Airworthiness Directives; Piper Aircraft, Inc. Airplanes, 36139-36140 [2016-13226]
Download as PDF
36139
Federal Register / Vol. 81, No. 108 / Monday, June 6, 2016 / Rules and Regulations
Ring, Bolt, Mixing Lever Gear Unit (flight
controls).
This final rule is effective June
6, 2016.
DATES:
Issued in Fort Worth, Texas, on May 23,
2016.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
You may examine the AD
docket on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2014–
0338; 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 address for the
Docket Office (phone: 800–647–5527) is
Document 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.
ADDRESSES:
[FR Doc. 2016–13103 Filed 6–3–16; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0338; Directorate
Identifier 2014–CE–010–AD; Amendment
39–18495; AD 2016–08–18]
RIN 2120–AA64
Gary
Wechsler, Aerospace Engineer, FAA,
Atlanta Aircraft Certification Office,
1701 Columbia Avenue, College Park,
Georgia 30337; telephone: (404) 474–
5575; fax: (404) 474–5606; email:
gary.wechsler@faa.gov.
FOR FURTHER INFORMATION CONTACT:
Airworthiness Directives; Piper
Aircraft, Inc. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that
published in the Federal Register. That
AD applies to certain Piper Aircraft, Inc.
Model PA–31–350 airplanes. The wing
locations of engine TIO–540–J2B and
LTIO–540–J2B in table 1 of the
Applicability, paragraph (c), section are
incorrect. This document corrects that
error. In all other respects, the original
document remains the same; however
we are publishing the entire rule in the
Federal Register.
SUMMARY:
SUPPLEMENTARY INFORMATION:
Airworthiness Directive 2016–08–18,
Amendment 39–18495 (81 FR 26106,
May 2, 2016), currently requires
inspecting the fuel hose assembly and
the turbocharger support assembly for
proper clearance between them,
inspecting each assembly for any sign of
damage, and making any necessary
repairs or replacements for certain Piper
Aircraft, Inc. Model PA–31–350
airplanes.
As published, the wing locations of
engine TIO–540–JJ2B and LTIO–540–
J2B in table 1 of the Applicability,
paragraph (c), section are incorrect. This
document corrects that error.
Although no other part of the
preamble or regulatory information has
been corrected, we are publishing the
entire rule in the Federal Register.
The effective date of this AD remains
June 6, 2016.
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2016–08–18 Piper Aircraft, Inc.:
Amendment 39–18495; Docket No.
FAA–2014–0338; Directorate Identifier
2014–CE–010–AD.
(a) Effective Date
This AD is effective June 6, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Piper Aircraft, Inc.
Model PA–31–350 airplanes, serial numbers
31–5001 through 31–5004, 31–7305005
through 31–8452024, and 31–8253001
through 31–8553002, certificated in any
category, that are equipped with the
following engines and fuel pump hose
assemblies:
TABLE 1 TO PARAGRAPH (c) OF THIS AD—APPLICABLE ENGINES AND FUEL PUMP HOSE ASSEMBLIES
Engine
Manufacturer’s hose name
Manufacturer’s part No.
(P/N)
LTIO–540–J2B (right wing) ............
Hose Assembly—Fuel ..................
Piper 39995–034 ..........................
TIO–540–J2B (left wing) ................
Hose, Fuel pump to Injector .........
Lycoming LW–12877–6S142 .......
LTIO–540–J2BD (right wing) .........
Hose, Fuel pump to Injector .........
Lycoming LW–12877–6S142 .......
TIO–540–J2BD (left wing) .............
Hose Assembly—Fuel ..................
Piper 39995–034 ..........................
mstockstill on DSK3G9T082PROD with RULES
(d) Subject
Joint Aircraft System Component (JASC)/
Air Transport Association (ATA) of America
Code 73: Engine Fuel and Control.
(e) Unsafe Condition
This AD was prompted by a report of an
engine fire caused by a leak in the fuel pump
inlet hose. We are issuing this AD to correct
the unsafe condition on these products.
(f) Compliance
Comply with this AD within the
compliance times specified in paragraphs
VerDate Sep<11>2014
16:21 Jun 03, 2016
Jkt 238001
(g)(1) through (j)(2) of this AD, unless already
done.
(g) Ensure Proper Clearance Between the
Fuel Hose Assembly and the Turbocharger
Support Assembly
(1) Within the next 60 hours time-inservice (TIS) after June 6, 2016 (the effective
date of this AD) or within the next 6 months
after June 6, 2016 (the effective date of this
AD), whichever occurs first, inspect to
determine the clearance between the inlet
and exit fuel hose assemblies listed in table
1 to paragraph (c) of this AD, and each
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
Hose description
Inlet fuel hose to
pump.
Exit fuel hose from
pump.
Exit fuel hose from
pump.
Inlet fuel hose to
pump.
engine fuel
engine fuel
engine fuel
engine fuel
turbocharger support assembly, Lycoming
P/N LW–18302. There should be a minimum
3/16-inch clearance. Do the inspection
following the INSTRUCTIONS section of
Piper Aircraft, Inc. Service Bulletin No.
1257A, dated August 4, 2015.
(2) Before further flight after the inspection
required in paragraph (g)(1) of this AD, if the
measured clearance is less than 3/16-inch,
make all necessary adjustments to make the
clearance a minimum of 3/16-inch between
the inlet and exit fuel hose assemblies listed
in table 1 to paragraph (c) of this AD and
each turbocharger support assembly,
E:\FR\FM\06JNR1.SGM
06JNR1
36140
Federal Register / Vol. 81, No. 108 / Monday, June 6, 2016 / Rules and Regulations
Lycoming P/N LW–18302, following the
INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
(h) Visually Inspect the Fuel Hose Assembly
and Replace If Necessary
(1) Within the next 60 hours TIS after June
6, 2016 (the effective date of this AD) or
within the next 6 months after June 6, 2016
(the effective date of this AD), whichever
occurs first, visually inspect the inlet and
exit fuel hose assemblies listed in table 1 to
paragraph (c) of this AD for evidence of
leaking, cracking, chafing, and any other sign
of damage. Do the inspection following the
INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
(2) Before further flight after the inspection
required in paragraph (h)(1) of this AD, if any
evidence of leaking, cracking, chafing, or any
other sign of damage is found in any inlet or
exit fuel host assembly listed in table 1 to
paragraph (c) of this AD, replace the fuel
hose assembly with a serviceable part. Do the
replacement following the INSTRUCTIONS
section of Piper Aircraft, Inc. Service Bulletin
No. 1257A, dated August 4, 2015.
mstockstill on DSK3G9T082PROD with RULES
(i) Visually Inspect the Turbocharger
Support Assembly and Replace If Necessary
(1) Within the next 60 hours TIS after June
6, 2016 (the effective date of this AD) or
within the next 6 months after June 6, 2016
(the effective date of this AD), whichever
occurs first, visually inspect each
turbocharger support assembly, Lycoming
P/N LW–18302, for evidence of chafing and
any other signs of damage. Do the inspection
following the INSTRUCTIONS section of
Piper Aircraft, Inc. Service Bulletin No.
1257A, dated August 4, 2015.
(2) Before further flight after the inspection
required in paragraph (i)(1) of this AD, if any
evidence of chafing or any other sign of
damage is found on any turbocharger support
assembly, replace Lycoming P/N LW–18302
with a serviceable part. Do the replacement
following the INSTRUCTIONS section of
Piper Aircraft, Inc. Service Bulletin No.
1257A, dated August 4, 2015.
(j) Engine Run-Up
(1) If any fuel line component was adjusted
or replaced during any actions required in
paragraphs (g)(1) through (i)(2) of this AD,
before further flight, perform an engine runup on the ground to check for leaks. Do the
engine run-up following the INSTRUCTIONS
section of Piper Aircraft, Inc. Service Bulletin
No. 1257A, dated August 4, 2015.
