Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 59963-59967 [2017-26949]
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Federal Register / Vol. 82, No. 241 / Monday, December 18, 2017 / Rules and Regulations
paragraph (j)(1), (j)(2), or (j)(3) of this AD, as
applicable.
(1) Airbus Service Bulletin A330–27–3218,
Revision 00, dated July 1, 2016.
(2) Airbus Service Bulletin A340–27–4203,
Revision 00, dated July 1, 2016.
(3) Airbus Service Bulletin A340–27–5067,
Revision 00, dated July 1, 2016.
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(k) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal
inspector or local Flight Standards District
Office, as appropriate. If sending information
directly to the International Section, send it
to the attention of the person identified in
paragraph (l)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
actions from a manufacturer, the action must
be accomplished using a method approved
by the Manager, International Section,
Transport Standards Branch, FAA; or the
European Aviation Safety Agency (EASA); or
Airbus’s EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
(3) Required for Compliance (RC): Except
as required by paragraph (h)(2) of this AD: If
any service information contains procedures
or tests that are identified as RC, those
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.
(l) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2017–0044, dated March 9, 2017, for related
information. This MCAI may be found in the
AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2017–0627.
(2) For more information about this AD,
contact Vladimir Ulyanov, Aerospace
Engineer, International Section, Transport
Standards Branch, FAA, 1601 Lind Avenue
SW, Renton, WA 98057–3356; telephone:
425–227–1138; fax: 425–227–1149.
(3) Service information identified in this
AD that is not incorporated by reference is
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available at the addresses specified in
paragraphs (m)(3) and (m)(4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A330–27–3218,
Revision 01, dated December 5, 2016.
(ii) Airbus Service Bulletin A340–27–4203,
Revision 01, dated December 5, 2016.
(iii) Airbus Service Bulletin A340–27–
5067, Revision 01, dated December 5, 2016.
(3) For service information identified in
this AD, contact Airbus SAS, Airworthiness
Office—EAL, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France; telephone: +33
5 61 93 36 96; fax: +33 5 61 93 45 80; email:
airworthiness.A330–A340@airbus.com;
internet: https://www.airbus.com.
(4) You may view this service information
at the FAA, Transport Standards Branch,
1601 Lind Avenue SW, Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on
December 5, 2017.
Dionne Palermo,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2017–26837 Filed 12–15–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–1170; Product
Identifier 2013–NM–054–AD; Amendment
39–19129; AD 2017–25–15]
RIN 2120–AA64
Airworthiness Directives; ATR–GIE
´
Avions de Transport Regional
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
´
ATR–GIE Avions de Transport Regional
Model ATR42–300 and –500 airplanes
and Model ATR72–202 and –212A
airplanes. This AD requires identifying
SUMMARY:
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59963
the serial number of the dual distributor
valve (DDV), and replacement of
affected DDVs. This AD was prompted
by an investigation performed on a
failed DDV that revealed a
nonconformity of crimping on an
internal valve. We are issuing this AD
to address the unsafe condition on these
products.
DATES: This AD becomes effective
January 2, 2018.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of January 2, 2018.
We must receive comments on this
AD by February 1, 2018.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC, between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this final rule, contact ATR–GIE Avions
´
´
de Transport Regional, 1, Allee Pierre
Nadot, 31712 Blagnac Cedex, France;
telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email
continued.airworthiness@atraircraft.com. You may view this
referenced service information at the
FAA, Transport Standards Branch, 1601
Lind Avenue SW, Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
It is also available on the internet at
https://www.regulations.gov by searching
for and locating Docket No. FAA–2017–
1170.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
1170; or in person at the Docket
Operations office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this AD, the regulatory
evaluation, any comments received, and
other information. The street address for
the Docket Operations office (telephone
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Federal Register / Vol. 82, No. 241 / Monday, December 18, 2017 / Rules and Regulations
800–647–5527) is in the ADDRESSES
section. Comments will be available in
the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Shahram Daneshmandi, Aerospace
Engineer, International Section,
Transport Standards Branch, FAA, 1601
Lind Avenue SW, Renton, WA 98057–
3356; telephone 425–227–1112; fax
425–227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency
(EASA), which is the Technical Agent
for the Member States of the European
Union, has issued EASA Airworthiness
Directive, 2013–0032, dated February
18, 2013 (referred to after this as the
Mandatory Continuing Airworthiness
Information, or ‘‘the MCAI’’), to correct
an unsafe condition for certain ATR–
´
GIE Avions de Transport Regional
Model ATR42–300 and –500 airplanes
and Model ATR72–202 and –212A
airplanes. The MCAI states:
During the investigation performed on a
failed dual distributor valve (DDV) shipped
to the DDV manufacturer, a non-conformity
of crimping on an internal valve has been
detected by the DDV manufacturer. This
defective crimping creates a lack of tightness
that prevents the complete deflation of the
related de-icing boot chamber during de-icing
cycles.
