Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters, 49952-49954 [2020-17894]
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49952
Federal Register / Vol. 85, No. 159 / Monday, August 17, 2020 / Rules and Regulations
(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) Pacific Aerospace Mandatory Service
Bulletin PACSB/XL/105, Issue 4, dated
December 19, 2018.
(ii) [Reserved]
(3) For Pacific Aerospace Limited service
information identified in this AD, contact
Pacific Aerospace Limited, Airport Road,
Hamilton, Private Bag 3027, Hamilton 3240,
New Zealand; phone: +64 7843 6144; fax:
+64 7843 6134; email: pacific@
aerospace.co.nz; internet: https://
www.aerospace.co.nz.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 901 Locust,
Kansas City, Missouri 64106. For information
on the availability of this material at the
FAA, call (816) 329–4148. It is also available
on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2020–0716.
(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: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on July 29, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
valve. This AD requires installing
auxiliary circuit breaker modification
(MOD) kits and inserting a Rotorcraft
Flight Manual (RFM) Supplement into
the existing RFM for your helicopter.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective September
21, 2020.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of September 21, 2020.
ADDRESSES: For service information
identified in this final rule, contact your
local Sikorsky Field Representative or
Sikorsky’s Service Engineering Group at
Sikorsky Aircraft Corporation, 124
Quarry Road, Trumbull, CT 06611;
telephone 1–800–946–4337 (1–800–
Winged–S); email wcs_cust_service_
eng.gr-sik@lmco.com. Operators may
also log on to the Sikorsky 360 website
at https://www.sikorsky360.com. You
may view this service information at the
FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood
Pkwy., Room 6N–321, Fort Worth, TX
76177. For information on the
availability of this material at the FAA,
call 817–222–5110. It is also available
on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
1115.
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
1115; 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.
FOR FURTHER INFORMATION CONTACT:
Michael Schwetz, Aviation Safety
Engineer, Boston ACO Branch, FAA,
1200 District Avenue, Burlington, MA
01803; telephone 781–238–7761; email
michael.schwetz@faa.gov.
SUPPLEMENTARY INFORMATION:
The FAA is adopting a new
airworthiness directive (AD) for certain
Sikorsky Aircraft Corporation (Sikorsky)
Model S–92A helicopters. This AD was
prompted by two incidents of erroneous
low oil pressure caution cockpit
indications and unintended actuation of
the main gearbox (MGB) auto bypass
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to Sikorsky Model S–92A
helicopters, serial number (S/N) 920006
through 920304 inclusive and S/N
920311 through 920314 inclusive. The
[FR Doc. 2020–17864 Filed 8–14–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–1115; Project
Identifier 2018–SW–065–AD; Amendment
39–21203; AD 2020–16–19]
RIN 2120–AA64
Airworthiness Directives; Sikorsky
Aircraft Corporation Helicopters
AGENCY:
SUMMARY:
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NPRM published in the Federal
Register on February 18, 2020 (85 FR
8771). The NPRM was prompted by two
incidents of erroneous low oil pressure
caution cockpit indications and
unintended actuation of the MGB auto
bypass valve caused by unintended
popping of the M XMSN OIL WARN
circuit breaker during flight. The root
cause of this circuit breaker popping is
unknown. When this circuit breaker
trips, the following cautions will
display ‘‘MGB PUMP 1 FAIL, MGB
PUMP 2 FAIL, MGB OIL HOT, MGB
MAN COOL, MGB OIL PRES.’’ With the
MGB auto bypass valve actuated, the
MGB BYPASS caution will not
annunciate. For the given conditions,
the appropriate action for the crew is
‘‘land as soon as possible’’ in
accordance with the RFM Emergency
Procedures. The erroneous indications
conflicting with correct gauge readings
may overwhelm the flight crew,
resulting in a forced landing of the
helicopter.
To address this unsafe condition,
Sikorsky developed MOD kits based on
helicopter S/N to introduce a separate
circuit breaker for the MGB last jet
pressure switch. These MOD kits
specify reworking the overhead panel to
install new clips and brackets, circuit
breaker wiring harnesses, wiring MODs,
the auxiliary circuit breaker panel, and
the M XMSN PRESS SWITCH circuit
breaker. Accordingly, the NPRM
proposed to require installing MOD kits
and inserting an RFM Supplement into
the existing RFM for your helicopter.