(2) If any leaks found during the engine
run-up required in paragraph (j)(1) of this AD
emanate from any fuel line component
adjusted, repaired, or replaced during any
actions required in paragraphs (g)(1) through
(i)(2) of this AD, before further flight, take all
necessary corrective actions following the
INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector
or local Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the ACO, send it to the
attention of the person identified in the
Related Information section of this AD.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
DEPARTMENT OF TRANSPORTATION
(l) Related Information
SUMMARY:
For more information about this AD,
contact Gary Wechsler, Aerospace Engineer,
FAA, Atlanta ACO, 1701 Columbia Avenue,
College Park, Georgia 30337; telephone: (404)
474–5575; fax: (404) 474–5606; email:
gary.wechsler@faa.gov.
(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 the AD specifies otherwise.
(i) Piper Aircraft, Inc. Service Bulletin No.
1257A, dated August 4, 2015.
(ii) Reserved.
(3) For Piper Aircraft, Inc. service
information identified in this AD, contact
Piper Aircraft, Inc., 926 Piper Drive, Vero
Beach, Florida 32960; telephone: (772) 567–
4361; fax: (772) 978–6573; Internet:
www.piper.com/home/pages/
Publications.cfm.
(4) You may view this service information
at FAA, Small Airplane Directorate, 901
Locust, Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148.
(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 Kansas City, Missouri, on May
31, 2016.
Pat Mullen,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2016–13226 Filed 6–3–16; 8:45 am]
BILLING CODE 4910–13–P
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Atlanta Aircraft
Certification Office (ACO), FAA, has the
VerDate Sep<11>2014
16:21 Jun 03, 2016
Jkt 238001
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2016–0449; Airspace
Docket No. 16–ASW–2]
Amendment of Class E Airspace;
Clovis, NM
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action modifies Class E
airspace extending upward from 700
feet above the surface at Portales
Municipal Airport, Clovis, NM.
Decommissioning of the Portales nondirectional radio beacon (NDB),
cancellation of NDB approaches at
Portales Municipal Airport, and
implementation of area navigation
(RNAV) procedures have made this
action necessary for the safety and
management of Instrument Flight Rules
(IFR) operations at the airport. This
action also updates the geographic
coordinates for Portales Municipal
Airport to coincide with the FAA’s
aeronautical database.
DATES: Effective 0901 UTC, September
15, 2016. The Director of the Federal
Register approves this incorporation by
reference action under Title 1, Code of
Federal Regulations, part 51, subject to
the annual revision of FAA Order
7400.9 and publication of conforming
amendments.
FAA Order 7400.9Z,
Airspace Designations and Reporting
Points, and subsequent amendments can
be viewed online at https://www.faa.gov/
air_traffic/publications/. For further
information, you can contact the
Airspace Policy Group, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone: 202–267–8783. The Order is
also available for inspection at the
National Archives and Records
Administration (NARA). For
information on the availability of FAA
Order 7400.9Z at NARA, call 202–741–
6030, or go to https://www.archives.gov/
federal_register/code_of_federalregulations/ibr_locations.html.
FAA Order 7400.9, Airspace
Designations and Reporting Points, is
published yearly and effective on
September 15.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Claypool, Federal Aviation
Administration, Operations Support
Group, Central Service Center, 10101
Hillwood Parkway, Fort Worth, TX
76177; telephone (817) 222–5711.
ADDRESSES:
E:\FR\FM\06JNR1.SGM
06JNR1
Agencies
[Federal Register Volume 81, Number 108 (Monday, June 6, 2016)]
[Rules and Regulations]
[Pages 36139-36140]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-13226]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0338; Directorate Identifier 2014-CE-010-AD;
Amendment 39-18495; AD 2016-08-18]
RIN 2120-AA64
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to certain Piper
Aircraft, Inc. Model PA-31-350 airplanes. The wing locations of engine
TIO-540-J2B and LTIO-540-J2B in table 1 of the Applicability, paragraph
(c), section are incorrect. This document corrects that error. In all
other respects, the original document remains the same; however we are
publishing the entire rule in the Federal Register.
DATES: This final rule is effective June 6, 2016.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0338; 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 address for the Docket Office (phone: 800-647-
5527) is Document 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: Gary Wechsler, Aerospace Engineer,
FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue,
College Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474-
5606; email: gary.wechsler@faa.gov.
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2016-08-18,
Amendment 39-18495 (81 FR 26106, May 2, 2016), currently requires
inspecting the fuel hose assembly and the turbocharger support assembly
for proper clearance between them, inspecting each assembly for any
sign of damage, and making any necessary repairs or replacements for
certain Piper Aircraft, Inc. Model PA-31-350 airplanes.
As published, the wing locations of engine TIO-540-JJ2B and LTIO-
540-J2B in table 1 of the Applicability, paragraph (c), section are
incorrect. This document corrects that error.
Although no other part of the preamble or regulatory information
has been corrected, we are publishing the entire rule in the Federal
Register.
The effective date of this AD remains June 6, 2016.
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):
2016-08-18 Piper Aircraft, Inc.: Amendment 39-18495; Docket No. FAA-
2014-0338; Directorate Identifier 2014-CE-010-AD.
(a) Effective Date
This AD is effective June 6, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Piper Aircraft, Inc. Model PA-31-350
airplanes, serial numbers 31-5001 through 31-5004, 31-7305005
through 31-8452024, and 31-8253001 through 31-8553002, certificated
in any category, that are equipped with the following engines and
fuel pump hose assemblies:
Table 1 to Paragraph (c) of This AD--Applicable Engines and Fuel Pump Hose Assemblies
----------------------------------------------------------------------------------------------------------------
Manufacturer's hose Manufacturer's part No.
Engine name (P/N) Hose description
----------------------------------------------------------------------------------------------------------------
LTIO-540-J2B (right wing)............ Hose Assembly--Fuel.... Piper 39995-034........ Inlet fuel hose to
engine fuel pump.
TIO-540-J2B (left wing).............. Hose, Fuel pump to Lycoming LW-12877-6S142 Exit fuel hose from
Injector. engine fuel pump.
LTIO-540-J2BD (right wing)........... Hose, Fuel pump to Lycoming LW-12877-6S142 Exit fuel hose from
Injector. engine fuel pump.
TIO-540-J2BD (left wing)............. Hose Assembly--Fuel.... Piper 39995-034........ Inlet fuel hose to
engine fuel pump.
----------------------------------------------------------------------------------------------------------------
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 73: Engine Fuel and Control.
(e) Unsafe Condition
This AD was prompted by a report of an engine fire caused by a
leak in the fuel pump inlet hose. We are issuing this AD to correct
the unsafe condition on these products.
(f) Compliance
Comply with this AD within the compliance times specified in
paragraphs (g)(1) through (j)(2) of this AD, unless already done.
(g) Ensure Proper Clearance Between the Fuel Hose Assembly and the
Turbocharger Support Assembly
(1) Within the next 60 hours time-in-service (TIS) after June 6,
2016 (the effective date of this AD) or within the next 6 months
after June 6, 2016 (the effective date of this AD), whichever occurs
first, inspect to determine the clearance between the inlet and exit
fuel hose assemblies listed in table 1 to paragraph (c) of this AD,
and each turbocharger support assembly, Lycoming P/N LW-18302. There
should be a minimum 3/16-inch clearance. Do the inspection following
the INSTRUCTIONS section of Piper Aircraft, Inc. Service Bulletin
No. 1257A, dated August 4, 2015.
