82 FR 32494 - Airworthiness Directives; GEVEN S.p.A., Seat Assemblies, Type D1-02 and D1-03

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 134 (July 14, 2017)

Page Range		32494-32496
FR Document		2017-14546

We propose to adopt a new airworthiness directive (AD) for certain Geven S.p.A., Type D1-02 and D1-03 seat assemblies. This proposed AD was prompted by a report that seat belt attachment bolts were found detached or partially detached from the seat. This proposed AD would require inspection, torque verification, and modification of certain model seats. We are proposing this AD to correct the unsafe condition on these products.

Federal Register, Volume 82 Issue 134 (Friday, July 14, 2017)

[Federal Register Volume 82, Number 134 (Friday, July 14, 2017)]
[Proposed Rules]
[Pages 32494-32496]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-14546]


=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0504; Directorate Identifier 2017-NE-12-AD]
RIN 2120-AA64


Airworthiness Directives; GEVEN S.p.A., Seat Assemblies, Type D1-
02 and D1-03

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Geven S.p.A., Type D1-02 and D1-03 seat assemblies. This 
proposed AD was prompted by a report that seat belt attachment bolts 
were found detached or partially detached from the seat. This proposed 
AD would require inspection, torque verification, and modification of 
certain model seats. We are proposing this AD to correct the unsafe 
condition on these products.

DATES: We must receive comments on this NPRM by August 28, 2017.

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.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 1200 New Jersey Avenue SE., West Building, Ground 
Floor, Room W12-140, Washington, DC 20590-0001.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax: 202-493-2251.
    For service information identified in this NPRM, contact Geven 
Technical Assistance Department, Via Boscofangone, Zona Industriale 
Nola-Marigliano, 80035 Nola (NA), Italy; phone: +39 081 31 21 396; fax: 
+39 081 31 21 321; email: [email protected]. You may view 
this service information at the FAA, Engine & Propeller Directorate, 
1200 District Avenue, Burlington, MA. For information on the 
availability of this material at the FAA, call 781-238-7125.

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-2017-
0504; 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 mandatory continuing airworthiness 
information (MCAI), the regulatory evaluation, any comments received, 
and other information. The address for the Docket Office (phone: 800-
647-5527) is in the ADDRESSES section. Comments will be available in 
the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Neil Doh, Aerospace Engineer, Boston 
Aircraft Certification Office, FAA, Engine & Propeller Directorate, 
1200 District Avenue, Burlington, MA 01803; phone: 781-238-7757; fax: 
781-238-7199; email: [email protected].

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-2017-0504; 
Directorate Identifier 2017-NE-12-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 
with FAA personnel concerning this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued EASA 
AD 2014-0187, dated August 20, 2014 (referred to hereinafter as ``the 
MCAI''), to correct an unsafe condition for the specified products. The 
MCAI states:

    An operator reported that seat belt attachment bolts were found 
detached or partially detached from the seat. A further check on 
several aeroplanes revealed that on a large number of seats of the 
same model, the seat belt attachment bolts were not properly torqued 
and secured as defined. This condition, if not detected and 
corrected, could lead to failure of the seats to perform their 
intended function, possibly resulting in injury to occupants in case 
of an emergency landing. To address this potential unsafe condition, 
Geven published SB No. D103-25-004 to provide inspection 
instructions to verify if the seat belt attachment bolts are 
properly torqued and secured, and correction of any deficiencies. In 
addition, for certain D1-03 seats, the SB provides instructions to 
modify the seat belt attachment assembly. For the reasons described 
above, this AD requires a one-time inspection of all safety belt 
attachment bolts and, depending on findings, accomplishment of the 
applicable corrective action(s). This AD also requires modification 
of the seat belt attachment assembly on certain D1-03 seats.

    You may obtain further information by examining the MCAI in the AD 
docket on the Internet at http://www.regulations.gov by searching for 
and locating Docket No. FAA-2017-0504.

