[Federal Register Volume 80, Number 18 (Wednesday, January 28, 2015)]
[Proposed Rules]
[Pages 4527-4528]
[FR Doc No: 2015-01465]

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ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 180

[EPA-HQ-OPP-2014-0209; FRL-9921-60]

Receipt of a Pesticide Petition Filed for Residues of Pesticide
Chemicals in or on Various Commodities

AGENCY: Environmental Protection Agency (EPA).

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

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SUMMARY: This document announces the Agency's receipt of an initial
filing of a pesticide petition 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 February 27, 2015.

ADDRESSES: Submit your comments, identified by docket identification
(ID) number EPA-HQ-OPP-2014-0209, 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: Susan Lewis, 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_ADDRESS>
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).

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 receipt of a pesticide petition 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 request before responding to the petitioner. EPA is not proposing
any particular action at this time. EPA has determined that the
pesticide petition described in this document contains 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 supports granting of
the pesticide petition. 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 this pesticide petition.
    Pursuant to 40 CFR 180.7(f), a summary of the petition that is the
subject of this document, prepared by the petitioner, is included in a
docket EPA has created for this rulemaking. The docket for this
petition 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.
    PP 3F8210. Bayer CropScience, 2 T.W. Alexander Dr., Research
Triangle Park, NC 27709, requests to establish a tolerance in 40 CFR
part 180.435 for residues of the insecticide, deltamethrin [(1R, 3R)-
3(2,2-dibromovinyl)-2,2-dimethylcyclopropane-carboxylic acid (S)-alpha-
cyano-3-phenoxybenzyl ester] and its major metabolites trans-
deltamethrin [(s)-alpha-cyano-3-phenoxybenzyl-(1R, 3S)-3-(2,2-
dibromovinyl)-2,2-dimethylcyclopropanecarboxylate] and alpha-R-
deltamethrin [(R)-alphacyano-3-phenoxybenzyl-(1R, 3R)-3-(2,2-
dibromovinyl)-2,2-dimethylcyclopropanecarboxylate, in or on food and
feed commodities following wide-area mosquito adulticide applications
at at 0.05 parts per million (ppm). High performance liquid
chromatography/triple stage quadrupole mass spectrometry (LC/MS/MS) is
used to measure and evaluate the chemical and its cis and trans
isomers.

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

    Dated: January 20, 2015.
Susan Lewis,
Director, Registration Division, Office of Pesticide Programs.
[FR Doc. 2015-01465 Filed 1-27-15; 8:45 am]
BILLING CODE 6560-50-P


[Federal Register Volume 80, Number 32 (Wednesday, February 18, 2015)]
[Proposed Rules]
[Pages 8568-8571]
[FR Doc No: 2015-02925]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-0245; Directorate Identifier 2014-NM-135-AD]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to supersede Airworthiness Directive (AD) 2012-24-
10, which applies to certain The Boeing Company Model 747-400 and -400F
series airplanes. AD 2012-24-10 currently requires installing new
software, replacing the duct assembly with a new duct assembly, making
wiring changes, and routing certain wire bundles. Since we issued AD
2012-24-10, we have received new reports of intermittent or blank
displays of a certain integrated display unit (IDU) that were due to an
intermittent false ground not addressed by the software installation or
wiring changes required by AD 2012-24-10. This proposed AD would retain
the requirements of AD 2012-24-10 and would require installing a new or
serviceable pressure switch bracket and altitude pressure switch, and
add an airplane to the applicability of the existing AD. We are
proposing this AD to prevent IDU malfunctions, which could affect the
ability of the flightcrew to read primary displays for airplane
attitude, altitude, or airspeed, and consequently reduce the ability of
the flightcrew to maintain control of the airplane.

DATES: We must receive comments on this proposed AD by April 6, 2015.

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 proposed AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management, P.
O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone<PHONE_NUMBER>,
extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.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-2015-
0245.