(2) Before further flight after the inspection required in
paragraph (g)(1) of this AD, if the measured clearance is less than
3/16-inch, make all necessary adjustments to make the clearance a
minimum of 3/16-inch between the inlet and exit fuel hose assemblies
listed in table 1 to paragraph (c) of this AD and each turbocharger
support assembly,
[[Page 36140]]
Lycoming P/N LW-18302, following the INSTRUCTIONS section of Piper
Aircraft, Inc. Service Bulletin No. 1257A, dated August 4, 2015.
(h) Visually Inspect the Fuel Hose Assembly and Replace If Necessary
(1) Within the next 60 hours TIS after June 6, 2016 (the
effective date of this AD) or within the next 6 months after June 6,
2016 (the effective date of this AD), whichever occurs first,
visually inspect the inlet and exit fuel hose assemblies listed in
table 1 to paragraph (c) of this AD for evidence of leaking,
cracking, chafing, and any other sign of damage. Do the inspection
following the INSTRUCTIONS section of Piper Aircraft, Inc. Service
Bulletin No. 1257A, dated August 4, 2015.
(2) Before further flight after the inspection required in
paragraph (h)(1) of this AD, if any evidence of leaking, cracking,
chafing, or any other sign of damage is found in any inlet or exit
fuel host assembly listed in table 1 to paragraph (c) of this AD,
replace the fuel hose assembly with a serviceable part. Do the
replacement following the INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated August 4, 2015.
(i) Visually Inspect the Turbocharger Support Assembly and Replace If
Necessary
(1) Within the next 60 hours TIS after June 6, 2016 (the
effective date of this AD) or within the next 6 months after June 6,
2016 (the effective date of this AD), whichever occurs first,
visually inspect each turbocharger support assembly, Lycoming P/N
LW-18302, for evidence of chafing and any other signs of damage. Do
the inspection following the INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated August 4, 2015.
(2) Before further flight after the inspection required in
paragraph (i)(1) of this AD, if any evidence of chafing or any other
sign of damage is found on any turbocharger support assembly,
replace Lycoming P/N LW-18302 with a serviceable part. Do the
replacement following the INSTRUCTIONS section of Piper Aircraft,
Inc. Service Bulletin No. 1257A, dated August 4, 2015.
(j) Engine Run-Up
(1) If any fuel line component was adjusted or replaced during
any actions required in paragraphs (g)(1) through (i)(2) of this AD,
before further flight, perform an engine run-up on the ground to
check for leaks. Do the engine run-up following the INSTRUCTIONS
section of Piper Aircraft, Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
(2) If any leaks found during the engine run-up required in
paragraph (j)(1) of this AD emanate from any fuel line component
adjusted, repaired, or replaced during any actions required in
paragraphs (g)(1) through (i)(2) of this AD, before further flight,
take all necessary corrective actions following the INSTRUCTIONS
section of Piper Aircraft, Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Atlanta Aircraft Certification Office (ACO),
FAA, has the authority to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19. In accordance with 14
CFR 39.19, send your request to your principal inspector or local
Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in the Related Information
section of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(l) Related Information
For more information about this AD, contact Gary Wechsler,
Aerospace Engineer, FAA, Atlanta ACO, 1701 Columbia Avenue, College
Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474-5606;
email: gary.wechsler@faa.gov.
(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 the AD specifies otherwise.
(i) Piper Aircraft, Inc. Service Bulletin No. 1257A, dated
August 4, 2015.
(ii) Reserved.
(3) For Piper Aircraft, Inc. service information identified in
this AD, contact Piper Aircraft, Inc., 926 Piper Drive, Vero Beach,
Florida 32960; telephone: (772) 567-4361; fax: (772) 978-6573;
Internet: www.piper.com/home/pages/Publications.cfm.
(4) You may view this service information at FAA, Small Airplane
Directorate, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
(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 Kansas City, Missouri, on May 31, 2016.
Pat Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-13226 Filed 6-3-16; 8:45 am]
BILLING CODE 4910-13-P