[[Page 32495]]

Related Service Information Under 1 CFR Part 51

    Geven S.p.A. has issued Service Bulletin (SB) No. D103-25-004, 
Revision 4, dated March 15, 2016. The SB describes procedures for 
inspection, torque verification, and modification of certain model 
seats known to be installed on ATR 42 and ATR 72 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 Italy, 
and is approved for operation in the United States. Pursuant to our 
bilateral agreement with the European Community, EASA has notified us 
of the unsafe condition described in the MCAI and service information 
referenced above. We are proposing this AD because we evaluated all 
information provided by EASA and determined the unsafe condition exists 
and is likely to exist or develop on other products of the same type 
design. This proposed AD would require inspection, torque verification 
and modification of certain model seats.

Costs of Compliance

    We estimate that this proposed AD affects an unknown number of seat 
assemblies installed on, but not limited to, 38 ATR 42 and ATR 72 
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
----------------------------------------------------------------------------------------------------------------
Seat modification ATR 42...........  1.5 work-hours x $85 per               $302         $429.50      $10,737.50
                                      hour = $127.50.
Torque check ATR 42................  0.8 work-hours x $85 per                  0           68.00        1,700.00
                                      hour = $68.00.
Seat modification ATR 72...........  2.3 work-hours x $85 per                368          563.50        7,325.50
                                      hour = $195.50.
Seat remove and replace ATR 72.....  1.2 work-hours x $85 per                  0          102.00        1,326.00
                                      hour = $102.00.
----------------------------------------------------------------------------------------------------------------

    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 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 to the extent 
that it justifies making a regulatory distinction, 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):

GEVEN S.p.A.: Docket No. FAA-2017-0504; Directorate Identifier 2017-
NE-12-AD.

(a) Comments Due Date

    We must receive comments by August 28, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all GEVEN S.p.A. (Geven) Type D1-02 and D1-03 
(also known as ``Lightweight Classic'' and ``Lightweight Prestige'') 
seats, with part numbers (P/Ns) and Effectivity Codes listed in 
Table 1.1.1 of Geven Service Bulletin (SB) No. D103-25-004, Revision 
4, dated March 15, 2016.
    These appliances are installed on, but not limited to, ATR 42 
and ATR 72 airplanes of U.S. registry.

(d) Subject

    Joint Aircraft System Component (JASC) 2500 Code, Cabin 
Equipment/Furnishings.

(e) Reason

    This AD was prompted by a report that seat belt attachment bolts 
were found detached or partially detached from the seat. We are 
issuing this AD to prevent failure of the seats.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.
    (1) For all Geven Type D1-02 and D1-03 (also known as 
``Lightweight Classic'' and ``Lightweight Prestige'') in-arm table, 
standard, and last row seats, P/N D1-02-( )( )( )-( )( )( ), and P/N 
D1-03-( )( )( )-( )( )( ), within 6 months after the effective date 
of this AD, modify the safety belt attachment assemblies on the 
aisle side spreader, and torque check the safety belt attachment 
assemblies on the central and fuselage side spreaders to 71 in-lbs 
(8 nm)

[[Page 32496]]

using Geven SB No. D103-25-004, Revision 4, dated March 15, 2016, 
and
    (2) For all Geven Type D1-02 and D1-03 (also known as 
``Lightweight Classic'' and ``Lightweight Prestige'') aft facing 
seats, P/N D1-02-( )( )( )-( )( )( ), and P/N D1-03-( )( )( )-( )( 
)( ), within 6 months after the effective date of this AD, torque 
check the seat belt attachment assemblies on the aisle side, 
central, and fuselage side spreaders to 71 in-lbs using Geven SB No. 
D103-25-004, Revision 4, dated March 15, 2016, and
    (3) Within 6 months after the effective date of this AD, verify 
that the safety belt attachment is free to rotate. If it is not free 
to rotate, replace the bushing in accordance with paragraph 3.3.1 of 
Geven SB No. D103-25-004, Revision 4, dated March 15, 2016, or
    (4) Within 6 months after the effective date of this AD, block 
each affected seat to prevent use of each affected seat until 
paragraphs (f)(1), (2), and (3) of this AD are accomplished.

