Airworthiness Directives; Bombardier, Inc., Airplanes, 2029-2032 [2023-00062]
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2029
Proposed Rules
Federal Register
Vol. 88, No. 8
Thursday, January 12, 2023
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF ENERGY
10 CFR Part 1021
Request for Information Regarding
Categorical Exclusions
Department of Energy.
Request for information; reopening of public comment period.
AGENCY:
ACTION:
On November 15, 2022, the
U.S. Department of Energy (DOE)
published a request for information to
help inform potential updates to
categorical exclusions in its regulations
implementing the National
Environmental Policy Act (NEPA).
Through the request for information,
DOE sought recommendations and
supporting information from interested
individuals and organizations on
establishing new categorical exclusions
and revising existing ones. In response
to public request, DOE is re-opening the
comment period for 30 days to allow
interested parties additional time to
provide input.
DATES: The comment period for the
request for information, published on
November 15, 2022 (87 FR 68385),
which closed on December 30, 2022, is
hereby reopened. Responses should be
submitted by February 13, 2023.
ADDRESSES: Submit comments, labeled
‘‘DOE NEPA RFI,’’ via https://
www.regulations.gov. This request for
information is assigned Docket ID:
DOE–HQ–2023–0002. Follow the online
instructions for submitting comments
electronically. Alternatively, responses
to this request for information may be
submitted by email to doe-neparulemaking@hq.doe.gov. There is no
need to submit comments using both
methods.
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SUMMARY:
For
further information on submitting
responses, contact Carrie Abravanel,
Office of NEPA Policy and Compliance
(GC–54), 202–586–8397,
Carrie.Abravanel@hq.doe.gov.
SUPPLEMENTARY INFORMATION: DOE
published a request for information on
FOR FURTHER INFORMATION CONTACT:
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17:11 Jan 11, 2023
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November 15, 2022 (87 FR 68385) that
started a 45-day comment period
(ending December 30, 2022). DOE is
considering revisions to ensure that its
NEPA reviews are aligned with the
latest DOE programs and initiatives for
clean energy and electricity
transmission projects, fully consider
potential environmental impacts and
community concerns, and are efficient
and effective at informing DOE
decisions. In the request for
information, DOE sought
recommendations and supporting
information from interested individuals
and organizations on establishing new
categorical exclusions and revising
existing ones. Through the request for
information, interested parties were
invited to:
• Identify a specific category of
actions related to clean energy projects
and clean energy infrastructure that is
not covered by existing DOE categorical
exclusions, but that is likely to meet the
standard of not having a significant
effect on the human environment; and
• Provide suggestions for revising
DOE’s existing categorical exclusions
related to clean energy projects and
clean energy infrastructure.
In response to public request, DOE
has determined that re-opening the
public comment period is appropriate to
allow interested parties additional time
to submit comments for DOE’s
consideration. Therefore, DOE is reopening the comment period for an
additional 30 days. Please see the
November 15, 2022, request for
information for additional background
information and instructions on
providing comments. That request for
information is available at https://
www.energy.gov/nepa/articles/requestinformation-regarding-categoricalexclusions-2022.
How should information be provided?
Responses should be submitted to
doe-nepa-rulemaking@hq.doe.gov by
February 13, 2023. Submitted
information will be included in the
public record of any associated
rulemaking, should DOE decide to
undertake revisions to its NEPA
regulations.
Confidential Business Information:
Pursuant to 10 CFR 1004.11, any person
submitting information that he or she
believes to be confidential and exempt
by law from public disclosure should
submit via email two well-marked
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copies: one copy of the document
marked ‘‘confidential’’ including all the
information believed to be confidential,
and one copy of the document marked
‘‘non-confidential’’ with the information
believed to be confidential deleted.
Submit these documents via email. DOE
will make its own determination about
the confidential status of the
information and treat it according to its
determination.
Signing Authority
This document of the Department of
Energy was signed on January 6, 2023,
by Samuel Walsh, General Counsel,
pursuant to delegated authority from the
Secretary of Energy. That document
with the original signature and date is
maintained by DOE. For administrative
purposes only, and in compliance with
requirements of the Office of the Federal
Register, the undersigned DOE Federal
Register Liaison Officer has been
authorized to sign and submit the
document in electronic format for
publication, as an official document of
the Department of Energy. This
administrative process in no way alters
the legal effect of this document upon
publication in the Federal Register.
Signed in Washington, DC, January 6,
2023.
Treena V. Garrett,
Federal Register Liaison Officer, U.S.
Department of Energy.
[FR Doc. 2023–00430 Filed 1–11–23; 8:45 am]
BILLING CODE 6450–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1662; Project
Identifier MCAI–2022–00689–T]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD–
100–1A10 airplanes. This proposed AD
was prompted by multiple reports of
SUMMARY:
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Federal Register / Vol. 88, No. 8 / Thursday, January 12, 2023 / Proposed Rules
erratic electrical system status on the
push button annunciators (PBAs) and
the engine instrument and crew alerting
system (EICAS) while on-ground and
during flight. This proposed AD would
require a records check and replacement
of affected left-hand (LH) direct current
power center (DCPC) units. 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 February 27,
2023.
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–2022–1662; 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 Bombardier service information
identified in this NPRM, contact
Bombardier Business Aircraft Customer
Response Center, 400 Coˆte-Vertu Road
West, Dorval, Que´bec H4S 1Y9, Canada;
telephone 514–855–2999; email ac.yul@
aero.bombardier.com; website
bombardier.com.
• You may view this service
information 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:
Steven Dzierzynski, Aerospace
Engineer, Avionics & Electrical Systems
Section, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7367; email 9-avs-nyaco-cos@
faa.gov.
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ADDRESSES:
SUPPLEMENTARY INFORMATION:
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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–2022–1662; Project Identifier
MCAI–2022–00689–T’’ 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 the 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 Steven Dzierzynski,
Aerospace Engineer, Avionics &
Electrical Systems Section, FAA, New
York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7367; email
9-avs-nyaco-cos@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
Transport Canada, which is the
aviation authority for Canada, has
issued Transport Canada AD CF–2022–
28, dated June 9, 2022 (Transport
Canada AD CF–2022–28) (also referred
to after this as the MCAI), to correct an
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unsafe condition on certain Bombardier,
Inc., Model BD–100–1A10 airplanes.
The MCAI states there have been
multiple reports of erratic electrical
system status on the PBAs and the
EICAS while on-ground and during
flight, and in several cases, leading to
momentary loss of electrical power and
loss of flight displays following flight
crew responses to the erratic statuses. It
was found that airplanes could
experience misleading electrical system
status indications (PBA and EICAS) as
a result of contamination of electrical
contacts in the LH DCPC internal
communication data bus. Those erratic
indications could cause the crew to turn
off fully-operational electrical power
sources, leading to partial or complete
loss of electrical power. Loss of
electrical power could result in the loss
of flight displays and reduced
controllability of the airplane.
The MCAI also stated that Transport
Canada previously issued CF–2020–46,
dated November 17, 2020 (which
corresponds to FAA AD 2021–23–14,
Amendment 39–21812 (86 FR 68889,
December 6, 2021)), which mandated
the use of revised Electrical Emergency
and Non-Normal Procedures in the
airplane flight manual that directed
crews not to turn off active generators in
the event of an erroneous electrical
system status indication. The MCAI
advised that further corrective action is
being developed to introduce a design
improvement to the DCPC that is
intended to protect the internal
communication data bus from
contaminants, and that a time-limited
maintenance check will also be
implemented.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2022–1662.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Bombardier
Service Bulletins 100–24–29 and 350–
24–004, both dated April 9, 2021. This
service information specifies procedures
for a records check to determine the
total flight hours and replacement of
affected LH DCPC units (part numbers
975GC02Y04, 975GC0Y05,
975GC02Y06, or 975GC02Y07). These
documents are distinct since they apply
to different airplane configurations. 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.
FAA’s Determination
This product has been approved by
the aviation authority of another
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Federal Register / Vol. 88, No. 8 / Thursday, January 12, 2023 / Proposed Rules
country, and is approved for operation
in the United States. Pursuant to the
FAA’s bilateral agreement with this
State of Design Authority, it has notified
the FAA of the unsafe condition
described in the MCAI and service
information described above. 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.
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
the service information already
described, except as discussed under
‘‘Differences Between this NPRM and
the MCAI or Service Information.’’
Differences Between This NPRM and
the MCAI or Service Information
The note to paragraph 2.B.(4) in
Bombardier Service Bulletins 100–24–
29 and 350–24–004, both dated April 9,
2021, specifies to reset the unit total
flight hours to zero at date of
incorporation. This proposed AD would
not require that action.
Interim Action
The FAA considers that this proposed
AD would be an interim action. The
MCAI states that further corrective
action is being developed. Once this
action is developed, approved, and
available, the FAA might consider
additional rulemaking.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 315
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
1 work-hours × $85 per hour = $85 ............................................................................................
