Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 87331-87334 [2023-27680]
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Federal Register / Vol. 88, No. 241 / Monday, December 18, 2023 / Rules and Regulations
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2023–24–01 Airbus Canada Limited
Partnership (Type Certificate Previously
Held by C Series Aircraft Limited
Partnership (CSALP); Bombardier, Inc.):
Amendment 39–22617; Docket No.
FAA–2023–2229; Project Identifier
MCAI–2023–00736–T.
(a) Effective Date
This airworthiness directive (AD) is
effective January 2, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Canada Limited
Partnership (Type Certificate previously held
by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD–500–
1A10 and BD–500–1A11 airplanes,
certificated in any category, as identified in
Transport Canada AD CF–2023–39, dated
June 6, 2023 (Transport Canada AD CF–
2023–39).
(d) Subject
Air Transport Association (ATA) of
America Code 28, Fuel.
(e) Unsafe Condition
This AD was prompted by a reported
interference between the pilot valve fittings
and their mating holes in the rear spar of the
center wing box. The FAA is issuing this AD
to address fitting failure, which could lead to
a failure of its shroud attachment and
subsequent fuel leak into the area behind the
rear spar and into the landing gear bay. Such
significant fuel leak, combined with a
potential ignition source such as a failure of
a bleed duct or a failure of wires/connectors
in these areas, could create a fire hazard on
the airplane.
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(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–
2023–39.
(h) Exception to Transport Canada AD CF–
2023–39
Where Transport Canada AD CF–2023–39
refers to its effective date, this AD requires
using the effective date of this AD.
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16:02 Dec 15, 2023
Jkt 262001
(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 International Validation Branch, send
it to the attention of the person identified in
paragraph (j)(1) of this AD. Information may
be emailed to: 9-AVS-AIR-730-AMOC@
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 Airbus
Canada Limited Partnership’s Transport
Canada Design Approval Organization
(DAO). If approved by the DAO, the approval
must include the DAO-authorized signature.
(j) Additional Information
(1) For more information about this AD,
contact Gabriel Kim, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; phone: 516–228–
7300; email: 9-avs-nyaco-cos@faa.gov.
(2) For Airbus Canada Limited Partnership
service information identified in this AD that
is not incorporated by reference, contact
Airbus Canada Limited Partnership, 13100
Henri-Fabre Boulevard, Mirabel, Que´bec J7N
3C6, Canada; telephone 450–476–7676; email
a220_
a220world.airbus.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.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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–2023–39,
dated June 6, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF–2023–39,
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;
website 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
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87331
availability of this material at the FAA, call
206–231–3195.
(5) You may view this material 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.
Issued on November 29, 2023.
Ross Landes,
Deputy Director for Regulatory Operations,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2023–27677 Filed 12–15–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–1496; Project
Identifier MCAI–2022–01059–T; Amendment
39–22619; AD 2023–24–03]
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 all MHI
RJ Aviation ULC Model CL–600–2B19
(Regional Jet Series 100 & 440); CL–600–
2C10 (Regional Jet Series 700, 701, &
702); CL–600–2C11 (Regional Jet Series
550); CL–600–2D15 (Regional Jet Series
705); CL–600–2D24 (Regional Jet Series
900); and CL–600–2E25 (Regional Jet
Series 1000) airplanes. This AD was
prompted by a determination that
aircraft maintenance manual (AMM)
tasks and certification maintenance
requirement (CMR) tasks are necessary.
This AD requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive AMM and CMR tasks. The
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective January 22,
2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 22, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1496; or in person at
Docket Operations between 9 a.m. and
SUMMARY:
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87332
Federal Register / Vol. 88, No. 241 / Monday, December 18, 2023 / Rules and Regulations
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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 service information identified
in this final rule, contact MHI RJ
Aviation Group, Customer Response
Center, 3655 Ave. des GrandesTourelles, Suite 110, Boisbriand,
Que´bec J7H 0E2 Canada; North America
toll-free telephone 833–990–7272 or
direct-dial telephone 450–990–7272; fax
514–855–8501; email thd.crj@
mhirj.com; website mhirj.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. It is also available at
regulations.gov under Docket No. FAA–
2023–1496.