The FAA is issuing this AD to address
the unsafe condition on these products.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The FAA received
comments from one commenter. The
following presents the comments
received on the NPRM and the FAA’s
response to the comments.
Request
The commenter expressed concern
about the compliance time of 400 hours
time-in-service (TIS), described it as a
substantial amount of time, and
suggested operators fix the problem
immediately. The commenter did not
provide a technical rationale for the
FAA to review.
The FAA disagrees that a shorter
compliance time is required to correct
the unsafe condition. In determining
that a compliance time of 400 hours TIS
mitigates the risk to an acceptable level,
the FAA considered factors including
Sikorsky service information, the scope
of the required actions in this AD, and
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Federal Register / Vol. 85, No. 159 / Monday, August 17, 2020 / Rules and Regulations
the scheduled maintenance for Sikorsky
Model S–92A helicopters.
Conclusion
The FAA reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
final rule as proposed.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Sikorsky Special
Service Instructions No. 92–121, dated
October 26, 2017 (SSI 92–121). This
service information describes
procedures for installing an auxiliary
circuit breaker panel MOD kit and M
XMSN PRESS SWITCH circuit breaker
MOD kit based on helicopter S/N.
The FAA also reviewed RFM
Supplement No. 45, Revision No. 2,
Sikorsky Model S–92A, Part 1, dated
April 27, 2017 (S–92A RFMS 45, Part 1,
Revision 2). This service information
specifies operating limitations, preflight
checks, normal and emergency
procedures, and malfunction
information for helicopters with
Avionics Management System version
7.1 or 8.0 with the MGB OIL OUT
warning activated, pump failure
indicating system, MGB auto bypass,
and M XMSN PRESS SWITCH circuit
breaker installed.
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.
Other Related Service Information
The FAA reviewed Sikorsky S–92
Helicopter Alert Service Bulletin 92–
63–037, Revision A, dated March 1,
2018. This service information contains
planning information pertaining to the
auxiliary circuit breaker panel and M
XMSN PRESS SWITCH circuit breaker
MOD kits, accomplishing SSI 92–121,
and inserting S–92A RFMS 45, Part 1,
Revision 2 into the helicopter cockpit.
Costs of Compliance
The FAA estimates that this AD
affects 36 helicopters of U.S. registry.
Labor costs are estimated at $85 per
work-hour. Based on these numbers, the
FAA estimates the following costs to
comply with this AD.
Modifying helicopters S/N 920006
through 920296 inclusive will take
about 48 work-hours and parts will cost
about $1,618 for an estimated cost of
$5,698 per helicopter and $182,336 for
the U.S. fleet size of 32 helicopters.
Modifying helicopters S/N 920297
through 920304 inclusive and S/N
920311 through 920314 inclusive will
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16:18 Aug 14, 2020
Jkt 250001
take about 2 work-hours and parts will
cost about $65 for an estimated cost of
$235 per helicopter and $940 for the
U.S. fleet size of 4 helicopters.
Revising the RFM will take about 0.5
work-hour for an estimated cost of $43
per helicopter and $1,548 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.
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
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.
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:
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49953
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 adding
the following new airworthiness
directive (AD):
■
2020–16–19 Sikorsky Aircraft Corporation:
Amendment 39–21203; Docket No.
FAA–2019–1115; Project Identifier
2018–SW–065–AD.
(a) Effective Date
This AD is effective September 21, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Sikorsky Aircraft
Corporation Model S–92A helicopters, serial
number (S/N) 920006 through 920304
inclusive and S/N 920311 through 920314
inclusive, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC)
Code: 6340, Rotor Drive Indicating System.
(e) Unsafe Condition
This AD was prompted by two incidents of
erroneous low oil pressure caution cockpit
indications and unintended actuation of the
main gearbox (MGB) auto bypass valve. The
FAA is issuing this AD to prevent the M
XMSM OIL WARN circuit breaker from
presenting erroneous cautions when tripped.