(g) Credit for Previous Actions

    You may take credit for the inspections, torque verifications, 
and modifications that are required by paragraphs (f)(1), (2), and 
(3) of this AD if you performed those actions before the effective 
date of this AD using Geven SB No. D103-25-004, Revision 4, dated 
March 15, 2016.

(h) Alternative Methods of Compliance (AMOCs)

    The Manager, Boston Aircraft Certification Office, FAA, may 
approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 
to make your request.

(i) Related Information

    (1) For more information about this AD, contact Neil Doh, 
Aerospace Engineer, Boston Aircraft Certification Office, FAA, 
Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 
01803; phone: 781-238-7757; fax: 781-238-7199; email: 
[email protected].
    (2) Refer to MCAI EASA AD 2014-0187, dated August 20, 2014, for 
more information. You may examine the MCAI in the AD docket on the 
Internet at http://www.regulations.gov by searching for and locating 
it in Docket No. FAA-2017-0504.
    (3) Geven SB No. D103-25-004, Revision 4, dated March 15, 2016 
can be obtained from Geven Technical Assistance Department, using 
the contact information in paragraph (i)(4) of this proposed AD.
    (4) For service information identified in this proposed AD, 
contact Geven Technical Assistance Department, Via Boscofangone, 
Zona Industriale Nola-Marigliano, 80035 Nola (NA), Italy; phone: +39 
081 31 21 396; fax: +39 081 31 21 321; email: 
[email protected].
    (5) You may view this service information at the FAA, Engine & 
Propeller Directorate, 1200 District Avenue, Burlington, MA. For 
information on the availability of this material at the FAA, call 
781-238-7125.

    Issued in Burlington, Massachusetts, on July 6, 2017.
Robert J. Ganley,
Acting Manager, Engine & Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-14546 Filed 7-13-17; 8:45 am]
BILLING CODE 4910-13-P

Federal Register / Vol. 82, No. 134 / Friday, July 14, 2017 / Proposed Rules 32495

Related Service Information Under 1 FAA’s Determination and Requirements products of the same type design. This
CFR Part 51 of This Proposed AD proposed AD would require inspection,
Geven S.p.A. has issued Service This product has been approved by torque verification and modification of
Bulletin (SB) No. D103–25–004, the aviation authority of Italy, and is certain model seats.
Revision 4, dated March 15, 2016. The approved for operation in the United Costs of Compliance
SB describes procedures for inspection, States. Pursuant to our bilateral
torque verification, and modification of agreement with the European We estimate that this proposed AD
certain model seats known to be Community, EASA has notified us of affects an unknown number of seat
installed on ATR 42 and ATR 72 the unsafe condition described in the assemblies installed on, but not limited
airplanes. This service information is MCAI and service information to, 38 ATR 42 and ATR 72 airplanes of
reasonably available because the referenced above. We are proposing this U.S. registry.
interested parties have access to it AD because we evaluated all
through their normal course of business information provided by EASA and We estimate the following costs to
or by the means identified in the determined the unsafe condition exists comply with this proposed AD:
ADDRESSES section. and is likely to exist or develop on other

ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators

Seat modification ATR 42 ............................... 1.5 work-hours × $85 per hour = $127.50 ..... $302 $429.50 $10,737.50
Torque check ATR 42 ..................................... 0.8 work-hours × $85 per hour = $68.00 ....... 0 68.00 1,700.00
Seat modification ATR 72 ............................... 2.3 work-hours × $85 per hour = $195.50 ..... 368 563.50 7,325.50
Seat remove and replace ATR 72 .................. 1.2 work-hours × $85 per hour = $102.00 ..... 0 102.00 1,326.00