$0
$85
$26,775
The FAA estimates the following
costs to do any necessary on-condition
actions that would be required based on
the results of any required actions. The
FAA has no way of determining the
number of aircraft that might need this
on-condition action:
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
8 work-hours × $85 per hour = $680 ....................................................................................................................
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The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some or all
of the costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
operators.
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.
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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,
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Frm 00003
Cost per
product
Parts cost
Fmt 4702
Sfmt 4702
Up to $35,000
Up to $35,680.
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:
■
Bombardier, Inc.: Docket No. FAA–2022–
1662; Project Identifier MCAI–2022–
00689–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by February 27,
2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc.,
Model BD–100–1A10 airplanes, certificated
in any category, having serial number 20003
through 20795 inclusive, 20797 through
20812 inclusive, 20814 through 20832
inclusive, and 20834 through 20836
inclusive.
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Federal Register / Vol. 88, No. 8 / Thursday, January 12, 2023 / Proposed Rules
(d) Subject
Air Transport Association (ATA) of
America Code 24, Electrical Power.
(e) Unsafe Condition
This AD was prompted by multiple reports
of erratic electrical system status on the push
button annunciators (PBAs) and the engine
instrument and crew alerting system (EICAS)
while on-ground and during flight. The FAA
is issuing this AD to address erratic
indications, which could cause the flight
crew to turn off fully-operational electrical
power sources, leading to partial or complete
loss of electrical power. The unsafe
condition, if not addressed, could result in
loss of electrical power could result in the
loss of flight displays and reduced
controllability of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Records Check
Within 60 days after the effective date of
this AD, verify the total flight hours of the
left-hand (LH) direct current power center
(DCPC) unit since the date of manufacture by
doing a records check in accordance with
paragraph 2.B.(1) of the Accomplishment
Instructions of the applicable service bulletin
identified in paragraphs (g)(1) and (2) of this
AD.
(1) For airplanes having serial number
20001 through 20500 inclusive, use
Bombardier Service Bulletin 100–24–29,
dated April 9, 2021.
(2) For airplanes having serial number
20501 through 20999 inclusive, use
Bombardier Service Bulletin 350–24–004,
dated April 9, 2021.
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(h) Replacement of the LH DCPC
If, during the records check required by
paragraph (g) of this AD, the total flight hours
since date of manufacture of the LH DCPC
unit is equal to or more than 3,100 total flight
hours and the LH DCPC has not been cleaned
as specified in Safran Service Bulletin
975GC02Y–24–018 before the effective date
of this AD: Within 19 months after the
effective date of this AD, replace the LH
DCPC unit in accordance with paragraphs
2.B.(2) through 2.B.(5) and 2.C. of the
Accomplishment Instructions of the
applicable service bulletin identified in
paragraphs (g)(1) and (2) of this AD.
(i) Exception to the Service Information
Although the note in paragraph 2.B.(4) of
the Accomplishment Instructions of
Bombardier Service Bulletins 100–24–29,
and 350–24–004, both dated April 9, 2021,
specifies that actions will reset ‘‘the unit total
flight hours to zero at date of incorporation,’’
this AD does not include that requirement.
(j) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York ACO
Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In
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17:11 Jan 11, 2023
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accordance with 14 CFR 39.19, send your
request to your principal inspector or
responsible Flight Standards Office, as
appropriate. If sending information directly
to the manager of the New York ACO Branch,
mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address
identified in paragraph (k)(1) of this AD or
email to: 9-avs-nyaco-cos@faa.gov. If mailing
information, also submit information by
email. Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, New York ACO Branch,
FAA; or Transport Canada; or Bombardier,
Inc.’s Transport Canada Design Approval
Organization (DAO). If approved by the DAO,
the approval must include the DAOauthorized signature.
(k) Additional Information
(1) Refer to Transport Canada AD CF–
2022–28, dated May 26, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2022–1662.
(2) For more information about this AD,
contact Steven Dzierzynski, Aerospace
Engineer, Avionics & Electrical Systems
Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7367; email 9-avsnyaco-cos@faa.gov.
(l) 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 this AD specifies otherwise.
(i) Bombardier Service Bulletin 100–24–29,
dated April 9, 2021.
(ii) Bombardier Service Bulletin 350–24–
004, dated April 9, 2021.
