of this AD, certificated in any
category.
    (1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700,
701, & 702) airplanes.
    (2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705)
airplanes.
    (3) Bombardier, Inc. Model CL-600-2D24 (Regional Jet Series 900)
airplanes.
    (4) Bombardier, Inc. Model CL-600-2E25 (Regional Jet Series
1000) airplanes.

(d) Subject

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

(e) Reason

    This AD was prompted by reports of loose or missing Hi-Lite
fasteners on the upper and lower engine pylon structure common to
the upper and lower pylon skin panels and engine thrust fitting. We
are issuing this AD to detect and correct protruding, loose, or
missing fasteners, which could result in structural failure of the
engine pylons.

(f) Compliance

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

(g) Inspection

    At the applicable time specified in paragraph (g)(1) or (g)(2)
of this AD, do a detailed visual inspection for protruding, loose,
or missing fasteners of the upper and lower engine pylons, in
accordance with Bombardier Temporary Revision (TR) 54-0007, dated
March 8, 2016, to the CRJ700/900/1000 Aircraft Maintenance Manual.
Repeat the inspection thereafter at intervals not to exceed 1,500
flight hours.
    (1) For airplanes that have accumulated more than 840 total
flight hours as of the effective date of this AD: Inspect within 660
flight hours or 3 months, whichever occurs first, after the
effective date of this AD.
    (2) For airplanes that have accumulated 840 total flight hours
or less as of the effective date of this AD: Inspect before the
accumulation of 1,500 total flight hours.

(h) Repair

    If any protruding, loose, or missing fastener is found during
any inspection required by paragraph (g) of this AD, before further
flight, repair, including applicable related investigative and
corrective actions, in accordance with Bombardier Repair Engineering
Order (REO) 670-54-51-034, ``Repair for Missing or Loose/Protruding
Fasteners in Upper and Lower Pylon Skins FS 1088-FS 1098, PBL 69.3 L
& RHS,'' dated March 7, 2016, except where Bombardier REO 670-54-51-
034, ``Repair for Missing or loose/Protruding Fasteners in Upper and
Lower Pylon Skins FS 1088-FS 1098, PBL 69.3 L & RHS,'' dated March
7, 2016, specifies to contact Bombardier for further instruction,
before further flight, repair using a method approved by the
Manager, New York Aircraft Certification Office (ACO), ANE-170, FAA;
or Transport Canada Civil Aviation (TCCA); or Bombardier, Inc.'s
TCCA Design Approval Organization (DAO).

(i) Credit for Previous Actions

    This paragraph provides credit only for the initial inspection
specified in paragraph (g) of this AD, if that action was performed
before the effective date of this AD using Bombardier Reference
Instruction Letter 4212, dated December 23, 2015; or Bombardier
Reference Instruction Letter 4212A, Revision A, dated January 28,
2016. This service information is not incorporated by reference in
this AD.

(j) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO,

ANE-170, 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 ACO, send it to ATTN: Program Manager,
Continuing Operational Safety, FAA, New York ACO, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone<PHONE_NUMBER>; fax
516-794-5531. 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: As of the effective date of
this AD, 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, New York ACO, ANE-170, FAA; or TCCA; or
Bombardier, Inc.'s TCCA DAO. If approved by the DAO, the approval
must include the DAO-authorized signature.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian Airworthiness Directive CF-2016-10, dated April 27,
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-2016-6892.
    (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) Bombardier Repair Engineering Order 670-54-51-034, ``Repair
for Missing or Loose/Protruding Fasteners in Upper and Lower Pylon
Skins FS 1088-FS 1098, PBL 69.3 L & RHS,'' dated March 7, 2016.
    (ii) Bombardier Temporary Revision 54-0007, dated March 8, 2016,
to the CRJ700/900/1000 Aircraft Maintenance Manual.
    (3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone<PHONE_NUMBER>; fax 514-855-
7401; email<EMAIL_ADDRESS>Internet http://www.bombardier.com.
    (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 May 17, 2016.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-12157 Filed 5-25-16; 8:45 am]
 BILLING CODE 4910-13-P