According to the manufacturer, some distribution of power and GEVEN S.p.A.: Docket No. FAA–2017–0504;
of the costs of this proposed AD may be responsibilities among the various Directorate Identifier 2017–NE–12–AD.
covered under warranty, thereby levels of government. (a) Comments Due Date
reducing the cost impact on affected For the reasons discussed above, I We must receive comments by August 28,
individuals. We do not control warranty certify this proposed regulation: 2017.
coverage for affected individuals. As a (1) Is not a ‘‘significant regulatory
result, we have included all costs in our action’’ under Executive Order 12866, (b) Affected ADs
cost estimate. (2) Is not a ‘‘significant rule’’ under None.
Authority for This Rulemaking the DOT Regulatory Policies and (c) Applicability
Procedures (44 FR 11034, February 26,
Title 49 of the United States Code This AD applies to all GEVEN S.p.A.
1979), (Geven) Type D1–02 and D1–03 (also known
specifies the FAA’s authority to issue (3) Will not affect intrastate aviation as ‘‘Lightweight Classic’’ and ‘‘Lightweight
rules on aviation safety. Subtitle I, in Alaska to the extent that it justifies Prestige’’) seats, with part numbers (P/Ns)
section 106, describes the authority of making a regulatory distinction, and and Effectivity Codes listed in Table 1.1.1 of
the FAA Administrator. ‘‘Subtitle VII: (4) Will not have a significant Geven Service Bulletin (SB) No. D103–25–
Aviation Programs,’’ describes in more economic impact, positive or negative, 004, Revision 4, dated March 15, 2016.
detail the scope of the Agency’s on a substantial number of small entities These appliances are installed on, but not
authority. under the criteria of the Regulatory limited to, ATR 42 and ATR 72 airplanes of
We are issuing this rulemaking under U.S. registry.
Flexibility Act.
the authority described in ‘‘Subtitle VII, (d) Subject
Part A, Subpart III, Section 44701: List of Subjects in 14 CFR Part 39
Joint Aircraft System Component (JASC)
General requirements.’’ Under that Air transportation, Aircraft, Aviation 2500 Code, Cabin Equipment/Furnishings.
section, Congress charges the FAA with safety, Incorporation by reference,
promoting safe flight of civil aircraft in (e) Reason
Safety.
air commerce by prescribing regulations This AD was prompted by a report that seat
for practices, methods, and procedures The Proposed Amendment belt attachment bolts were found detached or
the Administrator finds necessary for partially detached from the seat. We are
Accordingly, under the authority
issuing this AD to prevent failure of the seats.
safety in air commerce. This regulation delegated to me by the Administrator,
is within the scope of that authority the FAA proposes to amend 14 CFR part (f) Compliance
because it addresses an unsafe condition 39 as follows: Comply with this AD within the
that is likely to exist or develop on compliance times specified, unless already
products identified in this rulemaking PART 39—AIRWORTHINESS done.
action. DIRECTIVES (1) For all Geven Type D1–02 and D1–03
(also known as ‘‘Lightweight Classic’’ and
mstockstill on DSK30JT082PROD with PROPOSALS

Regulatory Findings ■ 1. The authority citation for part 39 ‘‘Lightweight Prestige’’) in-arm table,
We determined that this proposed AD continues to read as follows: standard, and last row seats, P/N D1–02–
( )( )( )–( )( )( ), and P/N D1–03–( )( )( )–
would not have federalism implications Authority: 49 U.S.C. 106(g), 40113, 44701. ( )( )( ), within 6 months after the effective
under Executive Order 13132. This date of this AD, modify the safety belt
proposed AD would not have a § 39.13 [Amended]
attachment assemblies on the aisle side
substantial direct effect on the States, on ■ 2. The FAA amends § 39.13 by adding spreader, and torque check the safety belt
the relationship between the national the following new airworthiness attachment assemblies on the central and
Government and the States, or on the directive (AD): fuselage side spreaders to 71 in-lbs (8 nm)

