Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 46336-46339 [2024-11005]
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lotter on DSK11XQN23PROD with PROPOSALS1
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Federal Register / Vol. 89, No. 104 / Wednesday, May 29, 2024 / Proposed Rules
time between protocol publication and
first credit generation)?
Question 4: Which protocol(s) for
generating voluntary carbon credits
from agriculture and forestry projects
should USDA evaluate for listing
through the Greenhouse Gas Technical
Assistance Provider and Third-Party
Verifier Program?
Question 5: For any protocol(s)
identified under Question 4:
(a) Has the protocol resulted in the
generation and sale of credits? If yes,
when was the most recent year and
volume of credit generation and
retirement? If not, is there evidence that
the protocol will generate credits (e.g.,
projects are under development)?
(b) What is the average size (in acres,
hectares, or another relevant unit) of
projects using the protocol?
(c) What is the average credit issuance
per unit land area (acre or hectare) for
projects using the protocol, inclusive of
credits that are contributed to a buffer
pool?
(d) Does the protocol reduce the cost,
paperwork, and/or reporting burden for
smaller, diversified, or underserved
farmers, ranchers, or private forest
landowners, while maintaining
reliability of offsets? If yes, how?
(e) Does the protocol allow multiple
entities to aggregate into a single
project? If yes, what are the parameters
for aggregation and is there evidence
that aggregation has successfully
occurred?
(f) Does the registry administering the
protocol use a fee structure that allows
for aggregated entities to pay a single
project fee, or does each entity need to
pay a project fee?
(g) What are the verification
requirements in the protocol, including
recordkeeping requirements?
(h) Does the protocol require on-site
verification? If yes, does the protocol
require 100% on-site verification, or
does the protocol specify a procedure
for determining an on-site verification
sample group? What is required as part
of the on-site verification? Does the
protocol allow remote verification
methods/technologies (e.g., remote
sensing)?
(i) Does the protocol include a risk
management approach for determining
which data inputs or project sites are
required for third-party verification? If
yes, what does the risk management
approach require?
(j) Does the protocol allow for
simplified measurement, monitoring,
reporting, and verification (MMRV)
processes? If yes, are there requirements
or restrictions for using the simplified
MMRV processes?
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(k) What quantification
methodology(ies) does the protocol
require for quantification of emissions
reductions and/or removals? What
scientific evidence is available to
support these methodologies?
(l) For protocols where models are
required to quantify emissions, is there
a process for model review and approval
prior to use by prospective projects? Can
approved models be used by any project
or are they specific to a project
developer?
(m) If models are allowed for
quantification of emissions reductions,
are models required to have gone
through scientific review,
parameterization, calibration, and
validation to demonstrate performance
for the practices on the relevant crops
and/or species in the geography of the
project? Does the protocol provide clear
guidance on where eligible models can
be applied?
(n) What does the protocol require or
allow for determining a project
baseline?
(o) How does the registry
administering the protocol restrict the
potential double counting of credits?
(p) Does the protocol require projects
to quantify and report uncertainty
associated with greenhouse gas
calculations?
(q) Has the protocol generated credits
which were later cancelled due to issues
of credit integrity or validity?
(r) For project categories where
reversals (i.e., the intentional or
unintentional release of sequestered
carbon for which credits have been
issued) are possible, does the protocol
contain procedures to maintain net GHG
impact?
(s) Where is information about the
protocol made publicly available?
Question 6: How should USDA
evaluate technical assistance providers
(TAP)? What should be the minimum
qualifications, certifications, and/or
expertise for a TAP to qualify for listing
under the Program?
Question 7: Should the qualifications
and/or registration process be different
for entities and individuals that seek to
register as a TAP?
Questions 8: What should be the
minimum qualifications and expertise
for a third-party verifier to qualify for
registration under the Program?
(Authority: Pub. L. 117–328, div. HH, title I,
section 201)
Melissa Bailey,
Associate Administrator, Agricultural
Marketing Service.
