Airworthiness Directives; Robinson Helicopter Company Helicopters, 58084-58086 [2024-15707]
Download as PDF
58084
Federal Register / Vol. 89, No. 137 / Wednesday, July 17, 2024 / Proposed Rules
(2) You must use this material as
applicable to do the actions required by this
AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2024–0073, dated March 18,
2024.
(ii) [Reserved]
(3) For EASA AD 2024–0073 identified in
this AD, contact EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email ADs@
easa.europa.eu; website easa.europa.eu. You
may find this EASA AD on the EASA website
at ad.easa.europa.eu.
(4) You may view this material at the FAA,
Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(5) You may view this material at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
visit www.archives.gov/federal-register/cfr/
ibr-locationsoremailfr.inspection@nara.gov.
Issued on July 9, 2024.
Peter A. White,
Deputy Director, Integrated Certificate
Management Division, Aircraft Certification
Service.
[FR Doc. 2024–15378 Filed 7–16–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1886; Project
Identifier AD–2023–01018–R]
RIN 2120–AA64
Airworthiness Directives; Robinson
Helicopter Company Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
Robinson Helicopter Company
(Robinson Helicopter) Model R22 Beta,
R22 Mariner, R44, and R44 II
helicopters with a certain governor
controller installed. This proposed AD
was prompted by reports of engine
governor failure, which was a result of
water intrusion inside of the governor
controller. This proposed AD would
require removing certain governor
controllers from service and installing a
part eligible for installation. This
proposed AD would also prohibit
installing certain governor controllers
on any helicopter. The FAA is
proposing this AD to address the unsafe
condition on these products.
ddrumheller on DSK120RN23PROD with PROPOSALS1
SUMMARY:
VerDate Sep<11>2014
16:31 Jul 16, 2024
Jkt 262001
The FAA must receive comments
on this proposed AD by September 3,
2024.
DATES:
You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
regulations.gov. Follow the instructions
for submitting comments.
• Fax: (202) 493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–1886; 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 NPRM, any comments
received, and other information. The
street address for Docket Operations is
listed above.
Material Incorporated by Reference:
• For Robinson Helicopter service
information, contact Robinson
Helicopter Company, Technical Support
Department, 2901 Airport Drive,
Torrance, CA 90505; phone (310) 539–
0508; fax (310) 539–5198; email ts1@
robinsonheli.com; or at
robinsonheli.com.
• You may view this service
information at the FAA, Office of the
Regional Counsel, Southwest Region,
10101 Hillwood Parkway, Room 6N–
321, Fort Worth, TX 76177. For
information on the availability of this
material at the FAA, call (817) 222–
5110.
Other Related Service Information:
For Robinson service information
identified in this NPRM, contact
Robinson Helicopter Company at its
contact information under Material
Incorporated by Reference above.
FOR FURTHER INFORMATION CONTACT: Eric
Moreland, Aviation Safety Engineer,
FAA, 3960 Paramount Boulevard,
Lakewood, CA 90712; phone: (562) 627–
5364; email: eric.r.moreland@faa.gov.
SUPPLEMENTARY INFORMATION:
ADDRESSES:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2024–1886; Project Identifier AD–
2023–01018–R’’ at the beginning of your
PO 00000
Frm 00005
Fmt 4702
Sfmt 4702
comments. The most helpful comments
reference a specific portion of the
proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend this proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Eric Moreland,
Aviation Safety Engineer, FAA, 3960
Paramount Boulevard, Lakewood, CA
90712; phone: (562) 627–5364; email:
eric.r.moreland@faa.gov. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
Background
The FAA has received three reports of
governor controller failures involving
Robinson Helicopter Model R22 Beta
and R44 II helicopters. These failures
resulted in three underspeed or
overspeed events, and two of these
events resulted in hard landings which
caused significant damage to the
helicopters. Each of these separate
incidents occurred after significant
rainfall where the helicopter was
exposed to those weather conditions.