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-2015-
0245; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this proposed AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (phone:<PHONE_NUMBER>) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Ana Martinez Hueto, Aerospace
Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA,
Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW.,
Renton, WA 98057-3356; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2015-0245;
Directorate Identifier 2014-NM-135-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://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 November 30, 2012, we issued AD 2012-24-10, Amendment 39-17280
(77 FR 73908, December 12, 2012), for certain The Boeing Company Model
747-400 and -400F series airplanes. AD 2012-24-10 requires installing
new software, replacing the duct assembly with a new duct assembly,
making wiring changes, and routing certain wire bundles. AD 2012-24-10
resulted from multiple reports of integrated display unit (IDU)
malfunctions and mode control panel (MCP) malfunctions. We issued AD
2012-24-10 to prevent IDU malfunctions, which could affect the ability
of the flightcrew to read primary displays for airplane attitude,
altitude, or airspeed, and consequently reduce the ability of the
flightcrew to maintain control of the airplane.

Actions Since AD 2012-24-10, Amendment 39-17280 (77 FR 73908, December
12, 2012), Was Issued

    Since we issued AD 2012-24-10, Amendment 39-17280 (77 FR 73908,
December 12, 2012), we have received reports of intermittent or blank
displays of a certain IDU in the flight deck that were due to an
intermittent false ground not addressed by the software installation or
wiring changes required by AD 2012-24-10. The false ground exists on
the 25,000 foot altitude analog/discrete signal of the environmental
control systems miscellaneous card, which is a signal that is
transmitted to the pack temperature controller. This false ground
creates a potential to circumvent the control logic by allowing the 3-
way valve to switch air sources before an aircraft reaches an altitude
of 25,000 feet, defeating the intent of the corrective actions of AD
2012-24-10.
    We have determined that the installation of a pressure switch
bracket and an altitude pressure switch is needed on the forward side
of the station 400 bulkhead to achieve an adequate level of safety. The
installation of the altitude pressure switch would change the operating
logic for the three-way valve, so that the source for equipment cooling
air is changed as the airplane transitions through an altitude of
25,000 feet. Since we issued AD 2012-24-10, Boeing issued Special
Attention Service Bulletin 747-21-2532; and Special Attention Service
Bulletin 747-21-2533; both dated February 13, 2014; which contain
procedures for installing the pressure switch bracket and altitude
pressure switch discussed previously.
    Since we issued AD 2012-24-10, Amendment 39-17280 (77 FR 73908,
December 12, 2012), Boeing also issued a revision to Boeing Alert
Service Bulletin 747-21A2523, Revision 1, dated October 3, 2011 (which
was referenced as a source of service information in AD 2012-24-10).
Boeing Alert Service Bulletin 747-21A2523, Revision 2, dated June 7,
2013, was issued to correct wiring instructions for 747-400BCF
airplanes that provide crew rest heat below a 25,000 foot altitude, and
to add an airplane configuration having variable number RT061 as Group
21 to the effectivity. The airplane that was added was recently
converted from a passenger to a freighter configuration, which this
proposed AD addresses. Since this

proposed AD adds this new airplane group to the applicability, we have
added paragraph (j) to this proposed AD, which provides new compliance
times for Group 21 airplanes.

Related Service Information Under 1 CFR Part 51

    Boeing issued Boeing Alert Service Bulletin 747-21A2523, Revision
2, dated June 7, 2013. This service information describes procedures
for changing the wiring and operating logic of the equipment cooling
three-way valve and replacing the existing duct assembly with a new
duct assembly on the main distribution manifold of the air conditioning
system.
    Boeing also issued Boeing Special Attention Service Bulletin 747-
21-2532, dated February 13, 2014. This service information describes
procedures for installing an altitude pressure switch on the forward
side of the station 400 bulkhead for the three-way valve of the
equipment cooling system. Boeing also issued Boeing Special Attention
Service Bulletin 747-21-2533, dated February 13, 2014. This service
information describes procedures for adding a second altitude signal to
the switching logic for the three-way valve to provide a second,
independent, altitude signal for the equipment cooling system.
    For information on the procedures and compliance times, see this
service information. This service information is reasonably available;
see ADDRESSES for ways to access this service information.