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32496 Federal Register / Vol. 82, No. 134 / Friday, July 14, 2017 / Proposed Rules

using Geven SB No. D103–25–004, Revision Issued in Burlington, Massachusetts, on Bombardier, Inc., Q-Series Technical
4, dated March 15, 2016, and July 6, 2017. Help Desk, 123 Garratt Boulevard,
(2) For all Geven Type D1–02 and D1–03 Robert J. Ganley, Toronto, Ontario M3K 1Y5, Canada;
(also known as ‘‘Lightweight Classic’’ and Acting Manager, Engine & Propeller telephone 416–375–4000; fax 416–375–
‘‘Lightweight Prestige’’) aft facing seats, P/N Directorate, Aircraft Certification Service. 4539; email thd.qseries@
D1–02–( )( )( )–( )( )( ), and P/N D1–03– [FR Doc. 2017–14546 Filed 7–13–17; 8:45 am] aero.bombardier.com; Internet http://
( )( )( )–( )( )( ), within 6 months after the BILLING CODE 4910–13–P www.bombardier.com. You may view
effective date of this AD, torque check the this referenced service information at
seat belt attachment assemblies on the aisle the FAA, Transport Airplane
side, central, and fuselage side spreaders to DEPARTMENT OF TRANSPORTATION Directorate, 1601 Lind Avenue SW.,
71 in-lbs using Geven SB No. D103–25–004, Renton, WA. For information on the
Revision 4, dated March 15, 2016, and Federal Aviation Administration availability of this material at the FAA,
(3) Within 6 months after the effective date call 425–227–1221.
of this AD, verify that the safety belt 14 CFR Part 39
attachment is free to rotate. If it is not free Examining the AD Docket
[Docket No. FAA–2015–8434; Directorate
to rotate, replace the bushing in accordance You may examine the AD docket on
Identifier 2015–NM–082–AD]
with paragraph 3.3.1 of Geven SB No. D103– the Internet at http://
25–004, Revision 4, dated March 15, 2016, or RIN 2120–AA64 www.regulations.gov by searching for
(4) Within 6 months after the effective date and locating Docket No. FAA–2015–
of this AD, block each affected seat to prevent Airworthiness Directives; Bombardier,
8434; or in person at the Docket
use of each affected seat until paragraphs Inc., Airplanes
Management Facility between 9 a.m.
(f)(1), (2), and (3) of this AD are and 5 p.m., Monday through Friday,
AGENCY: Federal Aviation
accomplished. except Federal holidays. The AD docket
Administration (FAA), DOT.
(g) Credit for Previous Actions ACTION: Supplemental notice of contains this proposed AD, the
You may take credit for the inspections, proposed rulemaking (SNPRM); regulatory evaluation, any comments
torque verifications, and modifications that reopening of comment period. received, and other information. The
are required by paragraphs (f)(1), (2), and (3) street address for the Docket Office
of this AD if you performed those actions
SUMMARY: We are revising an earlier (telephone: 800–647–5527) is in the
before the effective date of this AD using
proposal for certain Bombardier, Inc., ADDRESSES section. Comments will be
Geven SB No. D103–25–004, Revision 4, Model DHC–8–401 and –402 airplanes. available in the AD docket shortly after
dated March 15, 2016. This action revises the notice of receipt.
proposed rulemaking (NPRM) by adding FOR FURTHER INFORMATION CONTACT:
(h) Alternative Methods of Compliance certain airplanes to the applicability and Cesar Gomez, Aerospace Engineer,
(AMOCs) adding specified actions. We are Airframe and Mechanical Systems
The Manager, Boston Aircraft Certification proposing this airworthiness directive Branch, ANE–171, FAA, New York
Office, FAA, may approve AMOCs for this (AD) to address the unsafe condition on Aircraft Certification Office (ACO), 1600
AD. Use the procedures found in 14 CFR these products. Since these changes Stewart Avenue, Suite 410, Westbury,
39.19 to make your request. increase the scope of the NPRM, we are NY 11590; telephone 516–228–7318; fax
(i) Related Information reopening the comment period to allow 516–794–5531.
the public the chance to comment on SUPPLEMENTARY INFORMATION:
(1) For more information about this AD, these proposed changes.
contact Neil Doh, Aerospace Engineer, Comments Invited
DATES: The comment period for the
Boston Aircraft Certification Office, FAA,
NPRM published in the Federal We invite you to send any written
Engine & Propeller Directorate, 1200 District
Register on January 13, 2016 (81 FR relevant data, views, or arguments about
Avenue, Burlington, MA 01803; phone: 781–
238–7757; fax: 781–238–7199; email: 1586), is reopened. this proposal. Send your comments to
neil.doh@faa.gov.
We must receive comments on this an address listed under the ADDRESSES
(2) Refer to MCAI EASA AD 2014–0187, SNPRM by August 28, 2017. section. Include ‘‘Docket No. FAA–
dated August 20, 2014, for more information. ADDRESSES: You may send comments, 2015–8434; Directorate Identifier 2015–
You may examine the MCAI in the AD using the procedures found in 14 CFR NM–082–AD’’ at the beginning of your
docket on the Internet at http:// 11.43 and 11.45, by any of the following comments. We specifically invite
www.regulations.gov by searching for and methods: comments on the overall regulatory,
locating it in Docket No. FAA–2017–0504. • Federal eRulemaking Portal: Go to economic, environmental, and energy
(3) Geven SB No. D103–25–004, Revision http://www.regulations.gov. Follow the aspects of this proposed AD. We will
4, dated March 15, 2016 can be obtained from instructions for submitting comments. consider all comments received by the
Geven Technical Assistance Department, • Fax: 202–493–2251. closing date and may amend this
using the contact information in paragraph • Mail: U.S. Department of proposed AD based on those comments.
(i)(4) of this proposed AD. Transportation, Docket Operations, M– We will post all comments we
(4) For service information identified in 30, West Building, Ground Floor, Room receive, without change, to http://
this proposed AD, contact Geven Technical W12–140, 1200 New Jersey Avenue SE., www.regulations.gov, including any
Assistance Department, Via Boscofangone, Washington, DC 20590. personal information you provide. We
Zona Industriale Nola-Marigliano, 80035 • Hand Delivery: U.S. Department of will also post a report summarizing each
mstockstill on DSK30JT082PROD with PROPOSALS