Prior to these governor controller
failures, several operators notified
Robinson Helicopter of a malfunction of
the governor controller. Subsequent
investigation revealed evidence of water
E:\FR\FM\17JYP1.SGM
17JYP1
Federal Register / Vol. 89, No. 137 / Wednesday, July 17, 2024 / Proposed Rules
spotting inside of these governor
controllers. Testing involving the
application of water to the electronics of
a governor controller confirmed that
these conditions result in this
malfunction. As a result of this
investigation, it has been determined
that the root cause for these
malfunctions is water intrusion in the
circuit board of the governor controller.
In light of this, Robinson Helicopter
issued service bulletins which specify
exchanging the existing governor
controller with a governor which
provides additional moisture protection.
Since the affected parts may also be
installed on Robinson Helicopter Model
R22 Mariner and R44 helicopters, those
model helicopters are also affected by
the unsafe condition. The affected parts
cannot be installed on Robinson
Helicopter Model R22 and R22 Alpha
helicopters, so those model helicopters
are not affected by the unsafe condition.
The unsafe condition, if not addressed,
could result in loss of engine speed
governing such as an engine overspeed
or underspeed condition, and
subsequent unexpected loss of power
during critical phases of flight and
landing.
FAA’s Determination
The FAA is issuing this NPRM after
determining that the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
ddrumheller on DSK120RN23PROD with PROPOSALS1
Related Service Information Under 1
CFR Part 51
The FAA reviewed Robinson
Helicopter R22 Service Bulletin SB–121
and Robinson Helicopter R44 Service
Bulletin SB–114, each dated June 28,
2023 (SB–121 and SB–114). This service
information specifies procedures for
removing governor controller part
number (P/N) D270–1, Revision A thru
E, and replacing it with governor
controller P/N D270–1, Revision F (or
subsequent).
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 ADDRESSES.
Other Related Service Information
The FAA also reviewed Robinson R22
and R44 Engine Monitoring Unit (EMU)
Technician’s PC Software Guide, dated
Oct 9, 2020. This service information
provides information to program the
new EMU ID for the governor controller.
VerDate Sep<11>2014
16:31 Jul 16, 2024
Jkt 262001
Proposed AD Requirements in This
NPRM
This proposed AD would require
removing any governor controller P/N
D270–1, Revision A thru E inclusive,
from service and installing a governor
controller P/N D270–1, Revision F or
later approved revision. This proposed
AD would also prohibit installing
governor controller P/N D270–1,
Revision A through E inclusive, on any
helicopter.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 140
helicopters of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD. Labor costs are
estimated at $85 per work-hour.
Replacing the governor controller
would take approximately 2 work-hours
and parts would cost approximately
$1,800 for an estimated cost of $1,970
per helicopter and $275,800 for the U.S.
fleet.
Differences Between This Proposed AD
and the Service Information
The service information applies to
Robinson Helicopter Model R22-series
and R44-series helicopters with a
certain P/N D270–1 governor controllers
installed and also identifies which
serial-numbered helicopters the affected
parts were factory installed on, whereas
this proposed AD would apply to all
Robinson Helicopter Model R22 Beta,
R22 Mariner, R44, and R44 II
helicopters with a certain P/N D270–1
governor controllers installed. This
proposed AD would require
accomplishing certain actions specified
in SB–121 or SB–114, as applicable to
your helicopter model, except the
procedures in paragraph 4. of SB–121
and SB–114 must be accomplished by
persons authorized under 14 CFR 43.3.,
instead of ‘‘an appropriately rated
person.’’
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
PO 00000
Frm 00006
Fmt 4702
Sfmt 4702
58085
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 determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would 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 this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would 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.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Robinson Helicopter Company: Docket No.
FAA–2024–1886; Project Identifier AD–
2023–01018–R.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by September 3,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Robinson Helicopter
Company Model R22 Beta, R22 Mariner, R44,
and R44 II helicopters, certificated in any
category, with a governor controller part
number (P/N) D270–1, Revision A through E
inclusive, installed.
