Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 67523-67525 [2024-18629]
Download as PDF
Federal Register / Vol. 89, No. 162 / Wednesday, August 21, 2024 / Rules and Regulations
table, in the footnotes, in the third line,
‘‘1’’ should read ‘‘2’’.
[FR Doc. C1–2024–16643 Filed 8–20–24; 8:45 am]
BILLING CODE 0099–10–D
NUCLEAR REGULATORY
COMMISSION
10 CFR Part 72
[NRC–2024–0096]
RIN 3150–AL17
List of Approved Spent Fuel Storage
Casks: Holtec International HI–STORM
FW System Certificate of Compliance
No. 1032, Amendment No. 7
Nuclear Regulatory
Commission.
ACTION: Direct final rule; confirmation of
effective date.
AGENCY:
The U.S. Nuclear Regulatory
Commission (NRC) is confirming the
effective date of September 25, 2024, for
the direct final rule that was published
in the Federal Register on July 12, 2024.
The direct final rule amended the
Holtec International HI–STORM Flood/
Wind Multi-purpose Canister Storage
System listing within the ‘‘List of
approved spent fuel storage casks’’ to
include Amendment No. 7 to Certificate
of Compliance No. 1032.
DATES: Effective date: The U.S. Nuclear
Regulatory Commission (NRC) is
confirming the effective date of
September 25, 2024, for the direct final
rule that was published in the Federal
Register on July 12, 2024.
ADDRESSES: Please refer to Docket ID
NRC–2024–0096 when contacting the
NRC about the availability of
information for this action. You may
obtain publicly available information
related to this action by any of the
following methods:
• Federal Rulemaking Website: Go to
https://www.regulations.gov and search
for Docket ID NRC–2024–0096. Address
questions about NRC dockets to Helen
Chang; telephone: 301–415–3228; email:
Helen.Chang@nrc.gov. For technical
questions, contact the individual listed
in the FOR FURTHER INFORMATION
CONTACT section of this document.
• NRC’s Agencywide Documents
Access and Management System
(ADAMS): You may obtain publicly
available documents online in the
ADAMS Public Documents collection at
https://www.nrc.gov/reading-rm/
adams.html. To begin the search, select
‘‘Begin Web-based ADAMS Search.’’ For
problems with ADAMS, please contact
the NRC’s Public Document Room (PDR)
reference staff at 1–800–397–4209, 301–
lotter on DSK11XQN23PROD with RULES1
SUMMARY:
VerDate Sep<11>2014
15:51 Aug 20, 2024
Jkt 262001
415–4737, or by email to
PDR.Resource@nrc.gov. The
Amendment No. 7 of Certificate of
Compliance No. 1032 and associated
changes to the technical specifications,
and safety evaluation report can also be
viewed in ADAMS under Package
Accession No. ML24199A236.
• NRC’s PDR: The PDR, where you
may examine and order copies of
publicly available documents, is open
by appointment. To make an
appointment to visit the PDR, please
send an email to PDR.Resource@nrc.gov
or call 1–800–397–4209 or 301–415–
4737, between 8 a.m. and 4 p.m. eastern
time, Monday through Friday, except
Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Caylee Kenny, Office of Nuclear
Material Safety and Safeguards,
telephone: 301–415–7150, email:
Caylee.Kenny@nrc.gov; and Yen-Ju
Chen, Office of Nuclear Material Safety
and Safeguards, telephone: 301–415–
1018, email: Yen-Ju.Chen@nrc.gov. Both
are staff of the U.S. Nuclear Regulatory
Commission, Washington, DC 20555–
0001.
On July
12, 2024 (89 FR 57064), the NRC
published a direct final rule amending
its regulations in part 72 of title 10 of
the Code of Federal Regulations to
revise the Holtec International HI–
STORM Flood/Wind Multi-purpose
Canister Storage System (HI–STORM
FW System) listing in the ‘‘List of
approved spent fuel storage casks’’ to
include Amendment No. 7 to Certificate
of Compliance No. 1032. In the direct
final rule, the NRC stated that if no
significant adverse comments were
received, the direct final rule would
become effective on September 25,
2024. The NRC did not receive any
comments on the direct final rule.