A batch of serialized DDV, potentially
affected with the same manufacturing
discrepancy, has been identified by the DDV
manufacturer.
This condition, if not detected and
corrected, may affect the efficiency of the
pneumatic de-icing system, which could
reduce flight safety in icing conditions.
For the reasons described above, this AD
requires a one-time inspection of each DDV
to identify the serial number (s/n) and
replacement of the non-conforming DDV
units.
The affected DDV units installed on
aeroplanes and those delivered as spares
have been retraced by ATR and all noninstalled spare units have been quarantined,
which is why this AD only applies to specific
MSN [manufacturer serial number]
aeroplanes.
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You may examine the MCAI on the
internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2017–1170.
Related Service Information Under 1
CFR Part 51
´
Avions de Transport Regional has
issued the following service
information:
• ATR Service Bulletin ATR42–30–
0080, Revision 02, dated March 26,
2013.
• ATR Service Bulletin ATR42–30–
0081, Revision 02, dated March 26,
2013.
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15:19 Dec 15, 2017
Jkt 244001
• ATR Service Bulletin ATR72–30–
1049, Revision 03, dated March 26,
2013.
• ATR Service Bulletin ATR72–30–
1050, Revision 03, dated March 26,
2013.
This service information describes
procedures for identifying and replacing
affected DDVs. These documents are
distinct since they apply to different
airplane models. 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 of this AD.
FAA’s Determination and Requirements
of This AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are issuing this
AD because we evaluated all pertinent
information and determined the unsafe
condition exists and is likely to exist or
develop on other products of these same
type designs.
FAA’s Determination of the Effective
Date
There are currently no domestic
operators of this product. Therefore, we
find good cause that notice and
opportunity for prior public comment
are unnecessary. In addition, for the
reason(s) stated above, we find that good
cause exists for making this amendment
effective in less than 30 days.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not precede it by notice and
opportunity for public comment. We
invite you to send any written relevant
data, views, or arguments about this AD.
Send your comments to an address
listed under the ADDRESSES section.
Include ‘‘Docket No. FAA–2017–1170;
Product Identifier 2013–NM–054–AD’’
at the beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
this AD. We will consider all comments
received by the closing date and may
amend this AD based on those
comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
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substantive verbal contact we receive
about this AD.
Costs of Compliance
Currently, there are no affected
airplanes on the U.S. Register. If an
affected airplane is imported and placed
on the U.S. Register in the future, we
provide the following cost estimates to
comply with this AD. We estimate that
it will take about 84 work-hours per
product to comply with the basic
requirements of this AD. The average
labor rate is $85 per work-hour.
Required parts will cost about $12,000
per product. Based on these figures, we
estimate the cost of this AD to be
$19,140 per product.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. ‘‘Subtitle VII:
Aviation Programs,’’ describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in ‘‘Subtitle VII,
Part A, Subpart III, Section 44701:
General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
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 to the Director of the System
Oversight Division.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
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Federal Register / Vol. 82, No. 241 / Monday, December 18, 2017 / Rules and Regulations
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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
(a) Effective Date
This AD becomes effective January 2, 2018.
(b) Affected ADs
None.
