Published 2017-07-21 · Federal Register document 2017-15033
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Publication summary
We are adopting a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD requires installing an engine flame detector bracket assembly and harness assembly. This AD was prompted by reports of false fire warnings. The actions of this AD are intended to prevent an unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:54.997910+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2017-90ba553c3b802c53
- Source row
- results[206]
- Raw source SHA-256
- 90ba553c3b802c5316e8d18f30db5da9f7731a87f58278ec2965f199ef4375e9
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2017-10-10
- Effective date printed in this edition
- 2017-08-25
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 9 complete recorded clauses
Applicability wording · Applicability
(a) Applicability
This AD applies to Sikorsky Aircraft Corporation (Sikorsky)
Model S-92A helicopters, serial numbers 920006 through 920298,
certificated in any category.
Exact source excerpt. Text positions 8103–8282, end exclusive, in the original decoded publication. SHA-256: cf44ede2c43e2f18fd9aaaa877b7cdcf6cf334e81de815b396704b339b1634a9
Unsafe Condition
(b) Unsafe Condition
This AD defines the unsafe condition as a false fire warning.
This condition could result in an unnecessary emergency landing or
ditching.
Exact source excerpt. Text positions 8282–8450, end exclusive, in the original decoded publication. SHA-256: 3c32ee8c560905bac5067e9eb6fe8b1c4c470aff7b2edd2ba32d98abdcda3369
Effective Date
(c) Effective Date
This AD becomes effective August 25, 2017.
Exact source excerpt. Text positions 8450–8518, end exclusive, in the original decoded publication. SHA-256: 720d78667b39003af8ff7af345cc1a60bc5c74873ebd79bafb2baa0a61b2d89b
Compliance
(d) Compliance
You are responsible for performing each action required by this
AD within the
[[Page 33782]]
specified compliance time unless it has already been accomplished
prior to that time.
Exact source excerpt. Text positions 8518–8722, end exclusive, in the original decoded publication. SHA-256: e670ad2bb1f881e29b1a2810279ad42e2edca9757403d2a9e7460d8f00a7c4ff
Required Actions
(e) Required Actions
Within 180 hours time-in-service:
(1) For helicopters with a No. 2 engine outboard flame detector
bracket assembly (bracket) (either part number (P/N) 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
with a No. 2 engine flame detector harness assembly (harness) P/N
92310-04201-041 installed: If the harness was installed before the
bracket, replace the harness.
(2) For helicopters with a bracket (either P/N 92070-30033-014,
or both P/N 92070-30033-011 and 92070-30033-015) installed, and
without a harness P/N 92310-04201-041 installed: Remove the harness
and install harness P/N 92310-04201-041 by following the
Accomplishment Instructions, section 3.C.1, of Sikorsky S-92
Customer Service Notice 92-094, Revision B, dated June 14, 2016 (CSN
92-094).
(3) For helicopters without a bracket (either P/N 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
with a harness P/N 92310-04201-041 installed:
(i) Install a bracket P/N 92070-30033-014 by following the
Instructions, paragraph D, of Sikorsky Special Service Instructions
No. 92-107G, Revision G, dated February 25, 2016 (SSI 92-107G).
(ii) Replace the harness.
(4) For helicopters without a bracket (either P/N 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
without a harness P/N 92310-04201-041 installed:
(i) Install a bracket P/N 92070-30033-014 by following the
Instructions, paragraph D, of SSI 92-107G.
(ii) Remove the harness and install harness P/N 92310-04201-041
by following the Accomplishment Instructions, section 3.C.1, of CSN
92-094.
Exact source excerpt. Text positions 8722–10404, end exclusive, in the original decoded publication. SHA-256: 721cd97a9878062ed923fe9472da3d12e087f2045ea7d88115c7ba9d17c7f442
Alternative Methods of Compliance (AMOCs)
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Boston Aircraft Certification Office, FAA, may
approve AMOCs for this AD. Send your proposal to: Kristopher Greer,
Aerospace Engineer, Boston Aircraft Certification Office, Engine &
Propeller Directorate, 1200 District Avenue, Burlington,
Massachusetts 01803; telephone (781) 238-7799; email
[email protected].
(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.
Exact source excerpt. Text positions 10404–11163, end exclusive, in the original decoded publication. SHA-256: 27e1af3d1d0bf73f98e568b92f241af4b18793c98bc59d5803b3c5168a948d6b
Additional Information
(g) Additional Information
Sikorsky S-92 Alert Service Bulletin 92-26-006, Basic Issue,
dated February 25, 2016, and Sikorsky S-92 Alert Service Bulletin
92-26-007, Basic Issue, dated June 14, 2016, which are not
incorporated by reference, contain additional information about the
subject of this AD. For service information identified in this AD,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or
203-416-4299; email [email protected]. You may
review a copy of this service information at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177.