[FR Doc. 2024–11424 Filed 5–28–24; 8:45 am]
BILLING CODE P
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1470; Project
Identifier MCAI–2023–01284–T]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by 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 MHI RJ Aviation ULC Model
CL–600–2C10 (Regional Jet Series 700,
701 & 702), CL–600–2D15 (Regional Jet
Series 705), and CL–600–2D24 (Regional
Jet Series 900) airplanes. This proposed
AD was prompted by a report that the
electrical harnesses in the overhead bin
above the class divider may have
insufficient or no separation with the
class divider mounting plate. This
proposed AD would require inspecting
the overhead bin electrical harnesses at
the class dividers, and modifying the
class divider mounting plate assembly
or accomplishing a temporary repair if
necessary; and, eventually modifying
the class divider mounting plate
assembly if a modification was not done
after accomplishing the inspection, as
specified in a Transport Canada 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 July 15, 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–2024–1470; or in person at
Docket Operations between 9 a.m. and
SUMMARY:
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Federal Register / Vol. 89, No. 104 / Wednesday, May 29, 2024 / Proposed Rules
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 Transport Canada material,
contact Transport Canada, Transport
Canada National Aircraft Certification,
159 Cleopatra Drive, Nepean, Ontario
K1A 0N5, Canada; telephone 888–663–
3639; email TC.AirworthinessDirectivesConsignesdenavigabilite.TC@tc.gc.ca.
You may find this material on the
Transport Canada website tc.canada.ca/
en/aviation.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 2200 South 216th Street, Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
Fatin Saumik, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; email: 9-avs-nyaco-cos@
faa.gov.
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–2024–1470; Project Identifier
MCAI–2023–01284–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
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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 Fatin Saumik,
Aviation Safety Engineer, FAA, 1600
Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516–228–7300;
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–2023–
79, dated December 21, 2023 (Transport
Canada AD CF–2023–79) (also referred
to after this as the MCAI), to correct an
unsafe condition on certain MHI RJ
Aviation ULC Model CL–600–2C10
(Regional Jet Series 700, 701 & 702), CL–
600–2D15 (Regional Jet Series 705), and
CL–600–2D24 (Regional Jet Series 900)
airplanes. The MCAI states that the
electrical harnesses in the overhead bin
above the class divider may have
insufficient or no separation with the
class divider mounting plate. This
condition, if not corrected, could result
in the electrical harnesses becoming
chafed, which could affect the following
aircraft systems: ordinance signs,
emergency lights/signs, passenger
oxygen, and passenger address and air
conditioning systems.
The FAA is proposing this AD to
address the unsafe condition on these
products.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2024–1470.
Related Service Information Under 1
CFR Part 51
Transport Canada AD CF–2023–79
specifies procedures for inspecting the
left-hand and right-hand overhead bin
electrical harnesses at the class divider
for damage (e.g., chafing), and if damage
is found, modifying the class divider
mounting plate assembly to improve the
overhead bin harnesses protection or
accomplishing a temporary repair.
Transport Canada AD CF–2023–79 also
specifies procedures for eventually
modifying the class divider mounting
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46337
plate assembly if a modification was not
done after accomplishing the inspection
(i.e., if a temporary repair was done or
if no damage was found after
accomplishing the inspection). This
material 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
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 referenced 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 Transport Canada AD CF–2023–79
described previously, except for any
differences identified as exceptions in
the regulatory text of this proposed AD.
Explanation of Required Compliance
Information
In the FAA’s ongoing efforts to
improve the efficiency of the AD
process, the FAA developed a process to
use some civil aviation authority (CAA)
ADs as the primary source of
information for compliance with
requirements for corresponding FAA
ADs. The FAA has been coordinating
this process with manufacturers and
CAAs. As a result, the FAA proposes to
incorporate Transport Canada AD CF–
2023–79 by reference in the FAA final
rule. This proposed AD would,
therefore, require compliance with
Transport Canada AD CF–2023–79 in its
entirety through that incorporation,
except for any differences identified as
exceptions in the regulatory text of this
proposed AD. Service information
required by Transport Canada AD CF–
2023–79 for compliance will be
available at regulations.gov under
Docket No. FAA–2024–1470 after the
FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 246
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
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Federal Register / Vol. 89, No. 104 / Wednesday, May 29, 2024 / Proposed Rules
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
3 work-hours × $85 per hour = $255 ..........................................
Up to 9 work-hours × $85 per hour = $765 ................................
The FAA estimates the following
costs to do any necessary on-condition
actions that would be required based on
$0
366
Cost per product
Cost on U.S. operators
$255 ...................
Up to 1,131 ........
the results of any required actions. The
FAA has no way of determining the
$62,730.
Up to 278,226.
number of aircraft that might need these
on-condition actions:
ESTIMATED COSTS OF ON-CONDITION ACTIONS *
Labor cost
Parts cost
Up to 9 work-hours × $85 per hour = $765 ....................................................................
$366
Cost per product
Up to $1,131.
* The FAA has received no definitive data on which to base the cost estimates for the on-condition optional temporary repair specified in this
proposed AD.
Authority for This Rulemaking
List of Subjects in 14 CFR Part 39
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.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
lotter on DSK11XQN23PROD with PROPOSALS1
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.
