Published 2016-10-14 · Federal Register document 2016-24794
Airworthiness Directives; Continental Motors, Inc. Reciprocating Engines
Publication summary
We are adopting a new airworthiness directive (AD) for certain Continental Motors, Inc. (CMI) TSIO-550-K, TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating engines. This AD was prompted by a report of an uncommanded in-flight shutdown (IFSD) resulting in injuries and significant airplane damage. This AD requires replacing the oil cooler cross fitting assembly. We are issuing this AD to prevent failure of the oil cooler cross fitting and engine, IFSD, and loss of the airplane.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:51.853224+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2016-48fe8cb6c57c00b7
- Source row
- results[330]
- Raw source SHA-256
- 48fe8cb6c57c00b74623eb2b71ad0abe73b95a424a8ac83fecd389da4d1e3a81
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2016-21-04
- Effective date printed in this edition
- 2016-11-18
Read 9 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective November 18, 2016.
Exact source excerpt. Text positions 8403–8468, end exclusive, in the original decoded publication. SHA-256: eb630cdc90ad56ae3c19dc6042abdbae83632a9f4a4ff606a07909fa6d0ebff4
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8468–8497, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Continental Motors, Inc. (CMI) TSIO-550-K,
TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating
engines with an engine serial number below 1012296 and an oil cooler
cross fitting, part number AN918-1J or AN918-2J, installed.
Exact source excerpt. Text positions 8497–8782, end exclusive, in the original decoded publication. SHA-256: c638c6c99364415be9f76af3f829efe7d3f4766504b6f7466122c95cc4247877
Unsafe Condition
(d) Unsafe Condition
This AD was prompted by a report of an uncommanded in-flight
shutdown (IFSD) resulting in injuries and significant airplane
damage. We are issuing this AD to prevent failure of the oil cooler
cross fitting and engine, IFSD, and loss of the airplane.
Exact source excerpt. Text positions 8782–9062, end exclusive, in the original decoded publication. SHA-256: 2217e6873030aed642581de68ecb24c824a422c9179fe5f242e7fb5ea6bd1c66
Compliance
(e) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(1) Within 12 months or 100 flight hours after the effective
date of the AD, whichever occurs first, replace the oil cooler cross
fitting, nipple, and bushing. Use the Action Required paragraphs
III.1 through III.8 of CMI Critical Service Bulletin (CSB) CSB15-2,
Revision C, dated November 9, 2015 (also referred to as CMI CSB
CSB15-2C, dated November 9, 2015), or the Action Required paragraphs
III.1 through III.8 of CMI CSB CSB15-7, Revision B, dated April 26,
2016 (also referred to as CMI CSB15-7B, dated April 26, 2016), to
perform the replacement.
(2) Reserved.
Exact source excerpt. Text positions 9062–9749, end exclusive, in the original decoded publication. SHA-256: 60816f765cdbb37b496ccdeb19cf56e1149915bc4495bfc328d944d8deaf0b98
Credit for Previous Actions
(f) Credit for Previous Actions
You may take credit for the replacement that is required by
paragraph (e) of this AD, if the replacement was performed before
the effective date of this AD using CMI CSB CSB15-2B, dated November
6, 2015 or earlier versions; or CSB CSB15-7A, dated November 10,
2015 or earlier version.
Exact source excerpt. Text positions 9749–10076, end exclusive, in the original decoded publication. SHA-256: 2b6cb1341a3851a27bc5551ee1faafc418b5c23bf50bb6fc34bbc35651014978
Alternative Methods of Compliance (AMOCs)
(g) Alternative Methods of Compliance (AMOCs)
The Manager, Atlanta Certification Office, FAA, may approve
AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make
your request.
Exact source excerpt. Text positions 10076–10272, end exclusive, in the original decoded publication. SHA-256: 028572b07945ac816eecb70172b40db709d155fd5bdbeec925ee4528cdcf549a
Related Information
(h) Related Information
For more information about this AD, contact Scott Hopper,
Aerospace Engineer, Atlanta Aircraft Certification Office, FAA,
Small Airplane Directorate, 1701 Columbia Avenue, College Park, GA
30337; phone: 404-474-5535; fax: 404-474-5606; email:
[email protected].