(f) Compliance
(c) Applicability
This AD applies to ATR—GIE Avions de
´
Transport Regional airplanes, certificated in
any category, identified in paragraphs (c)(1)
through (c)(6) of this AD.
Note 1 to the introductory text of
paragraph (c) of this AD: In EASA AD 2013–
0032, dated February 18, 2013, airplanes
specified in paragraphs (c)(1) and (c)(2) of
this AD are identified as Group 1 airplanes
and airplanes specified in paragraphs (c)(3)
through (c)(6) of this AD are identified as
Group 2 airplanes.
(1) Model ATR42–500 airplanes:
Manufacturer serial numbers (MSNs) 645,
653, 657, 659, 661, 663, and 665.
(2) Model ATR72–212A airplanes: MSNs
778, 994, 995, 996, 998, 999, 1000, and 1020.
(3) Model ATR42–300 airplanes: MSNs 348
and 415.
(4) Model ATR42–500 airplanes: MSNs
497, 501, and 514.
(5) Model ATR72–202 airplanes: MSNs
192, 411, 496, 508, and 509.
(6) Model ATR72–212A airplanes: MSNs
468, 568, 595, 662, 796, 920, 926, 950, 1024,
1025, 1028, 1029, 1031, 1032, 1033, 1034,
1035, 1036, 1037, 1039, and 1040.
■
(d) Subject
Air Transport Association (ATA) of
America Code 30, Ice and Rain Protection.
2017–25–15 ATR—GIE Avions de
´
Transport Regional: Amendment 39–
19129; Docket No. FAA–2017–1170;
Product Identifier 2013–NM–054–AD.
(e) Reason
This AD was prompted by an investigation
performed on a failed dual distributor valve
(DDV) that revealed a nonconformity of
crimping on an internal valve. We are issuing
this AD to prevent the deflation of the related
§ 39.13
[Amended]
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2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
(i) Corrective Action
If, during the part identification required
by paragraph (g) of this AD, any DDV
identified in figure 1 to paragraphs (h) and
(i) of this AD is found: At the applicable time
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15:19 Dec 15, 2017
Jkt 244001
specified in figure 2 to the introductory text
of paragraph (i) of this AD, depending on the
location and the number of DDV affected,
and on whether the airplane is operated in
icing conditions or under Extended
Operations (ETOPS) rules, replace any
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deicing boot chamber during deicing cycles,
which could result in reduced controllability
of the airplane in icing conditions.
Sfmt 4700
Comply with this AD within the
compliance times specified, unless already
done.
(g) Part Identification
Within 6 months after the effective date of
this AD, identify the serial number of the
DDV as specified in paragraph (g)(1) or (g)(2)
of this AD, as applicable. A review of
airplane delivery or maintenance records is
acceptable to make the identification as
required by this paragraph, provided those
records can be relied upon for that purpose,
and the serial number of the DDV can be
conclusively identified from that review.
(1) For airplanes identified in paragraphs
(c)(1) and (c)(2) of this AD, identify the serial
number of the engine DDV part number
(P/N) B03AA1060, in accordance with the
Accomplishment Instructions of ATR Service
Bulletin ATR42–30–0081, Revision 02, dated
March 26, 2013; or ATR72–30–1050,
Revision 03, dated March 26, 2013; as
applicable to airplane model.
(2) For airplanes identified in paragraphs
(c)(3), (c)(4), (c)(5), and (c)(6) of this AD,
identify the serial number of the wing and/
or stabilizer DDV, P/N B03AA1031 or
B03AA1040, in accordance with the
Accomplishment Instructions of ATR Service
Bulletin ATR42–30–0080, Revision 02, dated
March 26, 2013; or ATR72–30–1049,
Revision 03, dated March 26, 2013; as
applicable to airplane model.
(h) Definition of Serviceable DDV
For purposes of this AD, a serviceable DDV
is any DDV having a serial number listed in
figure 1 to paragraphs (h) and (i) of this AD
with a suffix ‘‘R’’ added to the serial number.
affected DDV(s) with a new or serviceable
DDV, in accordance with the
Accomplishment Instructions of the
applicable service information specified in
paragraphs (i)(1) through (i)(4) of this AD.
