Airworthiness Directives; Continental Aerospace Technologies, Inc. Engines, 65120-65122 [2023-20445]
Download as PDF
65120
Federal Register / Vol. 88, No. 182 / Thursday, September 21, 2023 / Rules and Regulations
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) 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.
PART 39—AIRWORTHINESS
DIRECTIVES
(j) Alternative Methods of Compliance
(AMOCs)
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2023–17–12 Rolls-Royce Deutschland Ltd.
& Co. KG Engines: Amendment 39–
22538; Docket No. FAA–2023–1212;
Project Identifier MCAI–2022–00423–E.
(a) Effective Date
This airworthiness directive (AD) is
effective October 26, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Rolls-Royce
Deutschland Ltd. & Co. KG Model RB211
Trent 768–60, 772–60, and 772B–60 engines.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7230, Turbine Engine Compressor
Section.
ddrumheller on DSK120RN23PROD with RULES1
(e) Unsafe Condition
This AD was prompted by reports of cracks
on the intermediate-pressure compressor
(IPC) rotor shaft balance land. The FAA is
issuing this AD to detect cracks on the IPC
rotor shaft balance land. The unsafe
condition, if not addressed, could lead to IPC
rotor shaft failure and consequent
uncontained high-energy debris, possibly
resulting in damage to the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Except as specified in paragraphs (h) and
(i) of this AD: Perform all required actions
16:08 Sep 20, 2023
(1) Where EASA AD 2022–0055 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) This AD does not adopt the Remarks
paragraph of EASA AD 2022–0055.
(3) Where the service information
referenced in EASA AD 2022–0055 specifies
to use certain tooling, equivalent tooling may
be used.
Although the service information
referenced in EASA AD 2022–0055 specifies
to notify the manufacturer or supply pictures
to the manufacturer of any cracks, dents, or
nicks, this AD does not include that
requirement.
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
VerDate Sep<11>2014
(h) Exceptions to EASA AD 2022–0055
(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,
email: fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on September 18, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–20485 Filed 9–20–23; 8:45 am]
BILLING CODE 4910–13–P
(i) No Reporting Requirement
The Amendment
§ 39.13
within the compliance times specified in,
and in accordance with, European Union
Aviation Safety Agency AD 2022–0055, dated
March 23, 2022 (EASA AD 2022–0055).
Jkt 259001
(1) The Manager, AIR–520, Continued
Operational Safety 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 (k) of this AD and
email to: ANE-AD-AMOC@faa.gov.
(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.
(k) Additional Information
For more information about this AD,
contact Sungmo Cho, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des
Moines, WA 98198; phone: (781) 238–7241;
email: sungmo.d.cho@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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) European Union Aviation Safety Agency
(EASA) AD 2022–0055, dated March 23,
2022.
(ii) [Reserved]
(3) For EASA AD 2022–0055, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; phone: +49 221 8999 000;
email: ADs@easa.europa.eu; website:
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (817) 222–5110.
PO 00000
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Fmt 4700
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1159; Project
Identifier AD–2022–00692–E; Amendment
39–22530; AD 2023–17–04]
RIN 2120–AA64
Airworthiness Directives; Continental
Aerospace Technologies, Inc. Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2022–04–
04 for certain Continental Aerospace
Technologies, Inc. (Continental) Model
C–125, C145, IO–360, IO–470, IO–550,
O–300, O–470, TSIO–360, and TSIO–
520 series engines and certain
Continental Motors IO–520 series
engines with a certain oil filter adapter
installed. AD 2022–04–04 required
replacing the oil filter adapter fiber
gasket (fiber gasket) with an oil filter
adapter copper gasket (copper gasket).
This AD was prompted by reports of
two accidents that were the result of
power loss due to oil starvation. This
AD requires replacing the fiber gasket
with a copper gasket or a stainless steel
embedded within
polytetrafluoroethylene gasket (stainless
steel PTFE gasket). This AD also revises
the applicability to include Continental
model engines equipped with an F&M
Enterprises, Inc. (F&M) or a Stratus Tool
Technologies, LLC (Stratus) oil filter
adapter installed. The FAA is issuing
this AD to address the unsafe condition
on these products.
DATES: This AD is effective October 26,
2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of October 26, 2023.
