[Federal Register Volume 86, Number 218 (Tuesday, November 16, 2021)]
[Proposed Rules]
[Pages 63322-63324]
[FR Doc No: 2021-24956]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-1002; Project Identifier AD-2021-00332-R]
RIN 2120-AA64

Airworthiness Directives; Sikorsky Aircraft Corporation
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Sikorsky Aircraft Corporation Model S-76D helicopters. This
proposed AD was prompted by reports that certain Thales global
positioning system (GPS) satellite based augmentation system (SBAS)
receivers provided, under certain conditions, erroneous outputs on
aircraft positions. This proposed AD would require replacing affected
GPS receivers and prohibit installing those GPS receivers. The FAA is
proposing this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by [January 3,
2022.

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 https://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 your local
Sikorsky Field Representative or Sikorsky's Service Engineering Group
at Sikorsky Aircraft Corporation, Mailstop K100, 124 Quarry Road,
Trumbull, CT 06611; telephone 1-800-946-4337 (1-800-Winged-S); email
[email protected]. Operators may also log on to the
Sikorsky 360 website at https://www.sikorsky360.com. You may view this
service information at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX
76177. For information on the availability of this material at the FAA,
call<PHONE_NUMBER>.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1002; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this NPRM, any comments
received, and other information. The street address for Docket
Operations is listed above.

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

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2021-1002; Project Identifier
AD-2021-00332-R'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI

as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Nicholas Rediess, Aviation Safety Engineer, Boston ACO Branch, FAA,
1200 District Avenue, Burlington, MA 01803; phone:<PHONE_NUMBER>; fax:
(781) 238-7199; email: [email protected]. Any commentary that
the FAA receives which is not specifically designated as CBI will be
placed in the public docket for this rulemaking.

Background

    The European Aviation Safety Agency (now European Union Aviation
Safety Agency) (EASA), which is the Technical Agent for the Member
States of the European Union, has issued EASA AD 2019-0004, dated
January 11, 2019, and corrected on January 17, 2019 (EASA AD 2019-
0004), to correct an unsafe condition for Thales AVS France SAS
(Thales), formerly Thales Avionics SAS, GPS/SBAS receivers, Topstar 200
LPV, part number (P/N) C17149HA01 and C17149JA02, using SBAS, which are
known to be installed on, but not limited to, certain Model ATR 42-500
and ATR 72-212A aeroplanes and Sikorsky Model S-76D helicopters. EASA
advises of reports indicating that Thales GPS SBAS receivers provided,
under certain conditions, erroneous outputs on aircraft positions. EASA
AD 2019-0004 requires actions to prevent compromise of the safety
margins when the receiver is used for Localizer Performance with
Vertical guidance (LPV) and/or RNP-AR (Required Navigation
Performance--Authorization Required) operations. Following the issuance
of EASA AD 2019-0004, the FAA issued AD 2020-08-02, Amendment 39-21108
(85 FR 20586, April 14, 2020), to address the unsafe condition on these
products.
    After the issuance of EASA AD 2019-0004, EASA issued related EASA
AD 2021-0013, dated January 13, 2021 (EASA AD 2021-0013), in response
to a software update that was developed to ensure correct navigational
performance of certain Thales GPS SBAS receivers installed on ATR-GIE
Avions de Transport R[eacute]gional, formerly EADS ATR--Alenia,
Aerospatiale Matra ATR--ALENIA, Aerospatiale--Alenia, Aerospatiale--
Aeritalia, Model ATR 42-500 and ATR 72-212A aeroplanes.
    This proposed AD would require replacing affected GPS TopStar 200
LPV receivers installed on Sikorsky Aircraft Corporation Model S-76D
helicopters. The FAA is proposing this AD to address erroneous aircraft
position outputs from the GPS SBAS receivers, which could result in
controlled flight into terrain, and subsequent loss of control of the
helicopter.

FAA's Determination

    The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Sikorsky S-76D Helicopter Service Bulletin SB 76-
017, Basic Issue, dated May 11, 2021 (SB 76-017). SB 76-017 specifies
procedures for removing, updating, and installing GPS TopStar 200 LPV
receivers. SB 76-017 also provides instructions for sending the GPS
receiver(s) to Thales Authorized Repair Stations for the software
update.
    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.

Proposed AD Requirements in This NPRM

    This proposed AD would require replacing each affected GPS receiver
and prohibit installing an affected GPS receiver on any helicopter.

