Published 2023-09-21 · Federal Register document 2023-20445
Airworthiness Directives; Continental Aerospace Technologies, Inc. Engines
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[255]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-17-04
- Effective date printed in this edition
- 2023-10-26
Read 13 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective October 26, 2023.
Exact source excerpt. Text positions 9298–9388, end exclusive, in the original decoded publication. SHA-256: 01330bead2fe3261a524b26f4ba062e1ef399bf130354d586202ee8a11d4df36
Affected ADs
(b) Affected ADs
This AD replaces AD 2022-04-04, Amendment 39-21945 (87 FR 9435,
February 22, 2022) (AD 2022-04-04).
Exact source excerpt. Text positions 9388–9512, end exclusive, in the original decoded publication. SHA-256: 1e78b0bcadeac07ba3c6e875d61f338e0d5d6b87f4b8146631858eddb1a4be28
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 9512–10045, end exclusive, in the original decoded publication. SHA-256: b9598e7e1791e29c5b1f9a33b3bef8c699a02237aef3958c070d9fd298b1c094
Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 8550, Reciprocating
Engine Oil System.
Exact source excerpt. Text positions 10045–10147, end exclusive, in the original decoded publication. SHA-256: e021385a7de56459392b1911092e4d1a1b66119d927984194df321fd63552b80
Unsafe Condition
(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.
Exact source excerpt. Text positions 10147–10481, end exclusive, in the original decoded publication. SHA-256: af5d9f33508538eb12135e470fed366773b22061ce5af90998f324ffab507227
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 10481–10583, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(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.
Exact source excerpt. Text positions 10583–11281, end exclusive, in the original decoded publication. SHA-256: f552f5e296778c42244adcd6b396e7d1919f0f66e593e84e9fa9b1c0a5f47975
Installation Prohibition
(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.
Exact source excerpt. Text positions 11281–11445, end exclusive, in the original decoded publication. SHA-256: e0fa3abb3fde39a08fa4ce67549054bf89f64591ebb465c83ab673c1dff04434
Credit for Previous Actions
(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.
Exact source excerpt. Text positions 11445–11861, end exclusive, in the original decoded publication. SHA-256: 334ea2bfb7f11f24bf8a4ebc721f9d6ce5595cec0d709d10b6d8fb9238eb95f6
Special Flight Permit
(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.
Exact source excerpt. Text positions 11861–12329, end exclusive, in the original decoded publication. SHA-256: 831a917f27de6aad3252328ff130bb5ede1d007adf5e95ddc778eabf0f3c5fe8
Alternative Methods of Compliance (AMOCs)
(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.
Exact source excerpt. Text positions 12329–13160, end exclusive, in the original decoded publication. SHA-256: 278ae61075d7fe35f0997a0ecc92caf2ce5fddef528e9cead632ecbd8318f9ce
Additional Information
(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].
Exact source excerpt. Text positions 13160–13380, end exclusive, in the original decoded publication. SHA-256: 2d19701e661a3e026b891e87ab4448485c2a86d17eca0f160de767a0d8a225d4
Material Incorporated by Reference
(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.
Exact source excerpt. Text positions 13380–14597, end exclusive, in the original decoded publication. SHA-256: 22da48ec5f5e1a74b767031c756e9e83ae6b6f6a5fda196c76fd3d03092254e3
Explicit historical replacement wording
Find all recorded historical references to AD 2023-17-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 5b105078dfd79b0c50d4f2ac11e3b572bed80e20af6a302a8a637769a7afb932. Source manifest: 149920b02c8e8b773f2b9b6402ce5346667ed36ac39c4db241b0b434e02e19bc.
Official source · 2023-09-21
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[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:
<bullet> 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.
<bullet> 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
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.