Nola (NA), Italy; phone: +39 081 31 21 396; Transportation, Docket Operations, M– substantive verbal contact we receive
fax: +39 081 31 21 321; email: 30, West Building, Ground Floor, Room about this proposed AD.
Technical.assistance@geven.com. W12–140, 1200 New Jersey Avenue SE.,
(5) You may view this service information Washington, DC, between 9 a.m. and 5 Discussion
at the FAA, Engine & Propeller Directorate, p.m., Monday through Friday, except We issued an NPRM to amend 14 CFR
1200 District Avenue, Burlington, MA. For Federal holidays. part 39 by adding an AD that would
information on the availability of this • For service information identified apply to certain Bombardier, Inc. Model
material at the FAA, call 781–238–7125. in this proposed AD, contact DHC–8–401 and –402 airplanes. The

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Document Created: 2018-10-24 11:17:26
Document Modified: 2018-10-24 11:17:26

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Proposed Rules
Action		Notice of proposed rulemaking (NPRM).
Dates		We must receive comments on this NPRM by August 28, 2017.
Contact		Neil Doh, Aerospace Engineer, Boston Aircraft Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7757; fax: 781-238-7199; email: [email protected]
FR Citation		82 FR 32494
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

82 FR 32494 - Airworthiness Directives; GEVEN S.p.A., Seat Assemblies, Type D1-02 and D1-03

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 82, Issue 134 (July 14, 2017)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration