AD 2018-17-07
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | ATR - GIE Avions de Transport Régional | ATR42-500 | Airworthiness Directives; ATR--GIE Avions de Transport R gional Airplanes |
| aircraft | ATR - GIE Avions de Transport Régional | ATR72-212A | Airworthiness Directives; ATR--GIE Avions de Transport R gional Airplanes |
Unsafe Condition
An event was reported of several spurious alarms on a recently delivered ATR 72 aeroplane. During subsequent trouble-shooting, damage was found on the electrical harness wire bundle (Route 1M), due to chafing with a window blinding panel located on the left-hand (LH) side of the fuselage, zone 231. A bracket, necessary to maintain the harness wire bundle close to the structure of the fuselage and avoid chafing, was missing. The same bracket was also found missing on the right-hand (RH) side of the fuselage, zone 232, Route 2M, although without damage on the harness wire bundle. A quality investigation revealed another aeroplane on the production line where same brackets were not installed. This condition, if not detected and corrected, may lead to wire failure (cut or shorted) and, in case of several failures in combination, to loss of systems, possibly resulting in reduced control of the aeroplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the installation of the brackets, perform a one-time inspection of the wire bundles, and depending on findings, accomplish applicable corrective action(s).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Model ATR42-500 airplanes and Model ATR72-212A airplanes, manufacturer serial numbers 1071, 1141, 1341, 1367, and 1377 are not affected by the identified unsafe condition.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are superseding Airworthiness Directive (AD) 2017-24-01, which applied to certain ATR--GIE Avions de Transport R[eacute]gional Model ATR42-500 airplanes and Model ATR72-212A airplanes. AD 2017-24-01 required an inspection for routing attachments of electrical harness bundles and for wire damage, and corrective actions if necessary. This new AD adds additional airplanes to the applicability. This AD was prompted by a determination that additional airplanes are affected by the unsafe condition. We are issuing this AD to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to the ATR--GIE Avions de Transport
R[eacute]gional airplanes identified in paragraphs (c)(1) and (c)(2)
of this AD, certificated in any category.
(1) Model ATR42-500 airplanes, manufacturer serial numbers
(MSNs) 1001 through 1014 inclusive, 1016 through 1019 inclusive, and
1201 through 1212 inclusive.
(2) Model ATR72-212A airplanes, MSNs 1048 through 1070
inclusive, 1072 through 1140 inclusive, 1142 through 1200 inclusive,
1220 through 1340 inclusive, 1342 through 1353 inclusive, 1355
through 1366 inclusive, 1368 through 1376 inclusive, 1378 through
1380 inclusive, 1382, 1385, and 1388.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 83, Number 160 (Friday, August 17, 2018)]
[Rules and Regulations]
[Pages 40963-40966]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2018-17661]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0712; Product Identifier 2018-NM-089-AD; Amendment
39-19361; AD 2018-17-07]
RIN 2120-AA64
Airworthiness Directives; ATR--GIE Avions de Transport
R[eacute]gional Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are superseding Airworthiness Directive (AD) 2017-24-01,
which applied to certain ATR--GIE Avions de Transport R[eacute]gional
Model ATR42-500 airplanes and Model ATR72-212A airplanes. AD 2017-24-01
required an inspection for routing attachments of electrical harness
bundles and for wire damage, and corrective actions if necessary. This
new AD adds additional airplanes to the applicability. This AD was
prompted by a determination that additional airplanes are affected by
the unsafe condition. We are issuing this AD to address the unsafe
condition on these products.
[[Page 40964]]
DATES: This AD is effective September 4, 2018.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of September 4,
2018 .
We must receive comments on this AD by October 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:
<bullet> Federal eRulemaking Portal: Go to <a href="http://www.regulations.gov">http://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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 <a href="/cdn-cgi/l/email-protection#0c6f6362786562796968226d657e7b637e78646562697f7f4c6d787e21306d2c647e696a31" http: aircraft.com">aircraft.com</a>">continued.airworthiness@atr-<a href="http://aircraft.com">aircraft.com</a></a>; http://www.atr-<a href="http://aircraft.com">aircraft.com</a>. You may view this referenced
service information at the FAA, Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available on the
internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating
Docket No. FAA-2018-0712.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0712; 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 AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is listed above. Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Section, Transport Standards Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone and fax 206-321-3220.
