Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Helicopters, 33439-33441 [2017-15031]
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33439
Rules and Regulations
Federal Register
Vol. 82, No. 138
Thursday, July 20, 2017
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–0701; Directorate
Identifier 2016–SW–063–AD; Amendment
39–18962; AD 2017–15–02]
RIN 2120–AA64
Airworthiness Directives; Bell
Helicopter Textron, Inc. (Bell)
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
We are adopting a new
airworthiness directive (AD) for Bell
Model 212 and Model 412 helicopters.
This AD requires replacing certain oil
and fuel check valves and prohibits
installing them on any helicopter. This
AD is prompted by a report of cracked
or leaking check valves. These actions
are intended to address an unsafe
condition on these helicopters.
DATES: This AD becomes effective
August 4, 2017.
We must receive comments on this
AD by September 18, 2017.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Docket: Go to
https://www.regulations.gov. Follow the
online instructions for sending your
comments electronically.
• Fax: 202–493–2251.
• Mail: Send comments to the U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC 20590–0001.
• Hand Delivery: Deliver to the
‘‘Mail’’ address between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
asabaliauskas on DSKBBXCHB2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
16:15 Jul 19, 2017
Jkt 241001
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–
0701; 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 economic
evaluation, any comments received, and
other information. The street address for
the Docket Operations Office (telephone
800–647–5527) is in the ADDRESSES
section. Comments will be available in
the AD docket shortly after receipt.
For service information identified in
this final rule, contact Bell Helicopter
Textron, Inc., P.O. Box 482, Fort Worth,
TX 76101; telephone (817) 280–3391;
fax (817) 280–6466; or at https://
www.bellcustomer.com/files/. You may
review the referenced service
information at the FAA, Office of the
Regional Counsel, Southwest Region,
10101 Hillwood Pkwy., Room 6N–321,
Fort Worth, TX 76177.
FOR FURTHER INFORMATION CONTACT:
Jurgen E. Priester, Aviation Safety
Engineer, Delegation Systems
Certification Office, ASW–130, FAA,
10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone (817) 222–5159; email
jurgen.e.priester@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not provide you with notice and
an opportunity to provide your
comments prior to it becoming effective.
However, we invite you to participate in
this rulemaking by submitting written
comments, data, or views. We also
invite comments relating to the
economic, environmental, energy, or
federalism impacts that resulted from
adopting this AD. The most helpful
comments reference a specific portion of
the AD, explain the reason for any
recommended change, and include
supporting data. To ensure the docket
does not contain duplicate comments,
commenters should send only one copy
of written comments, or if comments are
filed electronically, commenters should
submit them only one time. We will file
in the docket all comments that we
receive, as well as a report summarizing
each substantive public contact with
FAA personnel concerning this
PO 00000
Frm 00001
Fmt 4700
Sfmt 4700
rulemaking during the comment period.
We will consider all the comments we
receive and may conduct additional
rulemaking based on those comments.
Discussion
We are adopting a new AD for Bell
Model 212 and Model 412 helicopters.
This AD is prompted by a report that
certain part numbered 209–062–520–
001 check valves manufactured by
Circor Aerospace as replacement parts
have been found cracked or leaking on
several Bell Model 427 and Model 429
helicopters. These check valves may be
installed as engine oil check valves on
Bell Model 212 helicopters. Similar
check valves, part number 209–062–
607–001, may be installed as fuel check
valves on Bell Model 212 or 412
helicopters. These check valves may
have a condition induced during
assembly that can cause the valve body
to crack, resulting in oil or fuel leakage.
These suspect check valves are marked
‘‘Circle Seal’’ and were manufactured
between October 2011 and March 2015.
If not corrected, this condition could
result in a crack, fuel or oil leakage, and
subsequent failure of the engine or a fire
and loss of control of the helicopter.
FAA’s Determination
We are issuing this AD because we
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop in other helicopters of these
same type designs.