E:\FR\FM\17JYP1.SGM
17JYP1
58086
Federal Register / Vol. 89, No. 137 / Wednesday, July 17, 2024 / Proposed Rules
(d) Subject
Joint Aircraft System Component (JASC)
Code: 2700, Flight Control System.
(e) Unsafe Condition
This AD was prompted by reports of
engine governor failures caused by water
intrusion. The FAA is issuing this AD to
prevent engine governor failures. The unsafe
condition, if not addressed, could result in
loss of engine speed governing such as an
engine overspeed or underspeed condition,
and subsequent unexpected loss of power
during critical phases of flight and landing.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) Within 90 days after the effective date
of this AD, remove the governor controller
from service and install a governor controller
P/N D270–1, Revision F or later approved
revision by following the Compliance
Procedure, paragraphs 2. though 5., of
Robinson Helicopter Company R22 Service
Bulletin SB–121 or R44 Service Bulletin SB–
114, each dated June 28, 2023 (SB–121 or
SB–114), as applicable to your helicopter
model, except the procedures in paragraph 4.
of SB–121 and SB–114 must be accomplished
by persons authorized under 14 CFR 43.3.
(2) As of the effective date of this AD, do
not install any governor controller P/N D270–
1, Revision A through E inclusive, on any
helicopter.
ddrumheller on DSK120RN23PROD with PROPOSALS1
(h) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, West 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 West Certification
Branch, send it to the attention of the person
identified in paragraph (i) of this AD.
Information may be emailed to: 9-ANMLAACO-AMOC-REQUESTS@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(i) Additional Information
For more information about this AD,
contact Eric Moreland, Aviation Safety
Engineer, FAA, 3960 Paramount Boulevard,
Lakewood, CA 90712; phone: (562) 627–
5364; email: eric.r.moreland@faa.gov.
(j) 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.
VerDate Sep<11>2014
16:31 Jul 16, 2024
Jkt 262001
(i) Robinson Helicopter Company R22
Service Bulletin SB–121, dated June 28,
2023.
(ii) Robinson Helicopter Company R44
Service Bulletin SB–114, dated June 28,
2023.
(3) For Robinson Helicopter Company
service information, contact Robinson
Helicopter Company, Technical Support
Department, 2901 Airport Drive, Torrance,
CA 90505; phone (310) 539–0508; fax (310)
539–5198; email ts1@robinsonheli.com; or at
robinsonheli.com.
(4) You may view this service information
at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Parkway,
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 material at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
visit www.archives.gov/federal-register/cfr/
ibr-locations or email fr.inspection@nara.gov.
Issued on July 10, 2024.
James D. Foltz,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–15707 Filed 7–16–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1890; Project
Identifier MCAI–2024–00087–T]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to
supersede Airworthiness Directive (AD)
2022–24–05, which applies to all Airbus
SAS Model A318, A319, A320, and
A321 series airplanes. AD 2022–24–05
requires repetitive inspections of certain
galleys for corrosion of trolley retainer
aluminum blocks and delamination of
the upper panel of the trolley
compartment, and applicable corrective
action. Since the FAA issued AD 2022–
24–05, the list of affected galleys has
been revised, and a modification has
been developed to restore the design
integrity of the affected galleys. This
proposed AD would continue to require
the actions in AD 2022–24–05, provide
optional terminating action for the
repetitive inspections, revise the list of
affected parts, and prohibit the
installation of affected parts under
SUMMARY:
PO 00000
Frm 00007
Fmt 4702
Sfmt 4702
certain conditions, as specified in a
European Union Aviation Safety Agency
(EASA). The FAA is proposing this AD
to address the unsafe condition on these
products.
DATES: The FAA must receive comments
on this proposed AD by September 3,
2024.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
regulations.gov. Follow the instructions
for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–1890; 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 NPRM, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For material identified in this
proposed AD, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000;
email ADs@easa.europa.eu; website
easa.europa.eu. You may find this
material on the EASA website at
ad.easa.europa.eu. It is also available at
regulations.gov under Docket No. FAA–
2024–1890.