Exact source excerpt. Text positions 10272–10568, end exclusive, in the original decoded publication. SHA-256: 3b38911a6ff042d751ff3b4100d96710b6b956418aa037ebc21ad195a6c6da49
Material Incorporated by Reference
(i) 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) Continental Motors, Inc. (CMI) Critical Service Bulletin
(CSB) CSB15-2, Revision C, dated November 9, 2015 (also referred to
as CMI CSB CSB15-2C, dated November 9, 2015).
(ii) CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also
referred to as CMI CSB CSB15-7B, dated April 26, 2016).
(3) For CMI service information identified in this AD, contact
Continental Motors, Inc., 2039 Broad Street, Mobile, Alabama 36615;
phone: 800-326-0089; Internet: http://www.continentalmotors.aero.
(4) You may view this service information at FAA, Engine &
Propeller Directorate, 1200 District Avenue, Burlington, MA. For
information on the availability of this material at the FAA, call
781-238-7125.
(5) You may view this service information at the National
Archives and Records Administration (NARA). For information on the
availability of this material at NARA, call 202-741-6030, or go to:
http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 10568–11912, end exclusive, in the original decoded publication. SHA-256: 9ec931879ae2d03847033692f4b64df40d4b4dd6aa59a4c9d8d3656019be83fd
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2016-21-04 · 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: 4333e60ff32c0b7624d287d934f229014243564e006ce55905a342005c3c91c2. Source manifest: 594058028834b595998090a2309fe46990a9f7e4c68cd8f5807f0c8fe5be908a.
Official source · 2016-10-14
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 81, Number 199 (Friday, October 14, 2016)]
[Rules and Regulations]
[Pages 70929-70931]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-24794]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-0069; Directorate Identifier 2016-NE-01-AD;
Amendment 39-18685; AD 2016-21-04]
RIN 2120-AA64
Airworthiness Directives; Continental Motors, Inc. Reciprocating
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Continental Motors, Inc. (CMI) TSIO-550-K, TSIOF-550-K, TSIO-550-C,
TSIOF-550-D, and TSIO-550-N reciprocating engines. This AD was
[[Page 70930]]
prompted by a report of an uncommanded in-flight shutdown (IFSD)
resulting in injuries and significant airplane damage. This AD requires
replacing the oil cooler cross fitting assembly. We are issuing this AD
to prevent failure of the oil cooler cross fitting and engine, IFSD,
and loss of the airplane.
DATES: This AD is effective November 18, 2016.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 18,
2016.
ADDRESSES: For service information identified in this final rule,
contact Continental Motors, Inc., 2039 Broad Street, Mobile, Alabama
36615; phone: 800-326-0089; Internet: http://www.continentalmotors.aero. You may view this service information at
the FAA, Engine & Propeller Directorate, 1200 District Avenue,
Burlington, MA. For information on the availability of this material at
the FAA, call 781-238-7125.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
0069; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The address for the Docket Office (phone: 800-647-
5527) is Document Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Scott Hopper, Aerospace Engineer,
Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate,
1701 Columbia Avenue, College Park, GA 30337; phone: 404-474-5535; fax:
404-474-5606; email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain CMI TSIO-550-K,
TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating
engines. The NPRM published in the Federal Register on March 11, 2016
(81 FR 12833). The NPRM was prompted by a report of an uncommanded IFSD
resulting in injuries and significant airplane damage. The NPRM
proposed to require replacing the oil cooler cross fitting assembly. We
are issuing this AD to correct the unsafe condition on these products.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
Change to Cost of Compliance
We increased our estimate of the cost of the affected parts in this
AD from $0 to $261 per engine and increased the number of labor hours
to perform the replacement from 1 to 2 hours. This increased the
overall estimated cost of compliance from $111,095 to $563,317.
Update to Service Information
We revised our reference in this AD from CMI Critical Service
Bulletin (CSB) CSB15-7, Revision A, dated November 10, 2015 (also
referred to as CMI CSB CSB15-7A, dated November 10, 2015) to CMI CSB
CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI CSB
CSB15-7B) to reflect the latest service information published by CMI.