ADDRESSES:
SUMMARY:
E:\FR\FM\21SER1.SGM
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Federal Register / Vol. 88, No. 182 / Thursday, September 21, 2023 / Rules and Regulations
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1159; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, any comments
received, and other information. The
address for Docket Operations is U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE, Washington, DC
20590.
Material Incorporated by Reference:
• For service information identified
in this final rule, contact Stratus Tool
Technologies, LLC, 2208 Air Park Drive,
Burlington, NC 27215; phone: (800)
822–3200; website: tempestplus.com.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call (817) 222–5110. It is also
available at regulations.gov under
Docket No. FAA–2022–1159.
FOR FURTHER INFORMATION CONTACT:
George Hanlin, Aviation Safety
Engineer, FAA, 1701 Columbia Avenue,
College Park, GA 30337; phone: (404)
474–5584; email: 9-ASO-ATLACO-ADs@
faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a supplemental
notice of proposed rulemaking (SNPRM)
to amend 14 CFR part 39 to supersede
AD 2022–04–04, Amendment 39–21945
(87 FR 9435, February 22, 2022) (AD
2022–04–04). AD 2022–04–04 applied
to certain Continental Model C–125,
C145, IO–360, IO–470, IO–520, IO–550,
O–300, O–470, TSIO–360, TSIO–520
series engines with a certain oil filter
adapter installed. The SNPRM
published in the Federal Register on
June 2, 2023 (88 FR 36258). The SNPRM
was prompted by a comment from an
individual commenter noting that
certain engine models were missing
from the applicability in the notice of
proposed rulemaking (NPRM). The
commenter also specified that the
referenced service information in the
NPRM has been revised by the
manufacturer. In response to this
comment, the FAA determined that
additional model engines are affected by
the unsafe condition and, as a result,
should be added to the applicability
paragraph of this AD. The FAA also
discovered that certain model engines,
with permold type crankcases, were
inadvertently included in the
applicability paragraph of the NPRM,
which the FAA removed in the SNPRM.
In the SNPRM, the FAA proposed to
require replacing the fiber gasket with a
copper or stainless steel PTFE gasket.
The FAA also proposed to revise the
applicability to include Continental
model engines equipped with an F&M
or a Stratus oil filter adapter installed
per Supplemental Type Certificate
SE8409SW, SE09356SC, or SE10348SC.
In addition, the FAA also proposed to
include the revised service information.
The FAA is issuing this AD to address
the unsafe condition on these products.
65121
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the SNPRM or on the determination of
the costs.
Conclusion
The FAA reviewed the relevant data
and determined that air safety requires
adoption of the AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on these
products. Except for minor editorial
changes, this AD is adopted as proposed
in the SNPRM.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Stratus Mandatory
Service Bulletin SB–001 Rev C, dated
June 16, 2022, which specifies
procedures for removing a fiber gasket
and replacing it with a copper gasket, P/
N AN900–28 or P/N AN900–29, or a
stainless steel PTFE gasket, P/N ST07,
as an improved alternative to the copper
gasket.
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.
Costs of Compliance
The FAA estimates that this AD
affects 6,300 engines installed on
airplanes of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
ddrumheller on DSK120RN23PROD with RULES1
ESTIMATED COSTS
Action
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
Replace fiber gasket with copper gasket or
stainless steel PTFE gasket.
2.5 work-hours × $85 per hour = $212.50 .....
$34
$246.50
$1,552,950
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.
The FAA is 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
VerDate Sep<11>2014
16:08 Sep 20, 2023
Jkt 259001
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
The FAA has 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
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
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) Will not affect intrastate aviation
in Alaska, and
(3) 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.
E:\FR\FM\21SER1.SGM
21SER1
65122
Federal Register / Vol. 88, No. 182 / Thursday, September 21, 2023 / Rules and Regulations
(g) Required Actions
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by:
a. Removing Airworthiness Directive
AD 2022–04–04, Amendment 39–21945
(87 FR 9435, February 22, 2022); and
■ b. Adding the following new
airworthiness directive:
■
■
2023–17–04 Continental Aerospace
Technologies, Inc.: Amendment 39–
22530; Docket No. FAA–2022–1159;
Project Identifier AD–2022–00692–E.
(b) Affected ADs
This AD replaces AD 2022–04–04,
Amendment 39–21945 (87 FR 9435, February
22, 2022) (AD 2022–04–04).
(c) Applicability
This AD applies to Continental Aerospace
Technologies, Inc. (Continental) model
engines equipped with an F&M Enterprises,
Inc. (F&M) or a Stratus Tool Technologies,
LLC (Stratus) oil filter adapter installed per
Supplemental Type Certificate SE8409SW,
SE09356SC, or SE10348SC.
Note 1 to paragraph (c): These F&M and
Stratus oil filter adapters are known to be
installed on Continental Model C–125, C–
145, GO–300, IO–360, IO–470, IO–520, IO–
550, O–300, O–470, TSIO–360, and TSIO–
520 series engines.
ddrumheller on DSK120RN23PROD with RULES1
(d) Subject
Joint Aircraft System Component (JASC)
Code 8550, Reciprocating Engine Oil System.
(e) Unsafe Condition
This AD was prompted by reports of two
accidents that were the result of power loss
due to oil starvation. The FAA is issuing this
AD to prevent loss of engine power. The
unsafe condition, if not addressed, could
result in failure of the engine, in-flight
shutdown, and loss of control of the airplane.
VerDate Sep<11>2014
16:08 Sep 20, 2023
Jkt 259001
(h) Installation Prohibition
After the effective date of this AD, do not
install an F&M or a Stratus oil filter adapter
fiber gasket on any affected engine.
(i) Credit for Previous Actions
You may take credit for the actions
required by paragraph (g) of this AD if you
performed those actions before the effective
date of this AD using Stratus Tool
Technologies Mandatory Service Bulletin
SB–001 Rev B, dated June 17, 2021, which
was previously approved for IBR on March
29, 2022 (87 FR 9435, February 22, 2022), but
is not incorporated by reference in this AD.
(j) Special Flight Permit
(a) Effective Date
This airworthiness directive (AD) is
effective October 26, 2023.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
Before accumulating 50 flight hours after
the effective date of this AD or at the next
scheduled oil change after the effective date
of this AD, whichever occurs first, remove
any F&M or Stratus oil filter adapter fiber
gasket from service and replace it with an oil
filter adapter copper gasket, part number (P/
N) AN900–28 or P/N AN900–29, or a
stainless steel polytetrafluoroethylene gasket,
P/N ST07, as applicable, in accordance with
the Compliance Instructions, paragraph 6.,
pages 6 through 10 (including all detailed
instructions for Figure 5 through Figure 16),
of Stratus Tool Technologies Mandatory
Service Bulletin SB–001 Rev C, dated June
16, 2022.
A special flight permit may be issued in
accordance with 14 CFR 21.197 and 21.199
to permit a one-time non-revenue ferry flight
to operate the airplane to the nearest location
where the maintenance action can be
performed provided that the engine oil
pressure and engine oil temperatures are in
their allowable ranges and there is no
noticeable increase in engine noise. This
flight must be performed with no passengers
on board.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, East Certification 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 branch, send it to the attention
of the person identified in paragraph (l) 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.
(3) AMOCs approved for AD 2022–04–04
are approved as AMOCs for the
corresponding provisions of this AD.
(l) Additional Information
For more information about this AD,
contact George Hanlin, Aviation Safety
Engineer, FAA, 1701 Columbia Avenue,
College Park, GA 30337; phone: (404) 474–
5584; email: 9-ASO-ATLACO-ADs@faa.gov.
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
(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) Stratus Tool Technologies Mandatory
Service Bulletin SB–001 Rev C, dated June
16, 2022.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Stratus Tool Technologies,
LLC, 2208 Air Park Drive, Burlington, NC
27215; phone: (800) 822–3200; website:
tempestplus.com.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (817) 222–5110.
(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,
email: fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on September 15, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–20445 Filed 9–20–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–1218; Project
Identifier MCAI–2022–01025–A; Amendment
39–22536; AD 2023–17–10]
RIN 2120–AA64
Airworthiness Directives; Vulcanair
S.p.A. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Vulcanair S.p.A. Model V1.0 airplanes.
This AD results from mandatory
continuing airworthiness information
(MCAI) originated by an aviation
authority of another country to identify
and correct an unsafe condition on an
aviation product. The MCAI identifies
the unsafe condition as corrosion on the
lower fuselage truss. This AD requires a
detailed visual inspection of the righthand (RH) and left-hand (LH) lower rear
attachments of the fuselage truss for
SUMMARY:
E:\FR\FM\21SER1.SGM
21SER1
Agencies
[Federal Register Volume 88, Number 182 (Thursday, September 21, 2023)]
[Rules and Regulations]
[Pages 65120-65122]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-20445]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1159; Project Identifier AD-2022-00692-E;
Amendment 39-22530; AD 2023-17-04]
RIN 2120-AA64
Airworthiness Directives; Continental Aerospace Technologies,
Inc. Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2022-04-04
for certain Continental Aerospace Technologies, Inc. (Continental)
Model C-125, C145, IO-360, IO-470, IO-550, O-300, O-470, TSIO-360, and
TSIO-520 series engines and certain Continental Motors IO-520 series
engines with a certain oil filter adapter installed. AD 2022-04-04
required replacing the oil filter adapter fiber gasket (fiber gasket)
with an oil filter adapter copper gasket (copper gasket). This AD was
prompted by reports of two accidents that were the result of power loss
due to oil starvation. This AD requires replacing the fiber gasket with
a copper gasket or a stainless steel embedded within
polytetrafluoroethylene gasket (stainless steel PTFE gasket). This AD
also revises the applicability to include Continental model engines
equipped with an F&M Enterprises, Inc. (F&M) or a Stratus Tool
Technologies, LLC (Stratus) oil filter adapter installed. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective October 26, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 26,
2023.
ADDRESSES:
[[Page 65121]]
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1159; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, any comments received, and other
information. The address for Docket Operations is U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For service information identified in this final rule,
contact Stratus Tool Technologies, LLC, 2208 Air Park Drive,
Burlington, NC 27215; phone: (800) 822-3200; website: tempestplus.com.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110. It is
also available at regulations.gov under Docket No. FAA-2022-1159.
FOR FURTHER INFORMATION CONTACT: George Hanlin, Aviation Safety
Engineer, FAA, 1701 Columbia Avenue, College Park, GA 30337; phone:
(404) 474-5584; email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a supplemental notice of proposed rulemaking (SNPRM)
to amend 14 CFR part 39 to supersede AD 2022-04-04, Amendment 39-21945
(87 FR 9435, February 22, 2022) (AD 2022-04-04). AD 2022-04-04 applied
to certain Continental Model C-125, C145, IO-360, IO-470, IO-520, IO-
550, O-300, O-470, TSIO-360, TSIO-520 series engines with a certain oil
filter adapter installed. The SNPRM published in the Federal Register
on June 2, 2023 (88 FR 36258). The SNPRM was prompted by a comment from
an individual commenter noting that certain engine models were missing
from the applicability in the notice of proposed rulemaking (NPRM). The
commenter also specified that the referenced service information in the
NPRM has been revised by the manufacturer. In response to this comment,
the FAA determined that additional model engines are affected by the
unsafe condition and, as a result, should be added to the applicability
paragraph of this AD. The FAA also discovered that certain model
engines, with permold type crankcases, were inadvertently included in
the applicability paragraph of the NPRM, which the FAA removed in the
SNPRM. In the SNPRM, the FAA proposed to require replacing the fiber
gasket with a copper or stainless steel PTFE gasket. The FAA also
proposed to revise the applicability to include Continental model
engines equipped with an F&M or a Stratus oil filter adapter installed
per Supplemental Type Certificate SE8409SW, SE09356SC, or SE10348SC. In
addition, the FAA also proposed to include the revised service
information. The FAA is issuing this AD to address the unsafe condition
on these products.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the SNPRM or on the determination
of the costs.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adoption of the AD as proposed. Accordingly, the FAA is
issuing this AD to address the unsafe condition on these products.
Except for minor editorial changes, this AD is adopted as proposed in
the SNPRM.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Stratus Mandatory Service Bulletin SB-001 Rev C,
dated June 16, 2022, which specifies procedures for removing a fiber
gasket and replacing it with a copper gasket, P/N AN900-28 or P/N
AN900-29, or a stainless steel PTFE gasket, P/N ST07, as an improved
alternative to the copper gasket.
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.