• You may view this material at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
Timothy Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone:
817–222–5102; email:
Timothy.P.Dowling@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2024–1890; Project Identifier
E:\FR\FM\17JYP1.SGM
17JYP1
Agencies
[Federal Register Volume 89, Number 137 (Wednesday, July 17, 2024)]
[Proposed Rules]
[Pages 58084-58086]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-15707]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1886; Project Identifier AD-2023-01018-R]
RIN 2120-AA64
Airworthiness Directives; Robinson Helicopter Company Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for Robinson Helicopter Company (Robinson Helicopter) Model R22 Beta,
R22 Mariner, R44, and R44 II helicopters with a certain governor
controller installed. This proposed AD was prompted by reports of
engine governor failure, which was a result of water intrusion inside
of the governor controller. This proposed AD would require removing
certain governor controllers from service and installing a part
eligible for installation. This proposed AD would also prohibit
installing certain governor controllers on any helicopter. The FAA is
proposing this AD to address the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by September
3, 2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-1886; 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 NPRM, any comments received, and other
information. The street address for Docket Operations is listed above.
Material Incorporated by Reference:
For Robinson Helicopter service information, contact
Robinson Helicopter Company, Technical Support Department, 2901 Airport
Drive, Torrance, CA 90505; phone (310) 539-0508; fax (310) 539-5198;
email robinsonheli.com">ts1@robinsonheli.com; or at robinsonheli.com.
You may view this service information at the FAA, Office
of the Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room
6N-321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call (817) 222-5110.
Other Related Service Information: For Robinson service information
identified in this NPRM, contact Robinson Helicopter Company at its
contact information under Material Incorporated by Reference above.
FOR FURTHER INFORMATION CONTACT: Eric Moreland, Aviation Safety
Engineer, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712; phone:
(562) 627-5364; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-1886; Project Identifier
AD-2023-01018-R'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Eric
Moreland, Aviation Safety Engineer, FAA, 3960 Paramount Boulevard,
Lakewood, CA 90712; phone: (562) 627-5364; email:
[email protected]. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.
Background
The FAA has received three reports of governor controller failures
involving Robinson Helicopter Model R22 Beta and R44 II helicopters.
These failures resulted in three underspeed or overspeed events, and
two of these events resulted in hard landings which caused significant
damage to the helicopters. Each of these separate incidents occurred
after significant rainfall where the helicopter was exposed to those
weather conditions. Prior to these governor controller failures,
several operators notified Robinson Helicopter of a malfunction of the
governor controller. Subsequent investigation revealed evidence of
water
[[Page 58085]]
spotting inside of these governor controllers. Testing involving the
application of water to the electronics of a governor controller
confirmed that these conditions result in this malfunction. As a result
of this investigation, it has been determined that the root cause for
these malfunctions is water intrusion in the circuit board of the
governor controller. In light of this, Robinson Helicopter issued
service bulletins which specify exchanging the existing governor
controller with a governor which provides additional moisture
protection. Since the affected parts may also be installed on Robinson
Helicopter Model R22 Mariner and R44 helicopters, those model
helicopters are also affected by the unsafe condition. The affected
parts cannot be installed on Robinson Helicopter Model R22 and R22
Alpha helicopters, so those model helicopters are not affected by the
unsafe condition. The unsafe condition, if not addressed, could result
in loss of engine speed governing such as an engine overspeed or
underspeed condition, and subsequent unexpected loss of power during
critical phases of flight and landing.
FAA's Determination
The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Robinson Helicopter R22 Service Bulletin SB-121
and Robinson Helicopter R44 Service Bulletin SB-114, each dated June
28, 2023 (SB-121 and SB-114). This service information specifies
procedures for removing governor controller part number (P/N) D270-1,
Revision A thru E, and replacing it with governor controller P/N D270-
1, Revision F (or subsequent).
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 ADDRESSES.
Other Related Service Information
The FAA also reviewed Robinson R22 and R44 Engine Monitoring Unit
(EMU) Technician's PC Software Guide, dated Oct 9, 2020. This service
information provides information to program the new EMU ID for the
governor controller.