Differences Between This Proposed AD and the Service Information

    SB 76-017 requires returning the GPS receiver(s) to Thales
Authorized Repair Stations for the software update, while this proposed
AD would require replacing the GPS receiver(s) instead.

Costs of Compliance

    The FAA estimates that this proposed AD would affect 22 helicopters
of U.S. Registry and that operators may incur the following costs in
order to comply with this proposed AD. Labor costs are estimated at $85
per work-hour.
    Replacing a GPS receiver would take about 3 work-hours and parts
would cost about $7,400, for an estimated cost of $7,655 per GPS
receiver and $336,820 for the U.S. fleet.

Authority for This Rulemaking

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

Regulatory Findings

    The FAA 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) Would not affect intrastate aviation in Alaska, and
    (3) Would 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:

Sikorsky Aircraft Corporation: Docket No. FAA-2021-1002; Project
Identifier AD-2021-00332-R.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive
(AD) by January 3, 2022.

(b) Affected ADs

    This AD affects AD 2020-08-02, Amendment 39-21108 (85 FR 20586,
April 14, 2020) (AD 2020-08-02).

(c) Applicability

    This AD applies to Sikorsky Aircraft Corporation Model S-76D
helicopters, certificated in any category, with Thales Global
Positioning System (GPS) TopStar 200 LPV receiver part number (P/N)
C17149HA01 installed.

(d) Subject

    Joint Aircraft System Component (JASC) Code: 3457, Global
Positioning System.

(e) Unsafe Condition

    This AD was prompted by reports that certain Thales GPS
satellite based augmentation system (SBAS) receivers provided, under
certain conditions, erroneous outputs on aircraft positions. The
unsafe condition, if not addressed, could result in controlled
flight into terrain and loss of control of the helicopter.

(f) Compliance

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

(g) Required Actions

    (1) Within 130 hours time-in-service after the effective date of
this AD, replace each affected GPS receiver identified in paragraph
(c) of this AD with GPS receiver P/N C17149RA01 in accordance with
the Accomplishment Instructions, paragraphs A., C., and D., of
Sikorsky S-76D Helicopter Service Bulletin SB 76-017, Basic Issue,
dated May 11, 2021.
    (2) As of the effective date of this AD, do not install a GPS
receiver identified in paragraph (c) of this AD on any helicopter.
    (3) Accomplishing paragraph (g)(1) of this AD terminates the
requirements of AD 2020-08-02.

((h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Boston ACO Branch, Compliance & Airworthiness
Division, FAA, has the authority to approve AMOCs for this AD, if
requested using the procedures found in 14 CFR 39.19. In accordance
with 14 CFR 39.19, send your request to your principal inspector or
local Flight Standards District Office, as appropriate. If sending
information directly to the manager of the certification office,
send it to the attention of the person identified in paragraph
(i)(1) of this AD.
    (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.

(i) Related Information

    (1) For more information about this AD, contact Nicholas
Rediess, Aviation Safety Engineer, Boston ACO Branch, FAA, 1200
District Avenue, Burlington, MA 01803; phone:<PHONE_NUMBER>; fax:
(781) 238-7199; email: [email protected].
    (2) For service information identified in this AD, contact your
local Sikorsky Field Representative or Sikorsky's Service
Engineering Group at Sikorsky Aircraft Corporation, Mailstop K100,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-946-4337 (1-
800-Winged-S); email [email protected]. Operators
may also log on to the Sikorsky 360 website at https://www.sikorsky360.com. You may view this referenced service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For
information on the availability of this material at the FAA, call
(817) 222-5110.

    Issued on November 8, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-24956 Filed 11-15-21; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 84, Number 175 (Tuesday, September 10, 2019)]
[Rules and Regulations]
[Pages 47407-47410]
[FR Doc No: 2019-19442]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0320; Product Identifier 2019-NM-017-AD; Amendment
39-19725; AD 2019-17-05]
RIN 2120-AA64

Airworthiness Directives; Airbus SAS Airplanes

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

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus SAS Model A330-200 Freighter, -200, and -300 series
airplanes; and certain Airbus SAS Model A340-200, -300, -500, and -600
series airplanes. This AD was prompted by a determination that certain
wing slat tracks that were inadvertently indicated as eligible for
installation on all Model A330 and A340 series airplanes are unable to
sustain the ultimate loads relative to the weight variant of certain
airplane configurations. This AD requires identifying affected parts,
inspecting for and repairing cracks, and replacing affected parts with
serviceable parts, as specified in a European Aviation Safety Agency
(EASA) AD, which is incorporated by reference. The FAA is issuing this
AD to address the unsafe condition on these products.