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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.
59965
Federal Register / Vol. 82, No. 241 / Monday, December 18, 2017 / Rules and Regulations
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(1) For airplanes identified in paragraphs
(c)(3) and (c)(4) of this AD: ATR Service
Bulletin ATR42–30–0080, Revision 02, dated
March 26, 2013.
(2) For airplanes identified in paragraph
(c)(1) of this AD: ATR Service Bulletin
ATR42–30–0081, Revision 02, dated March
26, 2013.
(3) For airplanes identified in paragraphs
(c)(5) and (c)(6) of this AD: ATR Service
Bulletin ATR72–30–1049, Revision 03, dated
March 26, 2013.
(4) For airplanes identified in paragraph
(c)(2) of this AD: ATR Service Bulletin
ATR72–30–1050, Revision 03, dated March
26, 2013.
(j) Credit for Previous Actions
This paragraph provides credit for actions
required by paragraph (g) of this AD, if those
actions were performed before the effective
date of this AD using the service information
identified in paragraphs (j)(1) through (j)(10)
of this AD, as applicable. This service
information is not incorporated by reference
in this AD.
(1) ATR Service Bulletin ATR42–30–0080,
dated October 18, 2012 (for Model ATR42–
300 and –500 airplanes).
(2) ATR Service Bulletin ATR42–30–0080,
Revision 01, dated February 5, 2013 (for
Model ATR42–300 and –500 airplanes).
(3) ATR Service Bulletin ATR42–30–0081,
dated October 18, 2012 (for Model ATR42–
500 airplanes).
(4) ATR Service Bulletin ATR42–30–0081,
Revision 01, dated February 5, 2013 (for
Model ATR42–500 airplanes).
VerDate Sep<11>2014
15:19 Dec 15, 2017
Jkt 244001
(5) ATR Service Bulletin ATR72–30–1049,
dated October 4, 2012 (for Model ATR72–202
and –212A airplanes).
(6) ATR Service Bulletin ATR72–30–1049,
Revision 01, dated October 10, 2012 (for
Model ATR72–202 and –212A airplanes).
(7) ATR Service Bulletin ATR72–30–1049,
Revision 02, dated February 5, 2013 (for
Model ATR72–202 and –212A airplanes).
(8) ATR Service Bulletin ATR72–30–1050,
dated October 4, 2012 (for Model ATR72–
212A airplanes).
(9) ATR Service Bulletin ATR72–30–1050,
Revision 01, dated November 6, 2012 (for
Model ATR72–212A airplanes).
(10) ATR Service Bulletin ATR72–30–
1050, Revision 02, dated February 5, 2013
(for Model ATR72–212A airplanes).
(k) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal
inspector or local Flight Standards District
Office, as appropriate. If sending information
directly to the manager of the certification
office, send it to the attention of the person
identified in paragraph (l)(2) of this AD.
Information may be emailed to: 9-ANM-116AMOC-REQUESTS@faa.gov. Before using
any approved AMOC, notify your appropriate
principal inspector, or lacking a principal
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Fmt 4700
Sfmt 4700
inspector, the manager of the local flight
standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
actions from a manufacturer, the action must
be accomplished using a method approved
by the Manager, International Section,
Transport Standards Branch, FAA; or the
European Aviation Safety Agency (EASA); or
´
ATR—GIE Avions de Transport Regional’s
EASA Design Organization Approval (DOA).
If approved by the DOA, the approval must
include the DOA-authorized signature.
(l) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2013–0032, dated February 18, 2013, for
related information. You may examine the
MCAI on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2017–1170.
(2) For more information about this AD,
contact Shahram Daneshmandi, Aerospace
Engineer, International Section, Transport
Standards Branch, FAA, 1601 Lind Avenue
SW, Renton, WA 98057–3356; telephone
425–227–1112; fax 425–227–1149.