The unsafe condition, if not addressed, could
result in erroneous low oil pressure caution
cockpit indication, unintended actuation of
the MGB auto bypass valve, increased oil
temperature, conflicting indications, and
forced landing of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Within 400 hours time-in-service:
(1) For helicopters S/N 920006 through
920296 inclusive:
(i) Install Modification (MOD) Kit Clips
and Brackets part number (P/N) 92070–
20115–015 by following the Instructions,
paragraph B. of Sikorsky Special Service
Instructions No. 92–121, dated October 26,
2017 (SSI 92–121).
(ii) Install the first portion of MOD Kit
Auxiliary Circuit Breaker Panel P/N 92070–
55075–011 by following the Instructions,
paragraph C. of Sikorsky SSI 92–121.
(iii) Install MOD Kit Left Hand (LH)
Cockpit Auxiliary Power Unit P/N 92070–
55096–012 by following the Instructions,
paragraph D. of Sikorsky SSI 92–121.
(iv) Install MOD Kit LH Cabin Auxiliary
Power Unit P/N 92070–55096–013 by
following the Instructions, paragraph E. of
Sikorsky SSI 92–121.
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Federal Register / Vol. 85, No. 159 / Monday, August 17, 2020 / Rules and Regulations
(v) Install MOD Kit LH Top Deck FLD P/
N 92070–55096–016 by following the
Instructions, paragraph F. of Sikorsky SSI
92–121.
(vi) Install MOD Kit MGB XMSN P/N
92070–55096–017 by following the
Instructions, paragraph G. of Sikorsky SSI
92–121.
(vii) Install the completion portion of MOD
Kit Auxiliary Circuit Break Panel P/N 92070–
55075–011 by following the Instructions,
paragraph H. of Sikorsky SSI 92–121.
(viii) Install MOD Kit Auxiliary Cabin
Panel Faceplate P/N 92070–55075–012 by
following the Instructions, paragraph J. of
Sikorsky SSI 92–121.
(2) For helicopters S/N 920297 through
920304 inclusive and S/N 920311 through
920314 inclusive:
(i) Modify the auxiliary circuit breaker
panel and transmission harness by following
the Instructions, paragraph I. of Sikorsky SSI
92–121.
(ii) Install MOD Kit Auxiliary Cabin Panel
Faceplate P/N 92070–55075–012 by
following the Instructions, paragraph J. of
Sikorsky SSI 92–121.
(3) Insert a copy of the Rotorcraft Flight
Manual (RFM) Supplement No. 45, Revision
No. 2, Sikorsky Model S–92A, Part 1, dated
April 27, 2017, into the existing RFM for
your helicopter.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Sikorsky Special Service Instructions
No. 92–121, dated October 26, 2017.
(ii) Rotorcraft Flight Manual Supplement
No. 45, Revision No. 2, Sikorsky Model S–
92A, Part 1, dated April 27, 2017.
(3) For Sikorsky Aircraft Corporation
service information identified in this AD,
contact your local Sikorsky Field
Representative or Sikorsky’s Service
Engineering Group at Sikorsky Aircraft
Corporation, 124 Quarry Road, Trumbull, CT
06611; telephone 1–800–946–4337 (1–800–
Winged–S); email wcs_cust_service_eng.grsik@lmco.com. Operators may also log on to
the Sikorsky 360 website at https://
www.sikorsky360.com.
(4) You may view this service information
at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy.,
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,
email fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
(h) Credit for Previous Actions
Issued on July 30, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
Completion of the Accomplishment
Instructions of Sikorsky S–92 Helicopter
Alert Service Bulletin 92–63–037, Revision
A, dated March 1, 2018, before the effective
date of this AD is considered acceptable for
compliance with the actions required by
paragraph (g) of this AD.
[FR Doc. 2020–17894 Filed 8–14–20; 8:45 am]
BILLING CODE 4910–13–P
(i) Alternative Methods of Compliance
(AMOCs)
DEPARTMENT OF TRANSPORTATION
(1) The Manager, Boston ACO 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 (j) 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.
Federal Aviation Administration
(j) Related Information
For more information about this AD,
contact Michael Schwetz, Aviation Safety
Engineer, Boston ACO Branch, FAA, 1200
District Avenue, Burlington, MA 01803;
telephone 781–238–7761; email
michael.schwetz@faa.gov.
(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.