FOR FURTHER INFORMATION CONTACT:
Elizabeth Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590;
telephone 516–228–7300; email 9-avsnyaco-cos@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 all MHI RJ Aviation ULC Model
CL–600–2B19 (Regional Jet Series 100 &
440); CL–600–2C10 (Regional Jet Series
700, 701, & 702); CL–600–2C11
(Regional Jet Series 550); CL–600–2D15
(Regional Jet Series 705); CL–600–2D24
(Regional Jet Series 900); and CL–600–
2E25 (Regional Jet Series 1000)
airplanes. The NPRM published in the
Federal Register on July 19, 2023 (88 FR
46118). The NPRM was prompted by
AD CF–2022–42, dated August 8, 2022,
issued by Transport Canada, which is
the aviation authority for Canada
(referred to after this as the MCAI). The
MCAI states that operators have
reported frequent flight interruptions
and high lavatory smoke detector
removal rates due to the frequent testing
of the smoke detector self-test switch by
the flight crew using unsuitable objects.
The MCAI also states there is a potential
dormant failure of the lavatory smoke
detector if the self-test switch check is
not performed in accordance with
revised procedures.
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16:02 Dec 15, 2023
Jkt 262001
In the NPRM, the FAA proposed to
require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive AMM and CMR tasks. The
FAA is issuing this AD to address a
potential dormant failure of the lavatory
smoke detector if the self-test switch
check is not performed in accordance
with revised AMM or CMR tasks. If
these maintenance task changes are not
implemented, and in combination with
a fire in the lavatory, this may lead to
a delay in the reaction time to address
smoke/fire in the lavatory.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–1496.
Discussion of Final Airworthiness
Directive
Comments
The FAA received a comment from
Air Line Pilots Association,
International, who supported the NPRM
without change.
The FAA received an additional
comment from MHI RJ Aviation. The
following presents the comment
received on the NPRM and the FAA’s
response.
Request To Identify Corrected
Revisions
MHI RJ requested that the corrected
revisions for Aircraft Maintenance
Manual (AMM) Tasks 26–16–00–710–
804–A01 and 26–16–00–710–803–A01
be identified as found in AMM CSP B–
001, Revision 71. The commenter stated
that the Maintenance Task Card Manual
(MTCM) Task Card updates were also
implemented in AMM Tasks 26–16–00–
710–804–A01 and 26–16–00–710–803–
A01, but references to the AMM tasks in
the proposed AD do not indicate the
corrected revision.
The FAA agrees with the requested
change since it provides a means for
operators to ensure the revised
maintenance tasks are included in the
AMM revision they are using. Therefore,
figure 1 to paragraph (h) of this AD has
been changed to specify AMM Rev 68 or
later approved revisions.
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
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Fmt 4700
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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 Service Information Under 1
CFR Part 51
The FAA reviewed Bombardier
Temporary Revision 2A–75, dated May
28, 2020. This service information
specifies new or more restrictive CMR
tasks. 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.
Costs of Compliance
The FAA estimates that this AD
affects 1,024 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
The FAA has determined that revising
the maintenance or inspection program
takes an average of 90 work-hours per
operator, although the agency
recognizes that this number may vary
from operator to operator. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), the FAA has
determined that a per-operator estimate
is more accurate than a per-airplane
estimate. Therefore, the agency
estimates the average total cost per
operator to be $7,650 (90 work-hours ×
$85 per work-hour).
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
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Federal Register / Vol. 88, No. 241 / Monday, December 18, 2023 / Rules and Regulations
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:
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
(c) Applicability
This AD applies to all MHI RJ Aviation
ULC (Type Certificate previously held by
Bombardier, Inc.) airplanes identified in
paragraphs (c)(1) through (6) of this AD,
certificated in any category.
(1) Model CL–600–2B19 (Regional Jet
Series 100 & 440) airplanes.