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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:
■
MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.):
Docket No. FAA–2024–1470; Project
Identifier MCAI–2023–01284–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by July 15, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC
(type certificate previously held by
Bombardier, Inc.) Model CL–600–2C10
(Regional Jet Series 700, 701 & 702), CL–600–
2D15 (Regional Jet Series 705), and CL–600–
2D24 (Regional Jet Series 900) airplanes,
certificated in any category, as identified in
Transport Canada AD CF–2023–79, dated
December 21, 2023 (Transport Canada AD
CF–2023–79), except for Group 3 and Group
5 airplanes identified Transport Canada AD
CF–2023–79.
Note 1 to paragraph (c): Group 3 airplanes
that are modified as specified in Service
Bulletin 670BA–25–110 become Group 2
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airplanes as identified in Transport Canada
AD CF–2023–79.
Note 2 to paragraph (c): Group 5 airplanes
that are modified as specified in Service
Bulletin 670BA–25–057 become Group 4
airplanes as identified in Transport Canada
AD CF–2023–79.
(d) Subject
Air Transport Association (ATA) of
America Code 25, Equipment/furnishings.
(e) Unsafe Condition
This AD was prompted by a report that the
electrical harnesses in the overhead bin
above the class divider may have insufficient
or no separation with the class divider
mounting plate. The FAA is issuing this AD
to address possible chafing of the electrical
harness with the class divider mounting
plate. The unsafe condition, if not addressed,
could result in the electrical harnesses
becoming chafed, which could affect the
following aircraft systems: ordinance signs,
emergency lights/signs, passenger oxygen,
and passenger address and air conditioning
systems.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Requirements
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, Transport Canada AD CF–
2023–79.
(h) Exception To Transport Canada AD CF–
2023–79
(1) Where Transport Canada AD CF–2023–
79 refers to its effective date or August 7,
2023 (the effective date of Transport Canada
AD CF–2023–56, dated July 24, 2023), this
AD requires using the effective date of this
AD.
(2) Where Transport Canada AD CF–2023–
79 refers to hours air time, this AD requires
using flight hours.
(3) Where paragraph A. of Part I of
Transport Canada AD CF–2023–79, specifies
‘‘and, modify as required,’’ for this AD,
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replace that text with ‘‘and, before further
flight, modify as required.’’
(4) Where any MHIRJ service information
referenced in Transport Canada AD CF–
2023–79 differs from any Safran service
information referenced in Transport Canada
AD CF–2023–79, the MHIRJ service
information takes precedence over the Safran
service information because the initial
revision of the Safran service information
does not list all affected part numbers.
(i) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Validation 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 International Validation
Branch, mail it to the address identified in
paragraph (j) of this AD. Information may be
emailed to: 9-AVS-NYACO-COS@faa.gov.
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, International Validation
Branch, FAA; or Transport Canada; or MHI
RJ Aviation ULC’s Transport Canada Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
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(j) Additional Information
For more information about this AD,
contact Fatin Saumik, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516–
228–7300; email: 9-avs-nyaco-cos@faa.gov.
(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 this AD specifies otherwise.
(i) Transport Canada AD CF–2023–79,
dated December 21, 2023.
(ii) [Reserved]
(3) Transport Canada AD CF–2023–79,
contact Transport Canada, Transport Canada
National Aircraft Certification, 159 Cleopatra
Drive, Nepean, Ontario K1A 0N5, Canada;
telephone 888–663–3639; email
TC.AirworthinessDirectivesConsignesdenavigabilite.TC@tc.gc.ca. You
may find this Transport Canada AD on the
Transport Canada website tc.canada.ca/en/
aviation.
(4) You may view this material at the FAA,
Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th Street, Des
Moines, WA. For information on the
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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-locations, or email fr.inspection@
nara.gov.
Issued on May 15, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–11005 Filed 5–28–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2024–1556; Airspace
Docket No. 24–ASW–12]
RIN 2120–AA66
Establishment of Class E Airspace;
Langtry, TX
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
establish Class E airspace at Langtry,
TX. The FAA is proposing this action to
support new instrument procedures at
this airport.
DATES: Comments must be received on
or before July 15, 2024.
ADDRESSES: Send comments identified
by FAA Docket No. FAA–2024–1556
and Airspace Docket No. 24–ASW–12
using any of the following methods:
Federal eRulemaking Portal: Go to
www.regulations.gov and follow the
online instruction for sending your
comments electronically.