SUPPLEMENTARY INFORMATION:
Discussion
We issued AD 2017-24-01, Amendment 39-19105 (82 FR 55755, November
24, 2017) (``AD 2017-24-01''), which applied to certain Model ATR42-500
airplanes and Model ATR72-212A airplanes. AD 2017-24-01 was prompted by
reports of electrical harness bundle chafing with a window blinding
panel in the fuselage due to missing routing attachments. AD 2017-24-01
required an inspection for routing attachments (i.e., brackets) of
electrical harness bundles and for wire damage, and corrective actions
if necessary. We issued AD 2017-24-01 to detect and correct missing
routing attachments of fuselage electrical harness bundles, which could
result in wire failure (cut or shorted) and, in case of several
failures in combination, the loss of systems, possibly resulting in
reduced control of the airplane.
Since we issued AD 2017-24-01, we have determined that additional
airplanes are affected by the unsafe condition.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive 2018-0105, dated May 08, 2018 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for certain Model ATR42-
500 airplanes and Model ATR72-212A airplanes. The MCAI states:
An event was reported of several spurious alarms on a recently
delivered ATR 72 aeroplane. During subsequent trouble-shooting,
damage was found on the electrical harness wire bundle (Route 1M),
due to chafing with a window blinding panel located on the left-hand
(LH) side of the fuselage, zone 231. A bracket, necessary to
maintain the harness wire bundle close to the structure of the
fuselage and avoid chafing, was missing. The same bracket was also
found missing on the right-hand (RH) side of the fuselage, zone 232,
Route 2M, although without damage on the harness wire bundle. A
quality investigation revealed another aeroplane on the production
line where same brackets were not installed.
This condition, if not detected and corrected, may lead to wire
failure (cut or shorted) and, in case of several failures in
combination, to loss of systems, possibly resulting in reduced
control of the aeroplane.
To address this potential unsafe condition, ATR published the
applicable SB [service bulletin] to provide inspection instructions.
Consequently, EASA issued AD 2017-0118 [which corresponds to FAA AD
2017-24-01] to require verification of the installation of the
brackets, a one-time inspection of the wire bundles, and depending
on findings, accomplishment of applicable corrective action(s).
Since that [EASA] AD was issued, an occurrence was reported of
engine intermittent auto-feather, caused by damage on the electrical
harness bundle Route 1M. The affected aeroplane MSN [manufacturer
serial number] was not identified in the Applicability of EASA AD
2017-0118.
For the reason described above, this [EASA] AD retains the
requirements of EASA AD 2017-0118, which is superseded, and expands
the Applicability to include additional aeroplanes, identified by
MSN in Group 2 as specified in section `Definitions' of this [EASA]
AD.
The MCAI includes MSNs 1071, 1141, 1341, 1367, and 1377 in its
applicability, but those MSNs are not identified in the definitions for
the affected groups. Those MSNs are not affected by the identified
unsafe condition. Therefore, we have not included those MSNs in our
applicability. You may examine the MCAI on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0712.
Related Service Information Under 1 CFR Part 51
ATR has issued Service Bulletin ATR42-92-0033, Revision 02, dated
April 12, 2018; and Service Bulletin ATR72-92-1044, Revision 02, dated
April 12, 2018. This service information describes procedures for an
inspection of routing attachments (i.e., brackets) of electrical
harness bundles and for wire damage, and corrective actions if
necessary. 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.
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 the same
type design.
[[Page 40965]]
FAA's Justification and Determination of the Effective Date
There are currently no domestic operators of this product.
Therefore, we good cause find that notice and opportunity for prior
public comment are unnecessary and that, for the same reason, 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-2018-0712; Product
Identifier 2018-NM-089-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 because of
those comments.