Related Service Information
We reviewed Bell Alert Service
Bulletin (ASB) 212–15–153, dated
September 4, 2015 (212–15–153), and
Bell ASB 212–15–155, dated September
15, 2015 (212–15–155), for Model 212
helicopters and Bell ASB 412–15–168,
dated September 15, 2015 (412–15–168),
for Model 412 helicopters. ASB 212–15–
153 describes procedures for inspecting
and replacing engine oil check valve
part number (P/N) 209–062–520–001
installed on certain serial-numbered
Model 212 helicopters. ASB 212–15–
155 and ASB 412–15–168 describe
procedures for inspecting and replacing
fuel check valve P/N 209–062–607–001
installed on certain serial-numbered
Model 212 and Model 412 helicopters.
E:\FR\FM\20JYR1.SGM
20JYR1
33440
Federal Register / Vol. 82, No. 138 / Thursday, July 20, 2017 / Rules and Regulations
AD Requirements
This AD requires, within 25 hours
time-in-service (TIS), replacing the
engine oil and fuel check valves.
This AD also prohibits installing a
check valve P/N 209–062–520–001 or
P/N 209–062–607–001 that was
manufactured by Circor Aerospace,
marked ‘‘Circle Seal,’’ and marked with
a manufacturing date code of ‘‘10/11’’
(October 2011) through ‘‘03/15’’ (March
2015) on any helicopter.
Differences Between This AD and the
Service Information
The manufacturer’s service
information describes procedures for an
inspection of the check valves within 25
hours TIS for a crack and allows 300
hours TIS to determine if the valve is
affected and to replace any affected
check valve. This AD requires replacing
all affected check valves within 25
hours TIS.
asabaliauskas on DSKBBXCHB2PROD with RULES
Costs of Compliance
We estimate that this AD affects 161
(59 Model 212 and 102 Model 412)
helicopters of U.S. Registry.
We estimate that operators may incur
the following costs in order to comply
with this AD. At an average labor rate
of $85, replacing each check valve
(engine oil or fuel) will require about 1
work-hour, and required parts will cost
$85. For the Model 212, we estimate a
total cost of $340 per helicopter and
$20,060 for the U.S. fleet. For the Model
412, we estimate a total cost of $170 per
helicopter and $17,340 for the U.S. fleet.
According to Bell’s service
information some of the costs of this AD
may be covered under warranty, thereby
reducing the cost impact on affected
individuals. We do not control warranty
coverage by Bell. Accordingly, we have
included all costs in our cost estimate.
FAA’s Justification and Determination
of the Effective Date
Providing an opportunity for public
comments prior to adopting these AD
requirements would delay
implementing the safety actions needed
to correct this known unsafe condition.
Therefore, we find that the risk to the
flying public justifies waiving notice
and comment prior to the adoption of
this rule because the actions required by
this AD must be accomplished within
25 hours TIS, a very short interval for
helicopters used in firefighting and
logging operations.
Since an unsafe condition exists that
requires the immediate adoption of this
AD, we determined that notice and
opportunity for public comment before
issuing this AD are impracticable and
that good cause exists for making this
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16:15 Jul 19, 2017
Jkt 241001
amendment effective in less than 30
days.
PART 39—AIRWORTHINESS
DIRECTIVES
Authority for This Rulemaking
■
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. ‘‘Subtitle VII:
Aviation Programs,’’ describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in ‘‘Subtitle VII,
Part A, Subpart III, Section 44701:
General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We determined that this 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, I certify
that this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in
Alaska to the extent that it justifies
making a regulatory distinction; and
4. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared an economic evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
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:
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
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):
■
2017–15–02 Bell Helicopter Textron, Inc.
(Bell): Amendment 39–18962; Docket
No. FAA–2017–0701; Directorate
Identifier 2016–SW–063–AD.
(a) Applicability
This AD applies to Bell Model 212 and 412
helicopters, certificated in any category, with
an engine oil check valve part number (P/N)
209–062–520–001 or fuel check valve P/N
209–062–607–001 manufactured by Circor
Aerospace, marked ‘‘Circle Seal’’ and with a
manufacturing date code of ‘‘10/11’’ (October
2011) through ‘‘03/15’’ (March 2015),
installed.
(b) Unsafe Condition
This AD defines the unsafe condition as a
cracked or leaking check valve, which could
result in loss of lubrication or fuel to the
engine, failure of the engine or a fire, and
subsequent loss of control of the helicopter.
(c) Effective Date
This AD becomes effective August 4, 2017.
(d) Compliance
You are responsible for performing each
action required by this AD within the
specified compliance time unless it has
already been accomplished prior to that time.