(3) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (m)(3) and (m)(4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
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ER18DE17.004</GPH>
59966
Federal Register / Vol. 82, No. 241 / Monday, December 18, 2017 / Rules and Regulations
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) ATR Service Bulletin ATR42–30–0080,
Revision 02, dated March 26, 2013.
(ii) ATR Service Bulletin ATR42–30–0081,
Revision 02, dated March 26, 2013.
(iii) ATR Service Bulletin ATR72–30–1049,
Revision 03, dated March 26, 2013.
(iv) ATR Service Bulletin ATR72–30–1050,
Revision 03, dated March 26, 2013.
(3) For service information identified in
this AD, contact ATR—GIE Avions de
´
´
Transport Regional, 1, Allee Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33
(0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18;
email continued.airworthiness@atraircraft.com.
(4) You may view this service information
at the FAA, Transport Standards Branch,
1601 Lind Avenue SW, Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on
December 6, 2017.
Dionne Palermo,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2017–26949 Filed 12–15–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–0807; Product
Identifier 2017–NM–080–AD; Amendment
39–19126; AD 2017–25–12]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for all The
Boeing Company Model 737–100, –200,
–200C, –300, –400, and –500 series
airplanes. This AD was prompted by
reports of cracking in the webs of the
stub beams at certain fuselage stations.
These cracks are the result of fatigue
caused by cyclical loading from
pressurization, wing loads, and landing
loads. This AD requires repetitive
inspections for cracking of the webs of
the stub beams at certain fuselage
Pmangrum on DSK3GDR082PROD with RULES
SUMMARY:
VerDate Sep<11>2014
15:19 Dec 15, 2017
Jkt 244001
stations, and applicable on-condition
actions. We are issuing this AD to
address the unsafe condition on these
products.
DATES: This AD is effective January 22,
2018.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 22, 2018.
ADDRESSES: For service information
identified in this final rule, contact
Boeing Commercial Airplanes,
Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC
110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet
https://www.myboeingfleet.com. You
may view this referenced service
information at the FAA, Transport
Standards Branch, 1601 Lind Avenue
SW, Renton, WA. For information on
the availability of this material at the
FAA, call 425–227–1221. It is also
available on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
0807.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
0807; 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 final rule, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (phone: 800–647–5527) is
Docket Management Facility, 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:
Galib Abumeri, Aerospace Engineer,
Airframe Section, FAA, Los Angeles
ACO Branch, 3960 Paramount
Boulevard, Lakewood, CA 90712–4137;
phone: 562–627–5324; fax: 562–627–
5210; email: galib.abumeri@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all The Boeing Company Model
737–100, –200, –200C, –300, –400, and
–500 series airplanes. The NPRM
published in the Federal Register on
August 30, 2017 (82 FR 41179). The
NPRM was prompted by reports of
cracking in the webs of the stub beams
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
59967
at certain fuselage stations. These cracks
are a result of fatigue caused by cyclical
loading from pressurization, wing loads,
and landing loads. The NPRM proposed
to require repetitive inspections for
cracking of the webs of the stub beams
at certain fuselage stations, and
applicable on-condition actions.
Comments
We 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.
Support for the NPRM
Boeing concurred with the NPRM.
Effect of Winglets on Accomplishment
of the Proposed Actions
Aviation Partners Boeing stated that
accomplishing Supplemental Type
Certificate (STC) ST01219SE does not
affect the ability to accomplish the
actions specified in the NPRM.
We concur with the commenter’s
request. We have redesignated
paragraph (c) of the proposed AD as
paragraph (c)(1) and added paragraph
(c)(2) to this AD to state that installation
of STC ST01219SE does not affect the
ability to accomplish the actions
required by this AD. Therefore, for
airplanes on which STC ST01219SE is
installed, a ‘‘change in product’’
alternative methods of compliance
(AMOC) approval request is not
necessary to comply with the
requirements of 14 CFR 39.17.
Conclusion
We 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.
We have determined that these minor
changes:
• Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
We also determined that these
changes will not increase the economic
burden on any operator or increase the
scope of this final rule.