We will post all comments we receive, without change, to <a href="http://www.regulations.gov">http://www.regulations.gov</a>, 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 U.S.-registered airplanes. 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:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Inspection................................. 3 work-hours x $85 per hour = $255. $0 $255
----------------------------------------------------------------------------------------------------------------
We have received no definitive data that would enable us to provide
cost estimates for the on-condition actions specified in this AD.
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:
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 removing airworthiness directive (AD)
2017-24-01, Amendment 39-19105 (82 FR 55755, November 24, 2017), and
adding the following new AD:
2018-17-07 ATR--GIE Avions de Transport R[eacute]gional: Amendment
39-19361; Docket No. FAA-2018-0712; Product Identifier 2018-NM-089-
AD.
(a) Effective Date
This AD is effective September 4, 2018.
(b) Affected ADs
This AD replaces AD 2017-24-01, Amendment 39-19105 (82 FR 55755,
November 24, 2017) (``AD 2017-24-01'').
(c) Applicability
This AD applies to the ATR--GIE Avions de Transport
R[eacute]gional airplanes identified in paragraphs (c)(1) and (c)(2)
of this AD, certificated in any category.
(1) Model ATR42-500 airplanes, manufacturer serial numbers
(MSNs) 1001 through 1014 inclusive, 1016 through 1019 inclusive, and
1201 through 1212 inclusive.
(2) Model ATR72-212A airplanes, MSNs 1048 through 1070
inclusive, 1072 through 1140 inclusive, 1142 through 1200 inclusive,
1220 through 1340 inclusive, 1342 through 1353 inclusive, 1355
through 1366 inclusive, 1368 through 1376 inclusive, 1378 through
1380 inclusive, 1382, 1385, and 1388.
(d) Subject
Air Transport Association (ATA) of America Code 92, Electric.
(e) Reason
This AD was prompted by reports of electrical harness bundle
chafing with a window blinding panel in the fuselage due to missing
routing attachments and by a determination that additional airplanes
that were not identified in AD 2017-24-01 are affected by the unsafe
condition. We are issuing this AD to detect and correct missing
[[Page 40966]]
routing attachments of fuselage electrical harness bundles, which
could result in wire failure (cut or shorted), and, in case of
several failures in combination, the loss of systems, possibly
resulting in reduced control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definitions
(1) For the purposes of this AD, Group 1 airplanes are
identified as the following: MSNs 1014, 1016 through 1019 inclusive,
1165 through 1212 inclusive, 1220 through 1340 inclusive, 1342
through 1353 inclusive, 1355 through 1366 inclusive, 1368 through
1376 inclusive, 1378 through 1380 inclusive, 1382, 1385 and 1388.
(2) For the purposes of this AD, Group 2 airplanes are
identified as the following: MSNs 1001 through 1013 inclusive, 1048
through 1070 inclusive, 1072 to 1140 inclusive 1142 through 1164
inclusive.
(h) Retained Inspection With New Service Information and Revised
Compliance Language
This paragraph restates the requirements of paragraph (g) of AD
2017-24-01, with new service information and revised compliance
language. For Group 1 airplanes: Within 6 months or 500 flight hours
after December 11, 2017 (the effective date of AD 2017-24-01),
whichever occurs first, do a detailed inspection for missing
brackets and damage (including but not limited to chafing and
electrical shorting) to wire bundles of the Route 1M and Route 2M
electrical harness, in accordance with the flowchart in paragraph
1.C., ``Description,'' and the Accomplishment Instructions of ATR
Service Bulletin ATR42-92-0033, Revision 02, dated April 12, 2018
(for Model ATR42-500 airplanes); or ATR Service Bulletin ATR72-92-
1044, Revision 02, dated April 12, 2018 (for Model ATR72-212A
airplanes); as applicable. Although ATR Service Bulletin ATR42-92-
0033, Revision 02, dated April 12, 2018; and ATR Service Bulletin
ATR72-92-1044, Revision 02, dated April 12, 2018; specify reporting,
this AD does not include that requirement.