(e) Required Actions
(1) Within 25 hours time-in-service:
(i) Replace each fuel check valve.
(ii) For Model 212 helicopters, replace each
engine oil check valve.
(2) After the effective date of this AD, do
not install any check valve P/N 209–062–
520–001 or P/N 209–062–607–001
manufactured by Circor Aerospace, marked
‘‘Circle Seal’’ and with a manufacturing date
code of ‘‘10/11’’ (October 2011) through
‘‘03/15’’ (March 2015), on any helicopter.
(f) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Delegation Systems
Certification Office, FAA, may approve
AMOCs for this AD. Send your proposal to:
Jurgen E. Priester, Aviation Safety Engineer,
Delegation Systems Certification Office,
ASW–130, FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone (817) 222–5159;
email jurgen.e.priester@faa.gov.
(2) For operations conducted under a 14
CFR part 119 operating certificate or under
14 CFR part 91, subpart K, we suggest that
you notify your principal inspector, or
lacking a principal inspector, the manager of
the local flight standards district office or
certificate holding district office before
operating any aircraft complying with this
AD through an AMOC.
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Federal Register / Vol. 82, No. 138 / Thursday, July 20, 2017 / Rules and Regulations
(g) Additional Information
Bell Alert Service Bulletin (ASB) 212–15–
153, dated September 4, 2015; Bell ASB 212–
15–155, dated September 15, 2015; and Bell
ASB 412–15–168, dated September 15, 2015,
which are not incorporated by reference,
contain additional information about the
subject of this AD. For service information
identified in this AD, contact Bell Helicopter
Textron, Inc., P.O. Box 482, Fort Worth, TX
76101; telephone (817) 280–3391; fax (817)
280–6466; or at https://
www.bellcustomer.com/files/. You may
review this service information at the FAA,
Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy., Room 6N–
321, Fort Worth, TX 76177.
(h) Subject
Joint Aircraft Service Component (JASC)
Codes: 7900 Engine Oil System and 2800
Aircraft Fuel System.
Issued in Fort Worth, Texas, on July 7,
2017.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 2017–15031 Filed 7–19–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF THE TREASURY
Internal Revenue Service
26 CFR Parts 1 and 31
[TD 9821]
RIN 1545–BN13
Return Due Date and Extended Due
Date Changes
Internal Revenue Service (IRS),
Treasury.
ACTION: Final and temporary
regulations.
AGENCY:
This document contains final
and temporary regulations that update
the due dates and extensions of time to
file certain tax returns and information
returns. The dates are updated to reflect
the new statutory requirements set by
section 2006 of the Surface
Transportation and Veterans Health
Care Choice Improvement Act of 2015
and section 201 of the Protecting
Americans from Tax Hikes Act of 2015.
These regulations affect taxpayers who
file Form W–2 (series, except Form W–
2G), Form W–3, Form 990 (series), Form
1099–MISC, Form 1041, Form 1041–A,
Form 1065, Form 1120 (series), Form
4720, Form 5227, Form 6069, Form
8804, or Form 8870.
DATES: Effective Date: These regulations
are effective July 20, 2017.
Applicability Date: For dates of
applicability, see §§ 1.1446–3T(g)–(h),
asabaliauskas on DSKBBXCHB2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
16:15 Jul 19, 2017
Jkt 241001
1.6012–6T(c)–(d), 1.6031(a)-1T(f)–(g),
1.6032–1T(b)–(c), 1.6033–2T(k)–(l),
1.6041–2T(d)–(e), 1.6041–6T(c)–(d),
1.6072–2T(g)–(h), 1.6081–1T(c)–(d),
1.6081–2T(h)–(i), 1.6081–3T(g)–(h),
1.6081–5T(f)–(g), 1.6081–6T(g)–(h),
1.6081–9T(f)–(g), and 31.6071(a)–1T(g)–
(h). For additional information, see the
dates of applicability section of this
preamble.
FOR FURTHER INFORMATION CONTACT:
Concerning these temporary regulations,
Jonathan R. Black, (202) 317–6845;
concerning submissions of comments
and/or requests for a hearing, Regina
Johnson (202) 317–6901 (not toll-free
numbers).