FAA's Determination

    We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of these same type
designs.

Proposed AD Requirements

    This proposed AD would retain all of the requirements of AD 2012-
24-10, Amendment 39-17280 (77 FR 73908, December 12, 2012.) This
proposed AD would also require installing a pressure switch bracket and
altitude pressure switch, and would add an airplane to the
applicability.

Costs of Compliance

    We estimate that this proposed AD affects 33 airplanes of U.S.
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Duct assembly and replacement wiring    44 work-hours x $85 per          $20,121         $23,861        $787,413
 changes (retained actions from AD       hour = $3,740.
 2012-24-10, Amendment 39-17280 (77 FR
 73908, December 12, 2012).
Software changes (retained actions      3 work-hours x $85 per                 0             255           8,415
 from AD 2012-24-10, Amendment 39-       hour = $255.
 17280 (77 FR 73908, December 12,
 2012).
Altitude pressure switch installation   13 work-hours x $85 per            5,230           6,335         209,055
 (new proposed action).                  hour = $1,105.
----------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some of the costs of this proposed
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 costs in our cost
estimate.

Authority for This Rulemaking

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

Regulatory Findings

    We have determined that this 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 that the 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 removing Airworthiness Directive (AD)
2012-24-10, Amendment 39-17280 (77 FR 73908, December 12, 2012), and
adding the following new AD:

The Boeing Company: Docket No. FAA-2015-0245; Directorate Identifier
2014-NM-135-AD.

(a) Comments Due Date

    The FAA must receive comments on this AD action by April 6,
2015.

(b) Affected ADs

    This AD replaces AD 2012-24-10, Amendment 39-17280 (77 FR 73908,
December 12, 2012).

(c) Applicability

    This AD applies to The Boeing Company Model 747-400 and -400F
series airplanes, certificated in any category, as identified in
Boeing Alert Service Bulletin 747-21A2523, Revision 2, dated June 7,
2013.

(d) Subject

    Air Transport Association (ATA) of America Code 21, Air
Conditioning; 31, Instruments.

(e) Unsafe Condition

    This AD was prompted by reports of intermittent or blank
displays of a certain integrated display unit (IDU) in the flight
deck. We are issuing this AD to prevent IDU malfunctions, which
could affect the ability of the flightcrew to read primary displays
for airplane attitude, altitude, or airspeed, and consequently
reduce the ability of the flightcrew to maintain control of the
airplane.

(f) Compliance

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

(g) Retained Software Update

    This paragraph restates the requirements of paragraph (g) of AD
2012-24-10, Amendment 39-17280 (77 FR 73908, December 12, 2012),
with revised service information. Within 12 months after January 16,
2013 (the effective date of AD 2012-24-10), except as provided by
paragraph (j) of this AD: Install integrated display system
software, in accordance with the Accomplishment Instructions of
Boeing Alert Service Bulletin 747-21A2523, Revision 1, dated October
3, 2011; or Boeing Alert Service Bulletin 747-21A2523, Revision 2,
dated June 7, 2013. As of the effective date of this AD, only Boeing
Alert Service Bulletin 747-21A2523, Revision 2, dated June 7, 2013,
may be used to accomplish the actions required by this paragraph.
    Note 1 to paragraph (g) and (j) of this AD: Boeing Alert Service
Bulletin 747-21A2523, Revision 1, dated October 3, 2011; and Boeing
Alert Service Bulletin 747-21A2523, Revision 2, dated June 7, 2013;
refer to Boeing Service Bulletin 747-31-2426, dated July 29, 2010
(for airplanes with Rolls-Royce engines); Boeing Service Bulletin
747-31-2427, dated July 29, 2010 (for airplanes with General
Electric engines); and Boeing Service Bulletin 747-31-2428, dated
July 29, 2010 (for airplanes with Pratt & Whitney engines); as
additional sources of guidance for the software installation
specified by paragraph (g) of this AD. Boeing Service Bulletin 747-
31-2426, dated July 29, 2010; Boeing Service Bulletin 747-31-2427,
dated July 29, 2010; and Boeing Service Bulletin 747-31-2428, dated
July 29, 2010; are not incorporated by reference in this AD.