Clarification of Part Number
We clarified in this AD that the affected oil cooler cross fitting
has a part number AN918-1J or AN918-2J.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed except for the
changes noted above. We have determined that these changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Relevant Service Information Under 1 CFR part 51
We reviewed CMI CSB CSB15-2, Revision C, dated November 9, 2015
(also referred to as CMI CSB CSB15-2C, dated November 9, 2015), and CMI
CSB CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI
CSB CSB15-7B, dated April 26, 2016). The CSBs describe detailed
procedures for replacing oil cooler cross fittings, nipples, and
bushings with a redesigned oil cooler cross fitting. 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
We estimate that this AD affects 1,307 engines installed on
airplanes of U.S. registry. We also estimate that it will take about 2
hours per engine to comply with this AD. The average labor rate is $85
per hour. Parts cost about $261 per engine. Based on these figures, we
estimate the total cost of this AD to U.S. operators to be $563,317.
Our cost estimate is exclusive of possible warranty coverage.
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
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
[[Page 70931]]
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):
2016-21-04 Continental Motors, Inc. (Type Certificate previously
held by Teledyne Continental Motors) Reciprocating Engines:
Amendment 39-18685; Docket No. FAA-2016-0069; Directorate Identifier
2016-NE-01-AD.
(a) Effective Date
This AD is effective November 18, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Continental Motors, Inc. (CMI) TSIO-550-K,
TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating
engines with an engine serial number below 1012296 and an oil cooler
cross fitting, part number AN918-1J or AN918-2J, installed.
(d) Unsafe Condition
This AD was prompted by a report of an uncommanded in-flight
shutdown (IFSD) resulting in injuries and significant airplane
damage. We are issuing this AD to prevent failure of the oil cooler
cross fitting and engine, IFSD, and loss of the airplane.
(e) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(1) Within 12 months or 100 flight hours after the effective
date of the AD, whichever occurs first, replace the oil cooler cross
fitting, nipple, and bushing. Use the Action Required paragraphs
III.1 through III.8 of CMI Critical Service Bulletin (CSB) CSB15-2,
Revision C, dated November 9, 2015 (also referred to as CMI CSB
CSB15-2C, dated November 9, 2015), or the Action Required paragraphs
III.1 through III.8 of CMI CSB CSB15-7, Revision B, dated April 26,
2016 (also referred to as CMI CSB15-7B, dated April 26, 2016), to
perform the replacement.
(2) Reserved.
(f) Credit for Previous Actions
You may take credit for the replacement that is required by
paragraph (e) of this AD, if the replacement was performed before
the effective date of this AD using CMI CSB CSB15-2B, dated November
6, 2015 or earlier versions; or CSB CSB15-7A, dated November 10,
2015 or earlier version.
(g) Alternative Methods of Compliance (AMOCs)
The Manager, Atlanta Certification Office, FAA, may approve
AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make
your request.
(h) Related Information
For more information about this AD, contact Scott Hopper,
Aerospace Engineer, Atlanta Aircraft Certification Office, FAA,
Small Airplane Directorate, 1701 Columbia Avenue, College Park, GA
30337; phone: 404-474-5535; fax: 404-474-5606; email:
[email protected].
(i) 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) Continental Motors, Inc. (CMI) Critical Service Bulletin
(CSB) CSB15-2, Revision C, dated November 9, 2015 (also referred to
as CMI CSB CSB15-2C, dated November 9, 2015).
(ii) CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also
referred to as CMI CSB CSB15-7B, dated April 26, 2016).
(3) For CMI service information identified in this AD, contact
Continental Motors, Inc., 2039 Broad Street, Mobile, Alabama 36615;
phone: 800-326-0089; Internet: http://www.continentalmotors.aero.
(4) You may view this service information at FAA, Engine &
Propeller Directorate, 1200 District Avenue, Burlington, MA. For
information on the availability of this material at the FAA, call
781-238-7125.
(5) You may view this service information at the National
Archives and Records Administration (NARA). For information on the
availability of this material at NARA, call 202-741-6030, or go to:
http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Burlington, Massachusetts, on October 7, 2016.
Colleen M. D'Alessandro,
Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2016-24794 Filed 10-13-16; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:25:10.917875+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 960c90c581fc934778b15cb92075545ec95a08b614f964034577c8c6cef817d4
- Text SHA-256
- 4333e60ff32c0b7624d287d934f229014243564e006ce55905a342005c3c91c2
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
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.