16:18 Aug 14, 2020
Jkt 250001
[Docket No. FAA–2020–0222; Project
Identifier AD–2019–00116–E; Amendment
39–21195; AD 2020–16–11]
RIN 2120–AA64
Airworthiness Directives; Continental
Aerospace Technologies, Inc. (Type
Certificate Previously Held by
Continental Motors, Inc.) Reciprocating
Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Continental Aerospace Technologies,
Inc. model GTSIO–520–C, GTSIO–520–
D, GTSIO–520–H, GTSIO–520–K,
GTSIO–520–L, GTSIO–520–M, GTSIO–
520–N, IO–550–G, IO–550–N, IO–550–
P, IO–550–R, IOF–550–N, IOF–550–P,
IOF–550–R, TSIO–520–BE, TSIO–550–
A, TSIO–550–B, TSIO–550–C, TSIO–
SUMMARY:
(k) Material Incorporated by Reference
VerDate Sep<11>2014
14 CFR Part 39
PO 00000
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Fmt 4700
Sfmt 4700
550–E, TSIO–550–G, TSIO–550–K,
TSIO–550–N, TSIOF–550–D, TSIOF–
550–J, TSIOF–550–K, and TSIOF–550–P
reciprocating aviation gasoline (AvGas)
engines with a certain cross-flow
cylinder assembly installed. This AD
was prompted by reports of in-flight
engine failures due to fractured crossflow cylinder assemblies. This AD
requires visual inspection and,
depending on the results of the
inspection, modification or replacement
of the cross-flow cylinder assembly. The
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective September
21, 2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 21, 2020.
ADDRESSES: For service information
identified in this final rule, contact
Continental Aerospace Technologies,
Inc., 2039 South Broad Street, Mobile,
Alabama 36615; phone: 251–436–8299;
website: https://
www.continentalmotors.aero. 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 781–238–7759.
It is also available on the internet at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–0222.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0222; 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.
FOR FURTHER INFORMATION CONTACT:
Boyce Jones, Aerospace Engineer,
Atlanta ACO Branch, FAA, 1701
Columbia Avenue, College Park, Georgia
30337; phone: 404–474–5535; fax: 404–
474–5606; email: boyce.jones@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all Continental Aerospace
E:\FR\FM\17AUR1.SGM
17AUR1
]]>Agencies
[Federal Register Volume 85, Number 159 (Monday, August 17, 2020)]
[Rules and Regulations]
[Pages 49952-49954]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-17894]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-1115; Project Identifier 2018-SW-065-AD; Amendment
39-21203; AD 2020-16-19]
RIN 2120-AA64
Airworthiness Directives; Sikorsky Aircraft Corporation
Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Sikorsky Aircraft Corporation (Sikorsky) Model S-92A
helicopters. This AD was prompted by two incidents of erroneous low oil
pressure caution cockpit indications and unintended actuation of the
main gearbox (MGB) auto bypass valve. This AD requires installing
auxiliary circuit breaker modification (MOD) kits and inserting a
Rotorcraft Flight Manual (RFM) Supplement into the existing RFM for
your helicopter. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective September 21, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of September 21,
2020.
ADDRESSES: For service information identified in this final rule,
contact your local Sikorsky Field Representative or Sikorsky's Service
Engineering Group at Sikorsky Aircraft Corporation, 124 Quarry Road,
Trumbull, CT 06611; telephone 1-800-946-4337 (1-800-Winged-S); email
[email protected]. Operators may also log on to the
Sikorsky 360 website at https://www.sikorsky360.com. You may view this
service information at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX
76177. For information on the availability of this material at the FAA,
call 817-222-5110. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
1115.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
1115; 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.
FOR FURTHER INFORMATION CONTACT: Michael Schwetz, Aviation Safety
Engineer, Boston ACO Branch, FAA, 1200 District Avenue, Burlington, MA
01803; telephone 781-238-7761; email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to Sikorsky Model S-92A
helicopters, serial number (S/N) 920006 through 920304 inclusive and S/
N 920311 through 920314 inclusive. The NPRM published in the Federal
Register on February 18, 2020 (85 FR 8771). The NPRM was prompted by
two incidents of erroneous low oil pressure caution cockpit indications
and unintended actuation of the MGB auto bypass valve caused by
unintended popping of the M XMSN OIL WARN circuit breaker during
flight. The root cause of this circuit breaker popping is unknown. When
this circuit breaker trips, the following cautions will display ``MGB
PUMP 1 FAIL, MGB PUMP 2 FAIL, MGB OIL HOT, MGB MAN COOL, MGB OIL
PRES.'' With the MGB auto bypass valve actuated, the MGB BYPASS caution
will not annunciate. For the given conditions, the appropriate action
for the crew is ``land as soon as possible'' in accordance with the RFM
Emergency Procedures. The erroneous indications conflicting with
correct gauge readings may overwhelm the flight crew, resulting in a
forced landing of the helicopter.