DATES: This AD is effective October 15, 2019.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 15,
2019.

ADDRESSES: For the material incorporated by reference (IBR) in this AD,
contact the EASA, at Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 89990 1000; email<EMAIL_ADDRESS>internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu. You may view this IBR material 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
206-231-3195. It is also available in the AD docket on the internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2019-0320.

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-2019-
0320; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations is U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax:<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Airbus SAS
Model A330-200 Freighter, -200 and -300 series airplanes; and certain
Airbus SAS Model A340-200, -300, -500, and -600 series airplanes. The
NPRM published in the Federal Register on May 8, 2019 (84 FR 20057).
The NPRM was prompted by a determination that certain wing slat tracks
that were inadvertently indicated as eligible for installation on all
Model A330 and A340 series airplanes are unable to sustain the ultimate
loads relative to the weight variant of certain airplane
configurations. The NPRM proposed to require inspecting any affected
part for cracking, and replacing with a serviceable part.
    The FAA is issuing this AD to address installation of affected
parts, which could result in slat detachment in flight and consequent
reduced control of the airplane.
    The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2019-0026, dated February 4, 2019
(``EASA AD 2019-0026'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Airbus SAS Model A330-200 Freighter, -200, and -
300 series airplanes; and certain Airbus SAS Model A340-200, -300, -
500, and -600 series airplanes. The MCAI states:

    It was recently determined that, since June 2010, the affected
parts were inadvertently indicated as eligible for installation on
all A330 and A340 aeroplanes in the applicable Illustrated Part
Catalogue (IPC), although in fact, those parts are not valid for
some aeroplane configurations (weight variants), because they are
unable to sustain ultimate load. Investigation demonstrated that
affected parts were never delivered as spare part. However, it
cannot be excluded that an affected part was removed in-service from
an aeroplane and installed on another.
    This condition, if not detected and corrected, could lead to
slat detachment in flight, possibly resulting in reduced control of
the aeroplane.
    To address this potential unsafe condition, Airbus published the
applicable SB [service bulletin] to provide instructions to identify
affected parts, and instructions to inspect [for cracking of] those
affected parts found installed.
    For the reasons described above, this [EASA] AD requires a one-
time detailed (DET) and special detailed inspection (SDI) of the aft
lug of each affected part and replacement of each affected part.
This [EASA] AD also prohibits installation of affected parts.

    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-2019-
0320.

Comments

    The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comments
received on the NPRM and the FAA's response to each comment.

Request To Include Additional Exceptions to the MCAI

    American Airlines (AAL) asked that an airplane records review for
the affected part identification be an approved method of compliance in
the proposed AD. AAL stated that its maintenance records indicate that
no affected #10 slat track was installed in production, or has been
installed since aircraft delivery.
    The FAA agrees with the commenter's request. The FAA has added
paragraph (h)(2) to this AD to allow a review of airplane maintenance
records in lieu of the inspections for the part numbers of the wing
slat tracks at the #10 position. Subsequent paragraphs have been
redesignated accordingly.
    AAL also asked that in cases where the slat track part number is
not identifiable, instructions be provided in the proposed AD to
specify a range for the slat track measured thickness used to identify
affected parts. AAL stated that Airbus Service Bulletin A330-57-3144,
dated November 12, 2018, which is referenced in EASA AD 2019-0026,
specifies that if the slat track part number is not identifiable, the
upper thickness of the aft lug must be measured, and if the dimension
is ``10.80 mm,'' the part is an affected slat track and must be
replaced. AAL questioned whether a slat track with a measurement other
than 10.80 mm would be affected. Therefore, AAL requested that Airbus
provide a specific tolerance range that would require further
inspection and ultimate replacement. AAL stated that Airbus provided a
range of between 10.763 mm and 11.275 mm for the part to be an affected
slat track, which will be added to the next revision of the referenced
service bulletin.
    The FAA agrees with the commenter's request for the reasons
provided. Paragraph (h)(3) has been added to this AD to specify the
measured dimension range of 10.763 mm through 11.275 mm inclusive for
an affected part. Subsequent paragraphs have been redesignated
accordingly.

Conclusion

    The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule with the changes described previously
and minor editorial changes. The FAA has determined that these minor
changes:
     Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was
already proposed in the NPRM.
    The FAA has also determined that these changes will not increase
the economic burden on any operator or increase the scope of this final
rule.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2019-0026 describes procedures for one-time detailed and
special detailed (high frequency eddy current) inspections for cracking
of the aft lug of each affected wing slat track (including an
inspection to first determine if an affected slat track is installed),
and replacement of any affected part with a serviceable part. This
material 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.