(3) For Bombardier service information
identified in this AD, contact Bombardier
Business Aircraft Customer Response Center,
400 Coˆte-Vertu Road West, Dorval, Que´bec
H4S 1Y9, Canada; telephone 514–855–2999;
email ac.yul@aero.bombardier.com; website
bombardier.com.
(4) You may view this service information
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 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 fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
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Issued on January 2, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–00062 Filed 1–11–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1659; Project
Identifier MCAI–2022–01254–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 adopt a
new airworthiness directive (AD) for
certain Airbus SAS Model A350–941
and –1041 airplanes. This proposed AD
was prompted by reports of broken
lower attachment studs on the AFT
galley complex. This proposed AD
would require repetitive detailed
inspections of the lower attachment
studs and, depending on findings,
replacement of the lower attachment
studs, as specified in a European Union
Aviation Safety Agency (EASA) AD,
which is proposed for incorporation by
reference (IBR). 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 February 27,
2023.
SUMMARY:
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–2022–1659; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
ADDRESSES:
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Agencies
[Federal Register Volume 88, Number 8 (Thursday, January 12, 2023)]
[Proposed Rules]
[Pages 2029-2032]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-00062]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1662; Project Identifier MCAI-2022-00689-T]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier, Inc., Model BD-100-1A10 airplanes. This
proposed AD was prompted by multiple reports of
[[Page 2030]]
erratic electrical system status on the push button annunciators (PBAs)
and the engine instrument and crew alerting system (EICAS) while on-
ground and during flight. This proposed AD would require a records
check and replacement of affected left-hand (LH) direct current power
center (DCPC) units. 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 February
27, 2023.
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-2022-1662; 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 Bombardier service information identified in this
NPRM, contact Bombardier Business Aircraft Customer Response Center,
400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">[email protected]bombardier.com; website
bombardier.com.
You may view this service information 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: Steven Dzierzynski, Aerospace
Engineer, Avionics & Electrical Systems Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7367; 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-2022-1662; Project Identifier
MCAI-2022-00689-T'' 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
the 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
Steven Dzierzynski, Aerospace Engineer, Avionics & Electrical Systems
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7367; 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
Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada AD CF-2022-28, dated June 9, 2022 (Transport
Canada AD CF-2022-28) (also referred to after this as the MCAI), to
correct an unsafe condition on certain Bombardier, Inc., Model BD-100-
1A10 airplanes. The MCAI states there have been multiple reports of
erratic electrical system status on the PBAs and the EICAS while on-
ground and during flight, and in several cases, leading to momentary
loss of electrical power and loss of flight displays following flight
crew responses to the erratic statuses. It was found that airplanes
could experience misleading electrical system status indications (PBA
and EICAS) as a result of contamination of electrical contacts in the
LH DCPC internal communication data bus. Those erratic indications
could cause the crew to turn off fully-operational electrical power
sources, leading to partial or complete loss of electrical power. Loss
of electrical power could result in the loss of flight displays and
reduced controllability of the airplane.
The MCAI also stated that Transport Canada previously issued CF-
2020-46, dated November 17, 2020 (which corresponds to FAA AD 2021-23-
14, Amendment 39-21812 (86 FR 68889, December 6, 2021)), which mandated
the use of revised Electrical Emergency and Non-Normal Procedures in
the airplane flight manual that directed crews not to turn off active
generators in the event of an erroneous electrical system status
indication. The MCAI advised that further corrective action is being
developed to introduce a design improvement to the DCPC that is
intended to protect the internal communication data bus from
contaminants, and that a time-limited maintenance check will also be
implemented.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1662.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Bombardier Service Bulletins 100-24-29 and 350-24-
004, both dated April 9, 2021. This service information specifies
procedures for a records check to determine the total flight hours and
replacement of affected LH DCPC units (part numbers 975GC02Y04,
975GC0Y05, 975GC02Y06, or 975GC02Y07). These documents are distinct
since they apply to different airplane configurations. 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.
FAA's Determination
This product has been approved by the aviation authority of another
[[Page 2031]]
country, and is approved for operation in the United States. Pursuant
to the FAA's bilateral agreement with this State of Design Authority,
it has notified the FAA of the unsafe condition described in the MCAI
and service information described above. 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.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the service information already described, except as discussed under
``Differences Between this NPRM and the MCAI or Service Information.''
Differences Between This NPRM and the MCAI or Service Information
The note to paragraph 2.B.(4) in Bombardier Service Bulletins 100-
24-29 and 350-24-004, both dated April 9, 2021, specifies to reset the
unit total flight hours to zero at date of incorporation. This proposed
AD would not require that action.