SUPPLEMENTARY INFORMATION:
Background
These updates to the regulations
reflect changes in tax return due dates
enacted by section 2006 of the Surface
Transportation and Veterans Health
Care Choice Improvement Act of 2015
(the Surface Transportation Act), Public
Law 114–41, 129 Stat. 443 (2015), as
well as changes to information return
due dates enacted by section 201 of the
Protecting Americans from Tax Hikes
Act of 2015 (PATH Act), Public Law
114–113, Div. Q, 129 Stat. 2242 (2015).
Prior to amendment by the Surface
Transportation Act, section 6072(a)
provided that the income tax returns of
partnerships (generally Form 1065,
‘‘U.S. Return of Partnership Income’’),
trusts and estates (generally Form 1041,
‘‘U.S. Income Tax Return for Estates and
Trusts’’), and individuals (generally
Form 1040, ‘‘U.S. Individual Income
Tax Return’’) were due on the fifteenth
day of the fourth month following the
close of the taxable year (April 15 for
calendar-year taxpayers). Section
6072(b) generally provided that the
income tax returns of corporations (most
forms in the Form 1120 series) were due
on the fifteenth day of the third month
following the close of the taxable year
(March 15 for calendar-year taxpayers).
Under section 6081(a), the Secretary
generally has authority to grant a
reasonable extension of time of up to six
months for filing any return, statement,
or other document (longer in the case of
taxpayers who are abroad).
Additionally, prior to amendment by
the Surface Transportation Act, section
6081(b) provided for a three-month
automatic extension of time to file for
all corporations.
Immediately prior to the enactment of
the Surface Transportation Act,
§ 1.6081–2 provided an automatic fivemonth extension of time to file Form
1065 and Form 8804, ‘‘Annual Return
for Partnership Withholding Tax
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
33441
(Section 1446),’’ § 1.6081–3 provided a
six-month automatic extension of time
to file the income tax return of all
corporations (three months longer than
the minimum three-month automatic
extension), and § 1.6081–6 provided an
automatic five-month extension of time
to file Form 1041, such that the
extended due date of these returns was
the fifteenth day of the ninth month
after the close of the taxable year
(September 15 for calendar-year
taxpayers). Section 1.6081–4 provided
an automatic six-month extension of
time to file individual income tax
returns, such that the extended due date
of an individual’s return was the
fifteenth day of the tenth month after
the close of the taxable year (October 15
for calendar-year taxpayers).
The amendments to section 6072(b) of
the Internal Revenue Code made by
section 2006(a) of the Surface
Transportation Act change the due date
for filing an income tax return by a C
corporation from the fifteenth day of the
third month following the close of the
taxable year (March 15 for calendar-year
taxpayers) to the fifteenth day of the
fourth month following the close of the
taxable year (April 15 for calendar-year
taxpayers). The amendments also
change the due date for filing an income
tax return by a partnership from the
fifteenth day of the fourth month
following the close of the taxable year
(April 15 for calendar-year taxpayers) to
the fifteenth day of the third month
following the close of the taxable year
(March 15 for calendar-year taxpayers).
Generally these amendments apply to
returns for taxable years beginning after
December 31, 2015. However, for any C
corporation with a taxable year ending
on June 30, these amendments apply to
returns for taxable years beginning after
December 31, 2025.
Section 2006(b) of the Surface
Transportation Act provides that for
taxable years beginning after December
31, 2015, the Secretary of the Treasury,
or the Secretary’s designee, shall modify
appropriate regulations regarding the
due dates of certain returns and the
maximum extensions of time to file
certain returns, as specified in that
section.
Section 2006(c) of the Surface
Transportation Act generally changes
the automatic extension of time to file
the tax return of a C corporation
provided by section 6081(b) from three
months to six months. However, there
are exceptions for C corporations with
taxable years that begin before January
1, 2026. These statutory exceptions are
(1) if a C corporation files for a calendar
year, the automatic extension is five
months; and (2) if the C corporation files
E:\FR\FM\20JYR1.SGM
20JYR1
Agencies
[Federal Register Volume 82, Number 138 (Thursday, July 20, 2017)]
[Rules and Regulations]
[Pages 33439-33441]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-15031]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 82, No. 138 / Thursday, July 20, 2017 / Rules
and Regulations
[[Page 33439]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-0701; Directorate Identifier 2016-SW-063-AD;
Amendment 39-18962; AD 2017-15-02]
RIN 2120-AA64
Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell)
Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for Bell
Model 212 and Model 412 helicopters. This AD requires replacing certain
oil and fuel check valves and prohibits installing them on any
helicopter. This AD is prompted by a report of cracked or leaking check
valves. These actions are intended to address an unsafe condition on
these helicopters.