Mail: Send comments to Docket
Operations, M–30; U.S. Department of
Transportation, 1200 New Jersey
Avenue SE, Room W12–140, West
Building Ground Floor, Washington, DC
20590–0001.
Hand Delivery or Courier: Take
comments to Docket Operations in
Room W12–140 of the West Building
Ground Floor at 1200 New Jersey
Avenue SE, Washington, DC, between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays.
Fax: Fax comments to Docket
Operations at (202) 493–2251.
Docket: Background documents or
comments received may be read at
www.regulations.gov at any time.
Follow the online instructions for
accessing the docket or go to Docket
SUMMARY:
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46339
Operations in Room W12–140 of the
West Building Ground Floor at 1200
New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FAA Order JO 7400.11H, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at www.faa.gov/air_traffic/
publications/. You may also contact the
Rules and Regulations Group, Office of
Policy, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783.
FOR FURTHER INFORMATION CONTACT: Raul
Garza Jr., Federal Aviation
Administration, Operations Support
Group, Central Service Center, 10101
Hillwood Parkway, Fort Worth, TX
76177; telephone (817) 222–5874.
SUPPLEMENTARY INFORMATION:
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it would
establish Class E airspace extending
upward from 700 feet above the surface
at 4M Ranch Airfield, Langtry, TX, to
support instrument flight rule (IFR)
operations at this airport.
Comments Invited
The FAA invites interested persons to
participate in this rulemaking by
submitting written comments, data, or
views. Comments are specifically
invited on the overall regulatory,
aeronautical, economic, environmental,
and energy-related aspects of the
proposal. The most helpful comments
reference a specific portion of the
proposal, explain the reason for any
recommended change, and include
supporting data. To ensure the docket
does not contain duplicate comments,
commenters should submit only one
time if comments are filed
electronically, or commenters should
send only one copy of written
comments if comments are filed in
writing.
The FAA will file in the docket all
comments it receives, as well as a report
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Agencies
[Federal Register Volume 89, Number 104 (Wednesday, May 29, 2024)]
[Proposed Rules]
[Pages 46336-46339]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-11005]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1470; Project Identifier MCAI-2023-01284-T]
RIN 2120-AA64
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain MHI RJ Aviation ULC Model CL-600-2C10 (Regional Jet Series
700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24
(Regional Jet Series 900) airplanes. This proposed AD was prompted by a
report that the electrical harnesses in the overhead bin above the
class divider may have insufficient or no separation with the class
divider mounting plate. This proposed AD would require inspecting the
overhead bin electrical harnesses at the class dividers, and modifying
the class divider mounting plate assembly or accomplishing a temporary
repair if necessary; and, eventually modifying the class divider
mounting plate assembly if a modification was not done after
accomplishing the inspection, as specified in a Transport Canada 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 July 15,
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-2024-1470; or in person at Docket Operations between 9
a.m. and
[[Page 46337]]
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 Transport Canada material, contact Transport Canada,
Transport Canada National Aircraft Certification, 159 Cleopatra Drive,
Nepean, Ontario K1A 0N5, Canada; telephone 888-663-3639; email
[email protected]. You may
find this material on the Transport Canada website tc.canada.ca/en/
aviation.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For information on the availability of
this material at the FAA, call 206-231-3195.
FOR FURTHER INFORMATION CONTACT: Fatin Saumik, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; 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-2024-1470; Project Identifier
MCAI-2023-01284-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 Fatin
Saumik, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; 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-2023-79, dated December 21, 2023
(Transport Canada AD CF-2023-79) (also referred to after this as the
MCAI), to correct an unsafe condition on certain MHI RJ Aviation ULC
Model CL-600-2C10 (Regional Jet Series 700, 701 & 702), CL-600-2D15
(Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900)
airplanes. The MCAI states that the electrical harnesses in the
overhead bin above the class divider may have insufficient or no
separation with the class divider mounting plate. This condition, if
not corrected, could result in the electrical harnesses becoming
chafed, which could affect the following aircraft systems: ordinance
signs, emergency lights/signs, passenger oxygen, and passenger address
and air conditioning systems.
The FAA is proposing this AD to address the unsafe condition on
these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-1470.
Related Service Information Under 1 CFR Part 51
Transport Canada AD CF-2023-79 specifies procedures for inspecting
the left-hand and right-hand overhead bin electrical harnesses at the
class divider for damage (e.g., chafing), and if damage is found,
modifying the class divider mounting plate assembly to improve the
overhead bin harnesses protection or accomplishing a temporary repair.