Proposed AD Requirements in This NPRM
This proposed AD would require removing any governor controller P/N
D270-1, Revision A thru E inclusive, from service and installing a
governor controller P/N D270-1, Revision F or later approved revision.
This proposed AD would also prohibit installing governor controller P/N
D270-1, Revision A through E inclusive, on any helicopter.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 140 helicopters of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD. Labor costs are
estimated at $85 per work-hour.
Replacing the governor controller would take approximately 2 work-
hours and parts would cost approximately $1,800 for an estimated cost
of $1,970 per helicopter and $275,800 for the U.S. fleet.
Differences Between This Proposed AD and the Service Information
The service information applies to Robinson Helicopter Model R22-
series and R44-series helicopters with a certain P/N D270-1 governor
controllers installed and also identifies which serial-numbered
helicopters the affected parts were factory installed on, whereas this
proposed AD would apply to all Robinson Helicopter Model R22 Beta, R22
Mariner, R44, and R44 II helicopters with a certain P/N D270-1 governor
controllers installed. This proposed AD would require accomplishing
certain actions specified in SB-121 or SB-114, as applicable to your
helicopter model, except the procedures in paragraph 4. of SB-121 and
SB-114 must be accomplished by persons authorized under 14 CFR 43.3.,
instead of ``an appropriately rated person.''
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 determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
Robinson Helicopter Company: Docket No. FAA-2024-1886; Project
Identifier AD-2023-01018-R.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by September 3, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Robinson Helicopter Company Model R22
Beta, R22 Mariner, R44, and R44 II helicopters, certificated in any
category, with a governor controller part number (P/N) D270-1,
Revision A through E inclusive, installed.
[[Page 58086]]
(d) Subject
Joint Aircraft System Component (JASC) Code: 2700, Flight
Control System.
(e) Unsafe Condition
This AD was prompted by reports of engine governor failures
caused by water intrusion. The FAA is issuing this AD to prevent
engine governor failures. The unsafe condition, if not addressed,
could result in loss of engine speed governing such as an engine
overspeed or underspeed condition, and subsequent unexpected loss of
power during critical phases of flight and landing.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) Within 90 days after the effective date of this AD, remove
the governor controller from service and install a governor
controller P/N D270-1, Revision F or later approved revision by
following the Compliance Procedure, paragraphs 2. though 5., of
Robinson Helicopter Company R22 Service Bulletin SB-121 or R44
Service Bulletin SB-114, each dated June 28, 2023 (SB-121 or SB-
114), as applicable to your helicopter model, except the procedures
in paragraph 4. of SB-121 and SB-114 must be accomplished by persons
authorized under 14 CFR 43.3.
(2) As of the effective date of this AD, do not install any
governor controller P/N D270-1, Revision A through E inclusive, on
any helicopter.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, West 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 West Certification Branch, send it to
the attention of the person identified in paragraph (i) of this AD.
Information may be emailed to: [email protected].
(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.
(i) Additional Information
For more information about this AD, contact Eric Moreland,
Aviation Safety Engineer, FAA, 3960 Paramount Boulevard, Lakewood,
CA 90712; phone: (562) 627-5364; email: [email protected].
(j) 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) Robinson Helicopter Company R22 Service Bulletin SB-121,
dated June 28, 2023.
(ii) Robinson Helicopter Company R44 Service Bulletin SB-114,
dated June 28, 2023.
(3) For Robinson Helicopter Company service information, contact
Robinson Helicopter Company, Technical Support Department, 2901
Airport Drive, Torrance, CA 90505; phone (310) 539-0508; fax (310)
539-5198; email robinsonheli.com">ts1@robinsonheli.com; or at robinsonheli.com.
(4) You may view this service information at the FAA, Office of
the Regional Counsel, Southwest Region, 10101 Hillwood Parkway, 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 material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on July 10, 2024.
James D. Foltz,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-15707 Filed 7-16-24; 8:45 am]
BILLING CODE 4910-13-P