(h) Retained Duct Assembly Replacement and Wiring Changes

    This paragraph restates the requirements of paragraph (h) of AD
2012-24-10, Amendment 39-17280 (77 FR 73908, December 12, 2012),
with revised service information. Within 60 months after January 16,
2013 (the effective date of AD 2012-24-10), except as provided by
paragraph (j) of this AD: Replace the duct assembly with a new duct
assembly, do wiring changes, and route certain wire bundles, in
accordance with the Accomplishment Instructions of Boeing Alert
Service Bulletin 747-21A2523, Revision 1, dated October 3, 2011; or
Boeing Alert Service Bulletin 747-21A2523, Revision 2, dated June 7,
2013. As of the effective date of this AD, only Boeing Alert Service
Bulletin 747-21A2523, Revision 2, dated June 7, 2013, may be used to
accomplish the actions required by this paragraph.

(i) New Installation of Pressure Switch Bracket and Altitude Pressure
Switch

    Within 60 months after the effective date of this AD: Install a
new or serviceable pressure switch bracket and a new or serviceable
altitude pressure switch on the forward side of the station 400
bulkhead, do wiring changes, route certain wire bundles, install a
new hose assembly, and perform a leak check and a functional logic
test, in accordance with the Accomplishment Instructions of the
service information specified in paragraph (i)(1) or (i)(2) of this
AD, as applicable.
    (1) For Model 747-400F series airplanes: Boeing Alert Service
Bulletin 747-21-2532, dated February 13, 2014.
    (2) For Model 747-400BCF series airplanes: Boeing Alert Service
Bulletin 747-21-2533, dated February 13, 2014.

(j) Actions for Group 21 Airplanes

    For Group 21 airplanes, as identified in Boeing Alert Service
Bulletin 747-21A2523, Revision 2, dated June 7, 2013, do the actions
specified in paragraphs (j)(1) and (j)(2) of this AD, in accordance
with the Accomplishment Instructions of Boeing Alert Service
Bulletin 747-21A2523, Revision 2, dated June 7, 2013.
    (1) Within 12 months after the effective date of this AD,
install integrated display system software.
    (2) Within 60 months after the effective date of this AD,
replace the duct assembly with a new duct assembly, do wiring
changes, and route certain wire bundles.

(k) Credit for Previous Actions

    This paragraph provides credit for actions required by
paragraphs (g) and (h) of this AD, if those actions were performed
before the effective date of this AD using Boeing Alert Service
Bulletin 747-21A2523, Revision 1, dated October 3, 2011.

(l) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle Aircraft Certification Office (ACO),
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 ACO, send it to the
attention of the person identified in paragraph (m)(1) of this AD.
Information may be emailed to<EMAIL_ADDRESS>    (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.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair required by this AD if it is approved by Boeing
Commercial Airplanes Organization Designation Authorization (ODA)
that has been authorized by the Manager, Seattle ACO, to make those
findings. For a repair method to be approved, the repair must meet
the certification basis of the airplane, and the approval must
specifically refer to this AD.
    (4) AMOCs approved for AD 2012-24-10, Amendment 39-17280 (77 FR
73908, December 12, 2012), are approved as AMOCs for the
corresponding provisions of paragraphs (g) and (h) of this AD.

(m) Related Information

    (1) For more information about this AD, contact Ana Martinez
Hueto, Aerospace Engineer, Cabin Safety and Environmental Systems
Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO),
1601 Lind Avenue SW., Renton, WA 98057-3356; phone:<PHONE_NUMBER>;
fax:<PHONE_NUMBER>; email<EMAIL_ADDRESS>    (2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-
5000, extension 1; fax<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may view this 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 February 2, 2015.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-02925 Filed 2-17-15; 8:45 am]
BILLING CODE 4910-13-P