DATES: This AD becomes effective August 4, 2017.
We must receive comments on this AD by September 18, 2017.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Docket: Go to https://www.regulations.gov. Follow the online instructions for sending your
comments electronically.
Fax: 202-493-2251.
Mail: Send comments to the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590-0001.
Hand Delivery: Deliver to the ``Mail'' address between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
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-
0701; 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 economic evaluation, any comments received, and
other information. The street address for the Docket Operations Office
(telephone 800-647-5527) is in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.
For service information identified in this final rule, contact Bell
Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101; telephone
(817) 280-3391; fax (817) 280-6466; or at https://www.bellcustomer.com/files/. You may review the referenced service information at the FAA,
Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy.,
Room 6N-321, Fort Worth, TX 76177.
FOR FURTHER INFORMATION CONTACT: Jurgen E. Priester, Aviation Safety
Engineer, Delegation Systems Certification Office, ASW-130, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5159; email
jurgen.e.priester@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments prior to it becoming effective. However, we
invite you to participate in this rulemaking by submitting written
comments, data, or views. We also invite comments relating to the
economic, environmental, energy, or federalism impacts that resulted
from adopting this AD. The most helpful comments reference a specific
portion of the AD, explain the reason for any recommended change, and
include supporting data. To ensure the docket does not contain
duplicate comments, commenters should send only one copy of written
comments, or if comments are filed electronically, commenters should
submit them only one time. We will file in the docket all comments that
we receive, as well as a report summarizing each substantive public
contact with FAA personnel concerning this rulemaking during the
comment period. We will consider all the comments we receive and may
conduct additional rulemaking based on those comments.
Discussion
We are adopting a new AD for Bell Model 212 and Model 412
helicopters. This AD is prompted by a report that certain part numbered
209-062-520-001 check valves manufactured by Circor Aerospace as
replacement parts have been found cracked or leaking on several Bell
Model 427 and Model 429 helicopters. These check valves may be
installed as engine oil check valves on Bell Model 212 helicopters.
Similar check valves, part number 209-062-607-001, may be installed as
fuel check valves on Bell Model 212 or 412 helicopters. These check
valves may have a condition induced during assembly that can cause the
valve body to crack, resulting in oil or fuel leakage. These suspect
check valves are marked ``Circle Seal'' and were manufactured between
October 2011 and March 2015. If not corrected, this condition could
result in a crack, fuel or oil leakage, and subsequent failure of the
engine or a fire and loss of control of the helicopter.
FAA's Determination
We are issuing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other helicopters of these same type
designs.
Related Service Information
We reviewed Bell Alert Service Bulletin (ASB) 212-15-153, dated
September 4, 2015 (212-15-153), and Bell ASB 212-15-155, dated
September 15, 2015 (212-15-155), for Model 212 helicopters and Bell ASB
412-15-168, dated September 15, 2015 (412-15-168), for Model 412
helicopters. ASB 212-15-153 describes procedures for inspecting and
replacing engine oil check valve part number (P/N) 209-062-520-001
installed on certain serial-numbered Model 212 helicopters. ASB 212-15-
155 and ASB 412-15-168 describe procedures for inspecting and replacing
fuel check valve P/N 209-062-607-001 installed on certain serial-
numbered Model 212 and Model 412 helicopters.
[[Page 33440]]
AD Requirements
This AD requires, within 25 hours time-in-service (TIS), replacing
the engine oil and fuel check valves.
This AD also prohibits installing a check valve P/N 209-062-520-001
or P/N 209-062-607-001 that was manufactured by Circor Aerospace,
marked ``Circle Seal,'' and marked with a manufacturing date code of
``10/11'' (October 2011) through ``03/15'' (March 2015) on any
helicopter.
Differences Between This AD and the Service Information
The manufacturer's service information describes procedures for an
inspection of the check valves within 25 hours TIS for a crack and
allows 300 hours TIS to determine if the valve is affected and to
replace any affected check valve. This AD requires replacing all
affected check valves within 25 hours TIS.