Costs of Compliance
The FAA estimates that this AD affects 6,300 engines installed on
airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace fiber gasket with copper 2.5 work-hours x $85 $34 $246.50 $1,552,950
gasket or stainless steel PTFE per hour = $212.50.
gasket.
----------------------------------------------------------------------------------------------------------------
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.
The FAA is 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
The FAA has 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) Will not affect intrastate aviation in Alaska, and
(3) 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.
[[Page 65122]]
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
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:
0
a. Removing Airworthiness Directive AD 2022-04-04, Amendment 39-21945
(87 FR 9435, February 22, 2022); and
0
b. Adding the following new airworthiness directive:
2023-17-04 Continental Aerospace Technologies, Inc.: Amendment 39-
22530; Docket No. FAA-2022-1159; Project Identifier AD-2022-00692-E.
(a) Effective Date
This airworthiness directive (AD) is effective October 26, 2023.
(b) Affected ADs
This AD replaces AD 2022-04-04, Amendment 39-21945 (87 FR 9435,
February 22, 2022) (AD 2022-04-04).
(c) Applicability
This AD applies to Continental Aerospace Technologies, Inc.
(Continental) model engines equipped with an F&M Enterprises, Inc.
(F&M) or a Stratus Tool Technologies, LLC (Stratus) oil filter
adapter installed per Supplemental Type Certificate SE8409SW,
SE09356SC, or SE10348SC.
Note 1 to paragraph (c): These F&M and Stratus oil filter
adapters are known to be installed on Continental Model C-125, C-
145, GO-300, IO-360, IO-470, IO-520, IO-550, O-300, O-470, TSIO-360,
and TSIO-520 series engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 8550, Reciprocating
Engine Oil System.
(e) Unsafe Condition
This AD was prompted by reports of two accidents that were the
result of power loss due to oil starvation. The FAA is issuing this
AD to prevent loss of engine power. The unsafe condition, if not
addressed, could result in failure of the engine, in-flight
shutdown, and loss of control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Before accumulating 50 flight hours after the effective date of
this AD or at the next scheduled oil change after the effective date
of this AD, whichever occurs first, remove any F&M or Stratus oil
filter adapter fiber gasket from service and replace it with an oil
filter adapter copper gasket, part number (P/N) AN900-28 or P/N
AN900-29, or a stainless steel polytetrafluoroethylene gasket, P/N
ST07, as applicable, in accordance with the Compliance Instructions,
paragraph 6., pages 6 through 10 (including all detailed
instructions for Figure 5 through Figure 16), of Stratus Tool
Technologies Mandatory Service Bulletin SB-001 Rev C, dated June 16,
2022.
(h) Installation Prohibition
After the effective date of this AD, do not install an F&M or a
Stratus oil filter adapter fiber gasket on any affected engine.
(i) Credit for Previous Actions
You may take credit for the actions required by paragraph (g) of
this AD if you performed those actions before the effective date of
this AD using Stratus Tool Technologies Mandatory Service Bulletin
SB-001 Rev B, dated June 17, 2021, which was previously approved for
IBR on March 29, 2022 (87 FR 9435, February 22, 2022), but is not
incorporated by reference in this AD.
(j) Special Flight Permit
A special flight permit may be issued in accordance with 14 CFR
21.197 and 21.199 to permit a one-time non-revenue ferry flight to
operate the airplane to the nearest location where the maintenance
action can be performed provided that the engine oil pressure and
engine oil temperatures are in their allowable ranges and there is
no noticeable increase in engine noise. This flight must be
performed with no passengers on board.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, East Certification 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 branch, send it to the
attention of the person identified in paragraph (l) 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.
(3) AMOCs approved for AD 2022-04-04 are approved as AMOCs for
the corresponding provisions of this AD.
(l) Additional Information
For more information about this AD, contact George Hanlin,
Aviation Safety Engineer, FAA, 1701 Columbia Avenue, College Park,
GA 30337; phone: (404) 474-5584; email: [email protected].
(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) Stratus Tool Technologies Mandatory Service Bulletin SB-001
Rev C, dated June 16, 2022.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Stratus Tool Technologies, LLC, 2208 Air Park Drive, Burlington, NC
27215; phone: (800) 822-3200; website: tempestplus.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110.
(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, email: [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on September 15, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-20445 Filed 9-20-23; 8:45 am]
BILLING CODE 4910-13-P