Additional Report of Cracking Since
NPRM Was Issued
Since we issued the NPRM, Boeing
received a report indicating that stub
beam cracking occurred at station (STA)
685 outside of the inspection areas
described in Boeing Alert Service
Bulletin 737–53A1364, dated May 24,
E:\FR\FM\18DER1.SGM
18DER1
]]>Agencies
[Federal Register Volume 82, Number 241 (Monday, December 18, 2017)]
[Rules and Regulations]
[Pages 59963-59967]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-26949]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-1170; Product Identifier 2013-NM-054-AD; Amendment
39-19129; AD 2017-25-15]
RIN 2120-AA64
Airworthiness Directives; ATR-GIE Avions de Transport
R[eacute]gional Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
ATR-GIE Avions de Transport R[eacute]gional Model ATR42-300 and -500
airplanes and Model ATR72-202 and -212A airplanes. This AD requires
identifying the serial number of the dual distributor valve (DDV), and
replacement of affected DDVs. This AD was prompted by an investigation
performed on a failed DDV that revealed a nonconformity of crimping on
an internal valve. We are issuing this AD to address the unsafe
condition on these products.
DATES: This AD becomes effective January 2, 2018.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of January 2,
2018.
We must receive comments on this AD by February 1, 2018.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in this final rule, contact ATR-
GIE Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email aircraft.com">[email protected]aircraft.com. You
may view this referenced service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information on
the availability of this material at the FAA, call 425-227-1221. It is
also available on the internet at https://www.regulations.gov by
searching for and locating Docket No. FAA-2017-1170.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1170; or in person at the Docket Operations office between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Operations office
(telephone
[[Page 59964]]
800-647-5527) is in the ADDRESSES section. Comments will be available
in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Section, Transport Standards Branch, FAA, 1601
Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1112; fax 425-
227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive, 2013-0032, dated February 18, 2013 (referred
to after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain ATR-GIE
Avions de Transport R[eacute]gional Model ATR42-300 and -500 airplanes
and Model ATR72-202 and -212A airplanes. The MCAI states:
During the investigation performed on a failed dual distributor
valve (DDV) shipped to the DDV manufacturer, a non-conformity of
crimping on an internal valve has been detected by the DDV
manufacturer. This defective crimping creates a lack of tightness
that prevents the complete deflation of the related de-icing boot
chamber during de-icing cycles.
A batch of serialized DDV, potentially affected with the same
manufacturing discrepancy, has been identified by the DDV
manufacturer.
This condition, if not detected and corrected, may affect the
efficiency of the pneumatic de-icing system, which could reduce
flight safety in icing conditions.
For the reasons described above, this AD requires a one-time
inspection of each DDV to identify the serial number (s/n) and
replacement of the non-conforming DDV units.
The affected DDV units installed on aeroplanes and those
delivered as spares have been retraced by ATR and all non-installed
spare units have been quarantined, which is why this AD only applies
to specific MSN [manufacturer serial number] aeroplanes.
You may examine the MCAI on the internet at https://www.regulations.gov
by searching for and locating Docket No. FAA-2017-1170.
Related Service Information Under 1 CFR Part 51
Avions de Transport R[eacute]gional has issued the following
service information:
ATR Service Bulletin ATR42-30-0080, Revision 02, dated
March 26, 2013.
ATR Service Bulletin ATR42-30-0081, Revision 02, dated
March 26, 2013.
ATR Service Bulletin ATR72-30-1049, Revision 03, dated
March 26, 2013.
ATR Service Bulletin ATR72-30-1050, Revision 03, dated
March 26, 2013.
This service information describes procedures for identifying and
replacing affected DDVs. These documents are distinct since they apply
to different airplane models. 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 of this AD.
FAA's Determination and Requirements of This AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of these
same type designs.
FAA's Determination of the Effective Date
There are currently no domestic operators of this product.
Therefore, we find good cause that notice and opportunity for prior
public comment are unnecessary. In addition, for the reason(s) stated
above, we find that good cause exists for making this amendment
effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2017-1170; Product
Identifier 2013-NM-054-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD based on
those comments.