Costs of Compliance
We estimate that this AD affects 161 (59 Model 212 and 102 Model
412) helicopters of U.S. Registry.
We estimate that operators may incur the following costs in order
to comply with this AD. At an average labor rate of $85, replacing each
check valve (engine oil or fuel) will require about 1 work-hour, and
required parts will cost $85. For the Model 212, we estimate a total
cost of $340 per helicopter and $20,060 for the U.S. fleet. For the
Model 412, we estimate a total cost of $170 per helicopter and $17,340
for the U.S. fleet.
According to Bell's service information some of the costs of this
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. We do not control warranty coverage by Bell.
Accordingly, we have included all costs in our cost estimate.
FAA's Justification and Determination of the Effective Date
Providing an opportunity for public comments prior to adopting
these AD requirements would delay implementing the safety actions
needed to correct this known unsafe condition. Therefore, we find that
the risk to the flying public justifies waiving notice and comment
prior to the adoption of this rule because the actions required by this
AD must be accomplished within 25 hours TIS, a very short interval for
helicopters used in firefighting and logging operations.
Since an unsafe condition exists that requires the immediate
adoption of this AD, we determined that notice and opportunity for
public comment before issuing this AD are impracticable and that good
cause exists for making this amendment effective in less than 30 days.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this 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, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska to the extent that
it justifies making a regulatory distinction; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared an economic evaluation of the estimated costs to comply
with this AD and placed it in the AD docket.
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):
2017-15-02 Bell Helicopter Textron, Inc. (Bell): Amendment 39-18962;
Docket No. FAA-2017-0701; Directorate Identifier 2016-SW-063-AD.
(a) Applicability
This AD applies to Bell Model 212 and 412 helicopters,
certificated in any category, with an engine oil check valve part
number (P/N) 209-062-520-001 or fuel check valve P/N 209-062-607-001
manufactured by Circor Aerospace, marked ``Circle Seal'' and with a
manufacturing date code of ``10/11'' (October 2011) through ``03/
15'' (March 2015), installed.
(b) Unsafe Condition
This AD defines the unsafe condition as a cracked or leaking
check valve, which could result in loss of lubrication or fuel to
the engine, failure of the engine or a fire, and subsequent loss of
control of the helicopter.
(c) Effective Date
This AD becomes effective August 4, 2017.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Actions
(1) Within 25 hours time-in-service:
(i) Replace each fuel check valve.
(ii) For Model 212 helicopters, replace each engine oil check
valve.
(2) After the effective date of this AD, do not install any
check valve P/N 209-062-520-001 or P/N 209-062-607-001 manufactured
by Circor Aerospace, marked ``Circle Seal'' and with a manufacturing
date code of ``10/11'' (October 2011) through ``03/15'' (March
2015), on any helicopter.
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Delegation Systems Certification Office, FAA,
may approve AMOCs for this AD. Send your proposal to: Jurgen E.
Priester, Aviation Safety Engineer, Delegation Systems Certification
Office, ASW-130, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177;
telephone (817) 222-5159; email jurgen.e.priester@faa.gov.
(2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, we suggest that you
notify your principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office or
certificate holding district office before operating any aircraft
complying with this AD through an AMOC.
[[Page 33441]]
(g) Additional Information
Bell Alert Service Bulletin (ASB) 212-15-153, dated September 4,
2015; Bell ASB 212-15-155, dated September 15, 2015; and Bell ASB
412-15-168, dated September 15, 2015, which are not incorporated by
reference, contain additional information about the subject of this
AD. For service information identified in this AD, contact Bell
Helicopter Textron, Inc., P.O. Box 482, Fort Worth, TX 76101;
telephone (817) 280-3391; fax (817) 280-6466; or at https://www.bellcustomer.com/files/. You may review this service information
at the FAA, Office of the Regional Counsel, Southwest Region, 10101
Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177.
(h) Subject
Joint Aircraft Service Component (JASC) Codes: 7900 Engine Oil
System and 2800 Aircraft Fuel System.
Issued in Fort Worth, Texas, on July 7, 2017.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2017-15031 Filed 7-19-17; 8:45 am]
BILLING CODE 4910-13-P