To address this unsafe condition, Sikorsky developed MOD kits based
on helicopter S/N to introduce a separate circuit breaker for the MGB
last jet pressure switch. These MOD kits specify reworking the overhead
panel to install new clips and brackets, circuit breaker wiring
harnesses, wiring MODs, the auxiliary circuit breaker panel, and the M
XMSN PRESS SWITCH circuit breaker. Accordingly, the NPRM proposed to
require installing MOD kits and inserting an RFM Supplement into the
existing RFM for your helicopter. The FAA is issuing this AD to address
the unsafe condition on these products.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received comments from one
commenter. The following presents the comments received on the NPRM and
the FAA's response to the comments.
Request
The commenter expressed concern about the compliance time of 400
hours time-in-service (TIS), described it as a substantial amount of
time, and suggested operators fix the problem immediately. The
commenter did not provide a technical rationale for the FAA to review.
The FAA disagrees that a shorter compliance time is required to
correct the unsafe condition. In determining that a compliance time of
400 hours TIS mitigates the risk to an acceptable level, the FAA
considered factors including Sikorsky service information, the scope of
the required actions in this AD, and
[[Page 49953]]
the scheduled maintenance for Sikorsky Model S-92A helicopters.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule as proposed.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Sikorsky Special Service Instructions No. 92-121,
dated October 26, 2017 (SSI 92-121). This service information describes
procedures for installing an auxiliary circuit breaker panel MOD kit
and M XMSN PRESS SWITCH circuit breaker MOD kit based on helicopter S/
N.
The FAA also reviewed RFM Supplement No. 45, Revision No. 2,
Sikorsky Model S-92A, Part 1, dated April 27, 2017 (S-92A RFMS 45, Part
1, Revision 2). This service information specifies operating
limitations, preflight checks, normal and emergency procedures, and
malfunction information for helicopters with Avionics Management System
version 7.1 or 8.0 with the MGB OIL OUT warning activated, pump failure
indicating system, MGB auto bypass, and M XMSN PRESS SWITCH circuit
breaker installed.
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.
Other Related Service Information
The FAA reviewed Sikorsky S-92 Helicopter Alert Service Bulletin
92-63-037, Revision A, dated March 1, 2018. This service information
contains planning information pertaining to the auxiliary circuit
breaker panel and M XMSN PRESS SWITCH circuit breaker MOD kits,
accomplishing SSI 92-121, and inserting S-92A RFMS 45, Part 1, Revision
2 into the helicopter cockpit.
Costs of Compliance
The FAA estimates that this AD affects 36 helicopters of U.S.
registry. Labor costs are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Modifying helicopters S/N 920006 through 920296 inclusive will take
about 48 work-hours and parts will cost about $1,618 for an estimated
cost of $5,698 per helicopter and $182,336 for the U.S. fleet size of
32 helicopters.
Modifying helicopters S/N 920297 through 920304 inclusive and S/N
920311 through 920314 inclusive will take about 2 work-hours and parts
will cost about $65 for an estimated cost of $235 per helicopter and
$940 for the U.S. fleet size of 4 helicopters.
Revising the RFM will take about 0.5 work-hour for an estimated
cost of $43 per helicopter and $1,548 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.
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
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.
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):
2020-16-19 Sikorsky Aircraft Corporation: Amendment 39-21203; Docket
No. FAA-2019-1115; Project Identifier 2018-SW-065-AD.
(a) Effective Date
This AD is effective September 21, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Sikorsky Aircraft Corporation Model S-92A
helicopters, serial number (S/N) 920006 through 920304 inclusive and
S/N 920311 through 920314 inclusive, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code: 6340, Rotor Drive
Indicating System.