We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
Costs of Compliance
Currently, there are no affected airplanes on the U.S. Register. If
an affected airplane is imported and placed on the U.S. Register in the
future, we provide the following cost estimates to comply with this AD.
We estimate that it will take about 84 work-hours per product to comply
with the basic requirements of this AD. The average labor rate is $85
per work-hour. Required parts will cost about $12,000 per product.
Based on these figures, we estimate the cost of this AD to be $19,140
per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
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 to
the Director of the System Oversight Division.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
[[Page 59965]]
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2017-25-15 ATR--GIE Avions de Transport R[eacute]gional: Amendment
39-19129; Docket No. FAA-2017-1170; Product Identifier 2013-NM-054-
AD.
(a) Effective Date
This AD becomes effective January 2, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to ATR--GIE Avions de Transport R[eacute]gional
airplanes, certificated in any category, identified in paragraphs
(c)(1) through (c)(6) of this AD.
Note 1 to the introductory text of paragraph (c) of this AD: In
EASA AD 2013-0032, dated February 18, 2013, airplanes specified in
paragraphs (c)(1) and (c)(2) of this AD are identified as Group 1
airplanes and airplanes specified in paragraphs (c)(3) through
(c)(6) of this AD are identified as Group 2 airplanes.
(1) Model ATR42-500 airplanes: Manufacturer serial numbers
(MSNs) 645, 653, 657, 659, 661, 663, and 665.
(2) Model ATR72-212A airplanes: MSNs 778, 994, 995, 996, 998,
999, 1000, and 1020.
(3) Model ATR42-300 airplanes: MSNs 348 and 415.
(4) Model ATR42-500 airplanes: MSNs 497, 501, and 514.
(5) Model ATR72-202 airplanes: MSNs 192, 411, 496, 508, and 509.
(6) Model ATR72-212A airplanes: MSNs 468, 568, 595, 662, 796,
920, 926, 950, 1024, 1025, 1028, 1029, 1031, 1032, 1033, 1034, 1035,
1036, 1037, 1039, and 1040.
(d) Subject
Air Transport Association (ATA) of America Code 30, Ice and Rain
Protection.
(e) Reason
This AD was prompted by an investigation performed on a failed
dual distributor valve (DDV) that revealed a nonconformity of
crimping on an internal valve. We are issuing this AD to prevent the
deflation of the related deicing boot chamber during deicing cycles,
which could result in reduced controllability of the airplane in
icing conditions.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Part Identification
Within 6 months after the effective date of this AD, identify
the serial number of the DDV as specified in paragraph (g)(1) or
(g)(2) of this AD, as applicable. A review of airplane delivery or
maintenance records is acceptable to make the identification as
required by this paragraph, provided those records can be relied
upon for that purpose, and the serial number of the DDV can be
conclusively identified from that review.
(1) For airplanes identified in paragraphs (c)(1) and (c)(2) of
this AD, identify the serial number of the engine DDV part number
(P/N) B03AA1060, in accordance with the Accomplishment Instructions
of ATR Service Bulletin ATR42-30-0081, Revision 02, dated March 26,
2013; or ATR72-30-1050, Revision 03, dated March 26, 2013; as
applicable to airplane model.
(2) For airplanes identified in paragraphs (c)(3), (c)(4),
(c)(5), and (c)(6) of this AD, identify the serial number of the
wing and/or stabilizer DDV, P/N B03AA1031 or B03AA1040, in
accordance with the Accomplishment Instructions of ATR Service
Bulletin ATR42-30-0080, Revision 02, dated March 26, 2013; or ATR72-
30-1049, Revision 03, dated March 26, 2013; as applicable to
airplane model.
(h) Definition of Serviceable DDV
For purposes of this AD, a serviceable DDV is any DDV having a
serial number listed in figure 1 to paragraphs (h) and (i) of this
AD with a suffix ``R'' added to the serial number.