Exact source excerpt. Text positions 11163–11869, end exclusive, in the original decoded publication. SHA-256: 91092099697488d12abb574c1723756c4417a7e7a381d86861c262fb7252b9ba
Subject
(h) Subject
Joint Aircraft Service Component (JASC) Code: 2612, Fire
Detection.
Exact source excerpt. Text positions 11869–11956, end exclusive, in the original decoded publication. SHA-256: 97710459851e2fde36b1ffec290aba604d1ae0dab08c105cb23117ec67ad4f84
Material Incorporated by Reference
(i) 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) Sikorsky S-92 Customer Service Notice 92-094, Revision B,
dated June 14, 2016.
(ii) Sikorsky Special Service Instructions No. 92-107G, Revision
G, dated February 25, 2016.
(3) For Sikorsky service information identified in this AD,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or
203-416-4299; email [email protected].
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkw., Room 6N-
321, Fort Worth, TX 76177. 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, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 11956–13288, end exclusive, in the original decoded publication. SHA-256: 8506b52edf8fc6b6a88bebb44b1170095358e61660e8466ed4c1ca510f973c76
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 2017-10-10 · 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: 7ec389002b4107fdbcb7ce79618a82bf9b233386871732cabd041c94d1717c2b. Source manifest: c43879c1fbee531cd679c09f49f7bd75961bb640b2cb3adad6f848ee2bb13dc3.
Official source · 2017-07-21
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 82, Number 139 (Friday, July 21, 2017)]
[Rules and Regulations]
[Pages 33780-33782]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-15033]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-5443; Directorate Identifier 2016-SW-021-AD;
Amendment 39-18884; AD 2017-10-10]
RIN 2120-AA64
Airworthiness Directives; Sikorsky Aircraft Corporation
Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for
Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This
AD requires installing an engine flame detector bracket assembly and
harness assembly. This AD was prompted by reports of false fire
warnings. The actions of this AD are intended to prevent an unsafe
condition on these products.
DATES: This AD is effective August 25, 2017.
The Director of the Federal Register approved the incorporation by
reference of certain documents listed in this AD as of August 25, 2017.
ADDRESSES: For service information identified in this final rule,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or 203-
416-4299; email [email protected]. You may review a
copy of the referenced service information at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
5443.
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-
5443; or in person at the Docket
[[Page 33781]]
Operations Office between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this AD, any
incorporated-by-reference service information, the economic evaluation,
any comments received, and other information. The street address for
the Docket Operations Office (phone: 800-647-5527) is U.S. Department
of Transportation, Docket Operations Office, M-30, West Building Ground
Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Kristopher Greer, Aerospace Engineer,
Boston Aircraft Certification Office, Engine & Propeller Directorate,
1200 District Avenue, Burlington, Massachusetts 01803; telephone (781)
238-7799; email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On December 27, 2016, at 81 FR 95066, the Federal Register
published our notice of proposed rulemaking (NPRM), which proposed to
amend 14 CFR part 39 by adding an AD that would apply to Sikorsky Model
S-92A helicopters, serial numbers 920006 through 920298. The NPRM
proposed to require installing a No. 2 engine outboard flame detector
bracket assembly (bracket) and a No. 2 engine flame detector harness
assembly (harness), if not already installed or if the bracket was not
installed before the harness. The proposed AD was prompted by reports
of false fire indications from the No. 2 engine outboard flame
detectors. The proposed requirements were intended to prevent a false
fire warning, which could result in an unnecessary emergency landing or
ditching.
Comments
We gave the public the opportunity to participate in developing
this AD, but we received no comments on the NPRM.
FAA's Determination
We have reviewed the relevant information and determined that an
unsafe condition exists and is likely to exist or develop on other
products of these same type designs and that air safety and the public
interest require adopting the AD requirements as proposed.
Related Service Information Under 1 CFR Part 51
We reviewed Sikorsky S-92 Customer Service Notice 92-094, Revision
B, dated June 14, 2016, which provides procedures for installing
harness part number (P/N) 92310-04201-041.
We also reviewed Sikorsky Special Service Instructions No. 92-107G,
Revision G, dated February 25, 2016, (SSI No. 92-107G) which specifies
installing new brackets, P/N 92070-30033-011, 92070-30033-014, and
92070-30033-015, to increase the stability of the No. 2 engine outboard
flame detector.
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.