Transport Canada AD CF-2023-79 also specifies procedures for eventually
modifying the class divider mounting plate assembly if a modification
was not done after accomplishing the inspection (i.e., if a temporary
repair was done or if no damage was found after accomplishing the
inspection). This material 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
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
referenced 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 Transport Canada AD CF-2023-79 described previously, except for
any differences identified as exceptions in the regulatory text of this
proposed AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate Transport Canada AD CF-2023-79 by reference
in the FAA final rule. This proposed AD would, therefore, require
compliance with Transport Canada AD CF-2023-79 in its entirety through
that incorporation, except for any differences identified as exceptions
in the regulatory text of this proposed AD. Service information
required by Transport Canada AD CF-2023-79 for compliance will be
available at regulations.gov under Docket No. FAA-2024-1470 after the
FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 246 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
[[Page 46338]]
Estimated Costs for Required Actions
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Labor cost Parts cost Cost per product Cost on U.S. operators
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3 work-hours x $85 per hour = $255..... $0 $255........................... $62,730.
Up to 9 work-hours x $85 per hour = 366 Up to 1,131.................... Up to 278,226.
$765.
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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 these on-condition actions:
Estimated Costs of On-Condition Actions *
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Labor cost Parts cost Cost per product
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Up to 9 work-hours x $85 per hour = $366 Up to $1,131.
$765.
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* The FAA has received no definitive data on which to base the cost
estimates for the on-condition optional temporary repair specified in
this proposed AD.
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:
MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier,
Inc.): Docket No. FAA-2024-1470; Project Identifier MCAI-2023-01284-
T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by July 15, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC (type certificate
previously held by Bombardier, Inc.) Model CL-600-2C10 (Regional Jet
Series 700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and
CL-600-2D24 (Regional Jet Series 900) airplanes, certificated in any
category, as identified in Transport Canada AD CF-2023-79, dated
December 21, 2023 (Transport Canada AD CF-2023-79), except for Group
3 and Group 5 airplanes identified Transport Canada AD CF-2023-79.
Note 1 to paragraph (c): Group 3 airplanes that are modified as
specified in Service Bulletin 670BA-25-110 become Group 2 airplanes
as identified in Transport Canada AD CF-2023-79.
Note 2 to paragraph (c): Group 5 airplanes that are modified as
specified in Service Bulletin 670BA-25-057 become Group 4 airplanes
as identified in Transport Canada AD CF-2023-79.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by a report that the electrical harnesses
in the overhead bin above the class divider may have insufficient or
no separation with the class divider mounting plate. The FAA is
issuing this AD to address possible chafing of the electrical
harness with the class divider mounting plate. The unsafe condition,
if not addressed, could result in the electrical harnesses becoming
chafed, which could affect the following aircraft systems: ordinance
signs, emergency lights/signs, passenger oxygen, and passenger
address and air conditioning systems.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, Transport Canada AD CF-2023-79.
(h) Exception To Transport Canada AD CF-2023-79
(1) Where Transport Canada AD CF-2023-79 refers to its effective
date or August 7, 2023 (the effective date of Transport Canada AD
CF-2023-56, dated July 24, 2023), this AD requires using the
effective date of this AD.
(2) Where Transport Canada AD CF-2023-79 refers to hours air
time, this AD requires using flight hours.
(3) Where paragraph A. of Part I of Transport Canada AD CF-2023-
79, specifies ``and, modify as required,'' for this AD,
[[Page 46339]]
replace that text with ``and, before further flight, modify as
required.''
(4) Where any MHIRJ service information referenced in Transport
Canada AD CF-2023-79 differs from any Safran service information
referenced in Transport Canada AD CF-2023-79, the MHIRJ service
information takes precedence over the Safran service information
because the initial revision of the Safran service information does
not list all affected part numbers.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation 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
International Validation Branch, mail it to the address identified
in paragraph (j) of this AD. Information may be emailed to: 9-AVS-
[email protected]. 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, International
Validation Branch, FAA; or Transport Canada; or MHI RJ Aviation
ULC's Transport Canada Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(j) Additional Information
For more information about this AD, contact Fatin Saumik,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; 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 this AD specifies otherwise.
(i) Transport Canada AD CF-2023-79, dated December 21, 2023.
(ii) [Reserved]
(3) Transport Canada AD CF-2023-79, contact Transport Canada,
Transport Canada National Aircraft Certification, 159 Cleopatra
Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-3639;
email [email protected]. You may find this Transport
Canada AD on the Transport Canada website tc.canada.ca/en/aviation.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th
Street, 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-locations, or email [email protected].
Issued on May 15, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-11005 Filed 5-28-24; 8:45 am]
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