Therefore, this direct final rule will
become effective as scheduled.
SUPPLEMENTARY INFORMATION:
Dated: August 16, 2024.
For the Nuclear Regulatory Commission.
Helen Chang,
Acting Chief, Regulatory Analysis and
Rulemaking Support Branch, Division of
Rulemaking, Environmental, and Financial
Support Office of Nuclear Material Safety
and Safeguards.
[FR Doc. 2024–18752 Filed 8–20–24; 8:45 am]
BILLING CODE 7590–01–P
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67523
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1009; Project
Identifier MCAI–2023–01221–T; Amendment
39–22782; AD 2024–14–01]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.)
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
MHI RJ Aviation ULC Model CL–600–
2D15 (Regional Jet Series 705) and CL–
600–2D24 (Regional Jet Series 900)
airplanes. This AD was prompted by a
report that torque wrenches used during
production installation of bulkhead
fittings on the oxygen lines of the
flightcrew oxygen mask stowage boxes
and adapter fitting on the oxygen
pressure gauge were out of calibration,
which resulted in a higher torque level
setting than required. This AD requires
replacement of the affected oxygen line
fittings, as specified in a Transport
Canada AD, which is incorporated by
reference. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective September
25, 2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 25, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–1009; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
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.AirworthinessDirectivesSUMMARY:
E:\FR\FM\21AUR1.SGM
21AUR1
67524
Federal Register / Vol. 89, No. 162 / Wednesday, August 21, 2024 / Rules and Regulations
Consignesdenavigabilite.TC@tc.gc.ca.
You may find this material on the
Transport Canada website at
tc.canada.ca/en/aviation. It is also
available at regulations.gov under
Docket No. FAA–2024–1009.
• 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:
Fatin Saumik, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; email Fatin.R.Saumik@
faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain MHI RJ Aviation ULC
Model CL–600–2D15 (Regional Jet
Series 705) and CL–600–2D24 (Regional
Jet Series 900) airplanes. The NPRM
published in the Federal Register on
April 29, 2024 (89 FR 33297). The
NPRM was prompted by AD CF–2023–
75, dated November 28, 2023, issued by
Transport Canada, which is the aviation
authority for Canada (Transport Canada
AD CF–2023–75) (also referred to as the
MCAI). The MCAI states MHI RJ
Aviation ULC received a quality escape
notice from a supplier, reporting that
torque wrenches used during
production installation of bulkhead
fittings on the oxygen lines of the
flightcrew oxygen mask stowage boxes
and adapter fitting on the oxygen
pressure gauge were out of calibration,
which resulted in a higher torque level
setting than required by drawing. This
over-torque could cause damage to the
oxygen line fittings which, if not
corrected, could cause oxygen leakage
before being annunciated and result in
lack of oxygen to the flightcrew when
needed.
In the NPRM, the FAA proposed to
require replacement of the affected
oxygen line fittings, as specified in
Transport Canada AD CF–2023–75. The
FAA is issuing 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–2024–1009.
Discussion of Final Airworthiness
Directive
Comments
The FAA received a comment from
the Air Line Pilots Association,
International (ALPA), who supported
the NPRM without change.
Conclusion
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
reviewed the relevant data, considered
the comment received, and determined
that air safety requires adopting this AD
as proposed. Accordingly, the FAA is
issuing this AD to address the unsafe
condition on this product. Except for
minor editorial changes, this AD is
adopted as proposed in the NPRM.
None of the changes will increase the
economic burden on any operator.
Related Material Under 1 CFR Part 51
Transport Canada AD CF–2023–75
specifies procedures for replacement of
the bulkhead fittings on the oxygen
lines of the mask stowage boxes and
replacement of the fitting adapter on the
oxygen pressure gauge. 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.
Costs of Compliance
The FAA estimates that this AD
affects 24 airplanes of U.S. registry. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
6 work-hours × $85 per hour = $510 ..........................................................................................