Other Related Service Information
We reviewed Sikorsky S-92 Alert Service Bulletin (ASB) 92-26-006,
Basic Issue, dated February 25, 2016. This service information provides
instructions for installing a new bracket by complying with SSI No. 92-
107G. We also reviewed S-92 ASB 92-26-007, Basic Issue, dated June 14,
2016. This service information specifies installing harness P/N 92310-
04201-041 after or concurrently with the new bracket.
Costs of Compliance
We estimate that this AD affects 50 helicopters of U.S. Registry
and that labor costs average $85 per work-hour. Based on these
estimates, we expect that installing a new bracket and harness requires
15.25 work hours for a labor cost of about $1,296. Parts cost $100 for
a total cost of about $1,396 per helicopter and $69,800 for the U.S.
fleet.
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.
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):
2017-10-10 Sikorsky Aircraft Corporation: Amendment 39-18884; Docket
No. FAA-2016-5443; Directorate Identifier 2016-SW-021-AD.
(a) Applicability
This AD applies to Sikorsky Aircraft Corporation (Sikorsky)
Model S-92A helicopters, serial numbers 920006 through 920298,
certificated in any category.
(b) Unsafe Condition
This AD defines the unsafe condition as a false fire warning.
This condition could result in an unnecessary emergency landing or
ditching.
(c) Effective Date
This AD becomes effective August 25, 2017.
(d) Compliance
You are responsible for performing each action required by this
AD within the
[[Page 33782]]
specified compliance time unless it has already been accomplished
prior to that time.
(e) Required Actions
Within 180 hours time-in-service:
(1) For helicopters with a No. 2 engine outboard flame detector
bracket assembly (bracket) (either part number (P/N) 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
with a No. 2 engine flame detector harness assembly (harness) P/N
92310-04201-041 installed: If the harness was installed before the
bracket, replace the harness.
(2) For helicopters with a bracket (either P/N 92070-30033-014,
or both P/N 92070-30033-011 and 92070-30033-015) installed, and
without a harness P/N 92310-04201-041 installed: Remove the harness
and install harness P/N 92310-04201-041 by following the
Accomplishment Instructions, section 3.C.1, of Sikorsky S-92
Customer Service Notice 92-094, Revision B, dated June 14, 2016 (CSN
92-094).
(3) For helicopters without a bracket (either P/N 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
with a harness P/N 92310-04201-041 installed:
(i) Install a bracket P/N 92070-30033-014 by following the
Instructions, paragraph D, of Sikorsky Special Service Instructions
No. 92-107G, Revision G, dated February 25, 2016 (SSI 92-107G).
(ii) Replace the harness.
(4) For helicopters without a bracket (either P/N 92070-30033-
014, or both P/N 92070-30033-011 and 92070-30033-015) installed, and
without a harness P/N 92310-04201-041 installed:
(i) Install a bracket P/N 92070-30033-014 by following the
Instructions, paragraph D, of SSI 92-107G.
(ii) Remove the harness and install harness P/N 92310-04201-041
by following the Accomplishment Instructions, section 3.C.1, of CSN
92-094.
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Boston Aircraft Certification Office, FAA, may
approve AMOCs for this AD. Send your proposal to: Kristopher Greer,
Aerospace Engineer, Boston Aircraft Certification Office, Engine &
Propeller Directorate, 1200 District Avenue, Burlington,
Massachusetts 01803; telephone (781) 238-7799; email
[email protected].
(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.
(g) Additional Information
Sikorsky S-92 Alert Service Bulletin 92-26-006, Basic Issue,
dated February 25, 2016, and Sikorsky S-92 Alert Service Bulletin
92-26-007, Basic Issue, dated June 14, 2016, which are not
incorporated by reference, contain additional information about the
subject of this AD. For service information identified in this AD,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or
203-416-4299; email [email protected]. You may
review a copy of 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) Code: 2612, Fire
Detection.
(i) 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) Sikorsky S-92 Customer Service Notice 92-094, Revision B,
dated June 14, 2016.
(ii) Sikorsky Special Service Instructions No. 92-107G, Revision
G, dated February 25, 2016.
(3) For Sikorsky service information identified in this AD,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or
203-416-4299; email [email protected].
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkw., Room 6N-
321, Fort Worth, TX 76177. 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, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Fort Worth, Texas, on May 5, 2017.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2017-15033 Filed 7-20-17; 8:45 am]
BILLING CODE 4910-13-P
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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:20:13.454561+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
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- Text SHA-256
- 7ec389002b4107fdbcb7ce79618a82bf9b233386871732cabd041c94d1717c2b
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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.