[GRAPHIC] [TIFF OMITTED] TR18DE17.003
(i) Corrective Action
If, during the part identification required by paragraph (g) of
this AD, any DDV identified in figure 1 to paragraphs (h) and (i) of
this AD is found: At the applicable time specified in figure 2 to
the introductory text of paragraph (i) of this AD, depending on the
location and the number of DDV affected, and on whether the airplane
is operated in icing conditions or under Extended Operations (ETOPS)
rules, replace any affected DDV(s) with a new or serviceable DDV, in
accordance with the Accomplishment Instructions of the applicable
service information specified in paragraphs (i)(1) through (i)(4) of
this AD.
[[Page 59966]]
[GRAPHIC] [TIFF OMITTED] TR18DE17.004
(1) For airplanes identified in paragraphs (c)(3) and (c)(4) of
this AD: ATR Service Bulletin ATR42-30-0080, Revision 02, dated
March 26, 2013.
(2) For airplanes identified in paragraph (c)(1) of this AD: ATR
Service Bulletin ATR42-30-0081, Revision 02, dated March 26, 2013.
(3) For airplanes identified in paragraphs (c)(5) and (c)(6) of
this AD: ATR Service Bulletin ATR72-30-1049, Revision 03, dated
March 26, 2013.
(4) For airplanes identified in paragraph (c)(2) of this AD: ATR
Service Bulletin ATR72-30-1050, Revision 03, dated March 26, 2013.
(j) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using the service information identified in
paragraphs (j)(1) through (j)(10) of this AD, as applicable. This
service information is not incorporated by reference in this AD.
(1) ATR Service Bulletin ATR42-30-0080, dated October 18, 2012
(for Model ATR42-300 and -500 airplanes).
(2) ATR Service Bulletin ATR42-30-0080, Revision 01, dated
February 5, 2013 (for Model ATR42-300 and -500 airplanes).
(3) ATR Service Bulletin ATR42-30-0081, dated October 18, 2012
(for Model ATR42-500 airplanes).
(4) ATR Service Bulletin ATR42-30-0081, Revision 01, dated
February 5, 2013 (for Model ATR42-500 airplanes).
(5) ATR Service Bulletin ATR72-30-1049, dated October 4, 2012
(for Model ATR72-202 and -212A airplanes).
(6) ATR Service Bulletin ATR72-30-1049, Revision 01, dated
October 10, 2012 (for Model ATR72-202 and -212A airplanes).
(7) ATR Service Bulletin ATR72-30-1049, Revision 02, dated
February 5, 2013 (for Model ATR72-202 and -212A airplanes).
(8) ATR Service Bulletin ATR72-30-1050, dated October 4, 2012
(for Model ATR72-212A airplanes).
(9) ATR Service Bulletin ATR72-30-1050, Revision 01, dated
November 6, 2012 (for Model ATR72-212A airplanes).
(10) ATR Service Bulletin ATR72-30-1050, Revision 02, dated
February 5, 2013 (for Model ATR72-212A airplanes).
(k) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the certification office, send it to the
attention of the person identified in paragraph (l)(2) of this AD.
Information may be emailed to: [email protected].
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Aviation
Safety Agency (EASA); or ATR--GIE Avions de Transport
R[eacute]gional's EASA Design Organization Approval (DOA). If
approved by the DOA, the approval must include the DOA-authorized
signature.
(l) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2013-0032, dated February 18, 2013, for related
information. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2017-1170.
(2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356;
telephone 425-227-1112; fax 425-227-1149.
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(3) and (m)(4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this
[[Page 59967]]
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) ATR Service Bulletin ATR42-30-0080, Revision 02, dated March
26, 2013.
(ii) ATR Service Bulletin ATR42-30-0081, Revision 02, dated
March 26, 2013.
(iii) ATR Service Bulletin ATR72-30-1049, Revision 03, dated
March 26, 2013.
(iv) ATR Service Bulletin ATR72-30-1050, Revision 03, dated
March 26, 2013.
(3) For service information identified in this AD, contact ATR--
GIE Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21;
fax +33 (0) 5 62 21 67 18; email aircraft.com">[email protected]aircraft.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information
on the availability of this material at the FAA, call 425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on December 6, 2017.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2017-26949 Filed 12-15-17; 8:45 am]
BILLING CODE 4910-13-P