Costs of Compliance

    The FAA estimates that this AD affects 104 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
7 work-hours x $85 per hour = $595...........................              $0             $595          $61,880
----------------------------------------------------------------------------------------------------------------

    The FAA estimates the following costs to do any necessary on-
condition action that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need this on-condition action:

                 Estimated Costs of On-Condition Action
------------------------------------------------------------------------
                                                             Cost per
              Labor cost                   Parts cost        product
------------------------------------------------------------------------
8 work-hours x $85 per hour = $680....              $0             $680
------------------------------------------------------------------------

    According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in the 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.
    The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
    This 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 and
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

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):

2019-17-05 Airbus SAS: Amendment 39-19725; Docket No. FAA-2019-0320;
Product Identifier 2019-NM-017-AD.

(a) Effective Date

    This AD is effective October 15, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the airplanes identified in paragraphs (c)(1)
through (6) of this AD, certificated in any category, as identified
in European Aviation Safety Agency (EASA) AD 2019-0026, dated
February 4, 2019 (``EASA AD 2019-0026'').
    (1) Airbus SAS Model A330-223F and -243F airplanes.
    (2) Airbus SAS Model A330-201, -202, -203, -223, and -243
airplanes.
    (3) Airbus SAS Model A330-301, -302, -303, -321, -322, -323, -
341, -342, and -343 airplanes.
    (4) Airbus SAS Model A340-211, -212, and -213 airplanes.
    (5) Airbus SAS Model A340-311, -312, and -313 airplanes.
    (6) Airbus SAS Model A340-541 and -642 airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

(e) Reason

    This AD was prompted by a determination that certain wing slat
tracks that had been inadvertently indicated as eligible for
installation on all Model A330 and A340 series airplanes are unable
to sustain the ultimate loads relative to the weight variant of
certain airplane configurations. The FAA is issuing this AD to
address installation of affected parts, which could result in slat
detachment in flight and consequent reduced control of the airplane.

(f) Compliance

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

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2019-0026.

(h) Exceptions to EASA AD 2019-0026

    (1) For purposes of determining compliance with the requirements
of this AD:

Where EASA AD 2019-0026 refers to its effective date, this AD
requires using the effective date of this AD.
    (2) Where EASA AD 2019-0026 requires inspecting to determine the
part number of the wing slat tracks at the #10 position, this AD
allows a review of airplane maintenance records in lieu of the
inspection if the part number can be conclusively determined from
that review.
    (3) EASA AD 2019-0026 refers to Airbus Service Bulletin A330-57-
3144, dated November 12, 2018, which specifies that if the slat
track part number is not identifiable, the upper thickness of the
aft lug must be measured, and if the dimension is 10.80 millimeters
(mm), it is an affected part and must be replaced. For this AD, the
affected part dimensions range from 10.763 mm through 11.275 mm
inclusive.
    (4) The ``Remarks'' section of EASA AD 2019-0026 does not apply
to this AD.

(i) 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 (j) of this AD. 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.
    (2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS's
EASA Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
    (3) Required for Compliance (RC): For any service information
referenced in EASA AD 2019-0026 that contains RC procedures and
tests: Except as required by paragraph (i)(2) of this AD, RC
procedures and tests must be done to comply with this AD; any
procedures or tests that are not identified as RC are recommended.
Those procedures and tests that are not identified as RC may be
deviated from using accepted methods in accordance with the
operator's maintenance or inspection program without obtaining
approval of an AMOC, provided the procedures and tests identified as
RC can be done and the airplane can be put back in an airworthy
condition. Any substitutions or changes to procedures or tests
identified as RC require approval of an AMOC.

(j) Related Information

    For more information about this AD, contact Vladimir Ulyanov,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax:<PHONE_NUMBER>.

(k) 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) European Aviation Safety Agency (EASA) AD 2019-0026, dated
February 4, 2019.
    (ii) [Reserved]
    (3) For EASA AD 2019-0026, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 89990 6017; email
<EMAIL_ADDRESS>internet www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://ad.easa.europa.eu.
    (4) You may view this EASA AD 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>. EASA AD
2019-0026 may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-
2019-0320.
    (5) You may view this material that is incorporated by reference
at the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, call 202-
741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Des Moines, Washington, on August 22, 2019.
Suzanne Masterson,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-19442 Filed 9-9-19; 8:45 am]
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