(i) New Requirement of This AD: Inspection
For Group 2 airplanes: Within 6 months or 500 flight hours after
the effective date of this AD, whichever occurs first, do a detailed
inspection for missing brackets and damage (including but not
limited to chafing and electrical shorting) to wire bundles of the
Route 1M and Route 2M electrical harness, in accordance with the
flowchart in paragraph 1.C., ``Description,'' and the Accomplishment
Instructions of ATR Service Bulletin ATR42-92-0033, Revision 02,
dated April 12, 2018 (for Model ATR42-500 airplanes); or ATR Service
Bulletin ATR72-92-1044, Revision 02, dated April 12, 2018 (for Model
ATR72-212A airplanes); as applicable. Although ATR Service Bulletin
ATR42-92-0033, Revision 02, dated April 12, 2018; and ATR Service
Bulletin ATR72-92-1044, Revision 02, dated April 12, 2018; specify
reporting, this AD does not include that requirement.
(j) New Requirements of This AD: Corrective Action
If the inspection required by paragraph (h) or (i) of this AD
reveals that any bracket is missing or any wire is damaged, before
further flight, do applicable corrective actions, in accordance with
the flowchart in paragraph 1.C., ``Description,'' and the
Accomplishment Instructions of ATR Service Bulletin ATR42-92-0033,
Revision 02, dated April 12, 2018 (for Model ATR42-500 airplanes);
or ATR Service Bulletin ATR72-92-1044, Revision 02, dated April 12,
2018 (for Model ATR72-212A airplanes); as applicable. Where ATR
Service Bulletin ATR42-92-0033, Revision 02, dated April 12, 2018;
and ATR Service Bulletin ATR72-92-1044, Revision 02, dated April 12,
2018; specify to contact ATR-GIE Avions de Transport R[eacute]gional
for appropriate action, before further flight, accomplish corrective
actions in accordance with the procedures specified in paragraph
(l)(2) of this AD.
(k) Credit for Previous Actions
This paragraph provides credit for actions required by
paragraphs (h), (i), and (j) of this AD, if those actions were
performed before the effective date of this AD using ATR Service
Bulletin ATR42-92-0033, dated May 3, 2017, or Revision 01, dated
July 20, 2017; or ATR Service Bulletin ATR72-92-1044, dated May 3,
2017, or Revision 01, dated July 20, 2017, as applicable. ATR
Service Bulletin ATR42-92-0033, dated May 3, 2017; and ATR72-92-
1044, dated May 3, 2017, were previously incorporated by reference
in AD 2017-24-01. ATR Service Bulletin ATR42-92-0033 Revision 01,
dated July 20, 2017; and ATR72-92-1044, Revision 01, dated July 20,
2017, were not previously incorporated by reference.
(l) 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 (m)(2) of this AD. Information
may be emailed to: <a href="/cdn-cgi/l/email-protection#98a1b5d9d6d5b5a9a9aeb5d9d5d7dbb5caddc9cdddcbcccbd8fef9f9b6fff7ee"><span class="__cf_email__" data-cfemail="360f1b77787b1b0707001b777b79751b64736763736562657650575718515940">[email protected]</span></a>. 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: As of the effective date of
this AD, for any requirement in this AD to obtain corrective actions
from a manufacturer, the action must be accomplished using a method
approved by the Manager, 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.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2018-0105, dated May 08, 2018,
for related information. This MCAI may be found in the AD docket on
the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and
locating Docket No. FAA-2018-0712.
(2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 206-321-3220.
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(3) and (n)(4) of this AD.
(n) 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) ATR Service Bulletin ATR42- 92-0033, Revision 02, dated
April 12, 2018.
(ii) ATR Service Bulletin ATR72-92-1044, Revision 02, dated
April 12, 2018.
(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 <a href="/cdn-cgi/l/email-protection#8deee2e3f9e4e3f8e8e9a3ece4fffae2fff9e5e4e3e8fefecdecf9ffa0b1ecade5ffe8ebb0" http: aircraft.com">aircraft.com</a>">continued.airworthiness@atr-<a href="http://aircraft.com">aircraft.com</a></a>; internet http://www.atr-<a href="http://aircraft.com">aircraft.com</a>.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Des Moines, Washington, on August 8, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-17661 Filed 8-16-18; 8:45 am]
BILLING CODE 4910-13-P
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