$350
$860
$20,640
lotter on DSK11XQN23PROD with RULES1
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
VerDate Sep<11>2014
15:51 Aug 20, 2024
Jkt 262001
develop on products identified in this
rulemaking action.
under the criteria of the Regulatory
Flexibility Act.
Regulatory Findings
List of Subjects in 14 CFR Part 39
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
E:\FR\FM\21AUR1.SGM
21AUR1
Federal Register / Vol. 89, No. 162 / Wednesday, August 21, 2024 / Rules and Regulations
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2024–14–01 MHI RJ Aviation ULC (Type
Certificate Previously Held by
Bombardier, Inc.): Amendment 39–
22782; Docket No. FAA–2024–1009;
Project Identifier MCAI–2023–01221–T.
(a) Effective Date
This airworthiness directive (AD) is
effective September 24, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC
(Type Certificate previously held by
Bombardier, Inc.) Model CL–600–2D15
(Regional Jet Series 705) and CL–600–2D24
(Regional Jet Series 900) airplanes,
certificated in any category, as identified in
Transport Canada AD CF–2023–75, dated
November 28, 2023 (Transport Canada AD
CF–2023–75).
(d) Subject
Air Transport Association (ATA) of
America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report that
torque wrenches used during production
installation of bulkhead fittings on the
oxygen lines of the flightcrew oxygen mask
stowage boxes and adapter fitting on the
oxygen pressure gauge were out of
calibration, which resulted in a higher torque
level setting than required. The FAA is
issuing this AD to address this over-torque,
which could cause damage to the oxygen line
fittings. The unsafe condition, if not
addressed, could result in oxygen leakage
before being annunciated and result in lack
of oxygen to the flightcrew when needed.
(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–
2023–75.
lotter on DSK11XQN23PROD with RULES1
(h) Exception to Transport Canada AD CF–
2023–75
(1) Where Transport Canada AD CF–2023–
75 refers to its effective date, this AD requires
using the effective date of this AD.
(2) Where Transport Canada AD CF–2023–
75 refers to hours air time, this AD requires
using flight hours.
(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
VerDate Sep<11>2014
15:51 Aug 20, 2024
Jkt 262001
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; 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 Fatin.R.Saumik@faa.gov.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the material listed in this paragraph
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as
applicable to do the actions required by this
AD, unless this AD specifies otherwise.
(i) Transport Canada AD CF–2023–75,
dated November 28, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF–2023–75,
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 at tc.canada.ca/
en/aviation.
(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-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. 2024–18629 Filed 8–20–24; 8:45 am]
BILLING CODE 4910–13–P
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Fmt 4700
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67525
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1006; Project
Identifier MCAI–2023–01222–T; Amendment
39–22781; AD 2024–13–07]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.)
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
MHI RJ Aviation ULC Model CL–600–
2D15 (Regional Jet Series 705) and CL–
600–2D24 (Regional Jet Series 900)
airplanes. This AD was prompted by a
notice from a supplier reporting that
torque wrenches used to install the air
driven generator (ADG) downlock cam
nut were out of calibration, which
resulted in a higher torque level setting
than required during the initial
production installation of the affected
cam nut. This AD requires replacement
of the affected ADG locking cam screw
and cam nut, as specified in a Transport
Canada AD, which is incorporated by
reference. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective September
25, 2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 25, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–1006; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
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.AirworthinessDirectivesSUMMARY:
E:\FR\FM\21AUR1.SGM
21AUR1
Agencies
[Federal Register Volume 89, Number 162 (Wednesday, August 21, 2024)]
[Rules and Regulations]
[Pages 67523-67525]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-18629]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1009; Project Identifier MCAI-2023-01221-T;
Amendment 39-22782; AD 2024-14-01]
RIN 2120-AA64
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain MHI RJ Aviation ULC Model CL-600-2D15 (Regional Jet Series 705)
and CL-600-2D24 (Regional Jet Series 900) airplanes. This AD was
prompted by a report that torque wrenches used during production
installation of bulkhead fittings on the oxygen lines of the flightcrew
oxygen mask stowage boxes and adapter fitting on the oxygen pressure
gauge were out of calibration, which resulted in a higher torque level
setting than required. This AD requires replacement of the affected
oxygen line fittings, as specified in a Transport Canada AD, which is
incorporated by reference. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective September 25, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September
25, 2024.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-1009; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
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.AirworthinessDirectives-
[[Page 67524]]
[email protected]. You may find this material on the
Transport Canada website at tc.canada.ca/en/aviation. It is also
available at regulations.gov under Docket No. FAA-2024-1009.