(e) Unsafe Condition
This AD was prompted by two incidents of erroneous low oil
pressure caution cockpit indications and unintended actuation of the
main gearbox (MGB) auto bypass valve. The FAA is issuing this AD to
prevent the M XMSM OIL WARN circuit breaker from presenting
erroneous cautions when tripped. The unsafe condition, if not
addressed, could result in erroneous low oil pressure caution
cockpit indication, unintended actuation of the MGB auto bypass
valve, increased oil temperature, conflicting indications, and
forced landing of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 400 hours time-in-service:
(1) For helicopters S/N 920006 through 920296 inclusive:
(i) Install Modification (MOD) Kit Clips and Brackets part
number (P/N) 92070-20115-015 by following the Instructions,
paragraph B. of Sikorsky Special Service Instructions No. 92-121,
dated October 26, 2017 (SSI 92-121).
(ii) Install the first portion of MOD Kit Auxiliary Circuit
Breaker Panel P/N 92070-55075-011 by following the Instructions,
paragraph C. of Sikorsky SSI 92-121.
(iii) Install MOD Kit Left Hand (LH) Cockpit Auxiliary Power
Unit P/N 92070-55096-012 by following the Instructions, paragraph D.
of Sikorsky SSI 92-121.
(iv) Install MOD Kit LH Cabin Auxiliary Power Unit P/N 92070-
55096-013 by following the Instructions, paragraph E. of Sikorsky
SSI 92-121.
[[Page 49954]]
(v) Install MOD Kit LH Top Deck FLD P/N 92070-55096-016 by
following the Instructions, paragraph F. of Sikorsky SSI 92-121.
(vi) Install MOD Kit MGB XMSN P/N 92070-55096-017 by following
the Instructions, paragraph G. of Sikorsky SSI 92-121.
(vii) Install the completion portion of MOD Kit Auxiliary
Circuit Break Panel P/N 92070-55075-011 by following the
Instructions, paragraph H. of Sikorsky SSI 92-121.
(viii) Install MOD Kit Auxiliary Cabin Panel Faceplate P/N
92070-55075-012 by following the Instructions, paragraph J. of
Sikorsky SSI 92-121.
(2) For helicopters S/N 920297 through 920304 inclusive and S/N
920311 through 920314 inclusive:
(i) Modify the auxiliary circuit breaker panel and transmission
harness by following the Instructions, paragraph I. of Sikorsky SSI
92-121.
(ii) Install MOD Kit Auxiliary Cabin Panel Faceplate P/N 92070-
55075-012 by following the Instructions, paragraph J. of Sikorsky
SSI 92-121.
(3) Insert a copy of the Rotorcraft Flight Manual (RFM)
Supplement No. 45, Revision No. 2, Sikorsky Model S-92A, Part 1,
dated April 27, 2017, into the existing RFM for your helicopter.
(h) Credit for Previous Actions
Completion of the Accomplishment Instructions of Sikorsky S-92
Helicopter Alert Service Bulletin 92-63-037, Revision A, dated March
1, 2018, before the effective date of this AD is considered
acceptable for compliance with the actions required by paragraph (g)
of this AD.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Boston ACO 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 (j) 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.
(j) Related Information
For more information about this AD, contact Michael Schwetz,
Aviation Safety Engineer, Boston ACO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; telephone 781-238-7761; email
[email protected].
(k) 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) Sikorsky Special Service Instructions No. 92-121, dated
October 26, 2017.
(ii) Rotorcraft Flight Manual Supplement No. 45, Revision No. 2,
Sikorsky Model S-92A, Part 1, dated April 27, 2017.
(3) For Sikorsky Aircraft Corporation service information
identified in this AD, contact your local Sikorsky Field
Representative or Sikorsky's Service Engineering Group at Sikorsky
Aircraft Corporation, 124 Quarry Road, Trumbull, CT 06611; telephone
1-800-946-4337 (1-800-Winged-S); email [email protected]. Operators may also log on to the Sikorsky 360 website
at https://www.sikorsky360.com.
(4) You may view this service information at the FAA, Office of
the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., 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, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on July 30, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-17894 Filed 8-14-20; 8:45 am]
BILLING CODE 4910-13-P