Interim Action
The FAA considers that this proposed AD would be an interim action.
The MCAI states that further corrective action is being developed. Once
this action is developed, approved, and available, the FAA might
consider additional rulemaking.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 315 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hours x $85 per hour = $85............................ $0 $85 $26,775
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need this on-condition action:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
8 work-hours x $85 per hour = Up to $35,000...... Up to $35,680.
$680.
------------------------------------------------------------------------
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed AD may be covered under warranty, thereby reducing the
cost impact on affected operators.
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:
Bombardier, Inc.: Docket No. FAA-2022-1662; Project Identifier MCAI-
2022-00689-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 27, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-100-1A10
airplanes, certificated in any category, having serial number 20003
through 20795 inclusive, 20797 through 20812 inclusive, 20814
through 20832 inclusive, and 20834 through 20836 inclusive.
[[Page 2032]]
(d) Subject
Air Transport Association (ATA) of America Code 24, Electrical
Power.
(e) Unsafe Condition
This AD was prompted by multiple reports of erratic electrical
system status on the push button annunciators (PBAs) and the engine
instrument and crew alerting system (EICAS) while on-ground and
during flight. The FAA is issuing this AD to address erratic
indications, which could cause the flight crew to turn off fully-
operational electrical power sources, leading to partial or complete
loss of electrical power. The unsafe condition, if not addressed,
could result in loss of electrical power could result in the loss of
flight displays and reduced controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Records Check
Within 60 days after the effective date of this AD, verify the
total flight hours of the left-hand (LH) direct current power center
(DCPC) unit since the date of manufacture by doing a records check
in accordance with paragraph 2.B.(1) of the Accomplishment
Instructions of the applicable service bulletin identified in
paragraphs (g)(1) and (2) of this AD.
(1) For airplanes having serial number 20001 through 20500
inclusive, use Bombardier Service Bulletin 100-24-29, dated April 9,
2021.
(2) For airplanes having serial number 20501 through 20999
inclusive, use Bombardier Service Bulletin 350-24-004, dated April
9, 2021.
(h) Replacement of the LH DCPC
If, during the records check required by paragraph (g) of this
AD, the total flight hours since date of manufacture of the LH DCPC
unit is equal to or more than 3,100 total flight hours and the LH
DCPC has not been cleaned as specified in Safran Service Bulletin
975GC02Y-24-018 before the effective date of this AD: Within 19
months after the effective date of this AD, replace the LH DCPC unit
in accordance with paragraphs 2.B.(2) through 2.B.(5) and 2.C. of
the Accomplishment Instructions of the applicable service bulletin
identified in paragraphs (g)(1) and (2) of this AD.
(i) Exception to the Service Information
Although the note in paragraph 2.B.(4) of the Accomplishment
Instructions of Bombardier Service Bulletins 100-24-29, and 350-24-
004, both dated April 9, 2021, specifies that actions will reset
``the unit total flight hours to zero at date of incorporation,''
this AD does not include that requirement.
(j) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York 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 responsible Flight Standards Office, as appropriate. If
sending information directly to the manager of the New York ACO
Branch, mail it to ATTN: Program Manager, Continuing Operational
Safety, at the address identified in paragraph (k)(1) of this AD or
email to: [email protected]. If mailing information, also
submit information by email. Before using any approved AMOC, notify
your appropriate principal inspector, or lacking a principal
inspector, the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada; or Bombardier, Inc.'s Transport
Canada Design Approval Organization (DAO). If approved by the DAO,
the approval must include the DAO-authorized signature.
(k) Additional Information
(1) Refer to Transport Canada AD CF-2022-28, dated May 26, 2022,
for related information. This Transport Canada AD may be found in
the AD docket at regulations.gov under Docket No. FAA-2022-1662.
(2) For more information about this AD, contact Steven
Dzierzynski, Aerospace Engineer, Avionics & Electrical Systems
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7367; email [email protected].
(l) 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 this AD specifies otherwise.
(i) Bombardier Service Bulletin 100-24-29, dated April 9, 2021.
(ii) Bombardier Service Bulletin 350-24-004, dated April 9,
2021.
(3) For Bombardier service information identified in this AD,
contact Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">[email protected]bombardier.com; website
bombardier.com.
(4) You may view this service information 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 service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on January 2, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-00062 Filed 1-11-23; 8:45 am]
BILLING CODE 4910-13-P