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: Fatin Saumik, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain MHI RJ Aviation
ULC Model CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24
(Regional Jet Series 900) airplanes. The NPRM published in the Federal
Register on April 29, 2024 (89 FR 33297). The NPRM was prompted by AD
CF-2023-75, dated November 28, 2023, issued by Transport Canada, which
is the aviation authority for Canada (Transport Canada AD CF-2023-75)
(also referred to as the MCAI). The MCAI states MHI RJ Aviation ULC
received a quality escape notice from a supplier, reporting that torque
wrenches used during production installation of bulkhead fittings on
the oxygen lines of the flightcrew oxygen mask stowage boxes and
adapter fitting on the oxygen pressure gauge were out of calibration,
which resulted in a higher torque level setting than required by
drawing. This over-torque could cause damage to the oxygen line
fittings which, if not corrected, could cause oxygen leakage before
being annunciated and result in lack of oxygen to the flightcrew when
needed.
In the NPRM, the FAA proposed to require replacement of the
affected oxygen line fittings, as specified in Transport Canada AD CF-
2023-75. The FAA is issuing 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-2024-1009.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from the Air Line Pilots Association,
International (ALPA), who supported the NPRM without change.
Conclusion
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 reviewed the relevant data, considered the
comment received, and determined that air safety requires adopting this
AD as proposed. Accordingly, the FAA is issuing this AD to address the
unsafe condition on this product. Except for minor editorial changes,
this AD is adopted as proposed in the NPRM. None of the changes will
increase the economic burden on any operator.
Related Material Under 1 CFR Part 51
Transport Canada AD CF-2023-75 specifies procedures for replacement
of the bulkhead fittings on the oxygen lines of the mask stowage boxes
and replacement of the fitting adapter on the oxygen pressure gauge.
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.
Costs of Compliance
The FAA estimates that this AD affects 24 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
6 work-hours x $85 per hour = $510........................... $350 $860 $20,640
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
[[Page 67525]]
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2024-14-01 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22782; Docket No. FAA-2024-1009;
Project Identifier MCAI-2023-01221-T.
(a) Effective Date
This airworthiness directive (AD) is effective September 24,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC (Type Certificate
previously held by Bombardier, Inc.) Model CL-600-2D15 (Regional Jet
Series 705) and CL-600-2D24 (Regional Jet Series 900) airplanes,
certificated in any category, as identified in Transport Canada AD
CF-2023-75, dated November 28, 2023 (Transport Canada AD CF-2023-
75).
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report that torque wrenches used
during production installation of bulkhead fittings on the oxygen
lines of the flightcrew oxygen mask stowage boxes and adapter
fitting on the oxygen pressure gauge were out of calibration, which
resulted in a higher torque level setting than required. The FAA is
issuing this AD to address this over-torque, which could cause
damage to the oxygen line fittings. The unsafe condition, if not
addressed, could result in oxygen leakage before being annunciated
and result in lack of oxygen to the flightcrew when needed.
(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-2023-75.
(h) Exception to Transport Canada AD CF-2023-75
(1) Where Transport Canada AD CF-2023-75 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where Transport Canada AD CF-2023-75 refers to hours air
time, this AD requires using flight hours.
(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: [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; 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 material listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(i) Transport Canada AD CF-2023-75, dated November 28, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF-2023-75, 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 at tc.canada.ca/en/
aviation.
(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-locations, or email [email protected].
Issued on July 10, 2024.
James D. Foltz,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-18629 Filed 8-20-24; 8:45 am]
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