(2) Model CL–600–2C10 (Regional Jet
Series 700, 701, & 702) airplanes.
(3) Model CL–600–2C11 (Regional Jet
Series 550) airplanes.
(4) Model CL–600–2D15 (Regional Jet
Series 705) airplanes.
(5) Model CL–600–2D24 (Regional Jet
Series 900) airplanes.
(6) Model CL–600–2E25 (Regional Jet
Series 1000) airplanes.
(e) Reason
This AD was prompted by a determination
that new or more restrictive aircraft
maintenance manual (AMM) tasks and
certification maintenance requirement (CMR)
tasks are necessary. The FAA is issuing this
AD to address a potential dormant failure of
the lavatory smoke detector if the self-test
switch check is not performed in accordance
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Maintenance or Inspection Program
Revision for Model CL–600–2B19 (Regional
Jet Series 100 & 440) Airplanes
For Model CL–600–2B19 (Regional Jet
Series 100 & 440) airplanes: Within 60 days
after the effective date of this AD, revise the
existing maintenance or inspection program,
as applicable, to incorporate the information
specified in Bombardier Temporary Revision
2A–75, dated May 28, 2020. The initial
compliance time is within 12 months after
the effective date of this AD.
(h) Maintenance or Inspection Program
Revision for Other Airplanes
For airplanes identified in paragraphs
(c)(2) through (6) of this AD: Within 60 days
after the effective date of this AD, revise the
existing maintenance or inspection program,
as applicable, to incorporate the information
specified in Figure 1 to paragraph (h) of this
AD. The initial compliance time for doing the
tasks is within 12 months after the effective
date of this AD.
Figure 1 to Paragraph (h)—AMM task for an
operational check of the lavatory smoke
detector (forward and aft)
Interval Limitation
AMM Task Numbers (CSP B-001 Rev 68 or
later approved revisions)
All
3,000 flight hours
26-16-00-710-804-AO 1
26-16-00-710-803-AOl
After the existing maintenance or
inspection program has been revised as
required by paragraph (g) or (h) of this AD,
no alternative actions (e.g., inspections) or
intervals may be used unless the actions, and
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (j)(1) of this AD.
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(b) Affected ADs
None.
with the revised AMM or CMR tasks. If these
maintenance task changes are not
implemented, and in combination with a fire
in the lavatory, this may lead to a delay in
the reaction time to address smoke/fire in the
lavatory.
Effectivity
(i) No Alternative Actions or Intervals
(j) Other FAA 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.
VerDate Sep<11>2014
(a) Effective Date
This airworthiness directive (AD) is
effective January 22, 2024.
(d) Subject
Air Transport Association (ATA) of
America Code 26, Fire Protection.
PART 39—AIRWORTHINESS
DIRECTIVES
§ 39.13
2023–24–03 MHI RJ Aviation ULC (Type
Certificate Previously Held by
Bombardier, Inc.): Amendment 39–
22619; Docket No. FAA–2023–1496;
Project Identifier MCAI–2022–01059–T.
16:02 Dec 15, 2023
Jkt 262001
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 certification office,
send it to ATTN: Program Manager,
Continuing Operational Safety, FAA,
International Validation Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7300. 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
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RJ Aviation ULC’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–
2022–42, dated August 8, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2023–1496.
(2) For more information about this AD,
contact Elizabeth Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
E:\FR\FM\18DER1.SGM
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ER18DE23.016
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.
87333
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Federal Register / Vol. 88, No. 241 / Monday, December 18, 2023 / Rules and Regulations
(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
to do the actions required by this AD, unless
this AD specifies otherwise.
(i) Bombardier Temporary Revision 2A–75,
dated May 28, 2020.
(ii) [Reserved]
(3) For service information identified in
this AD, contact MHI RJ Aviation Group,
Customer Response Center, 3655 Ave. des
Grandes-Tourelles, Suite 110, Boisbriand,
Que´bec J7H 0E2 Canada; North America tollfree telephone 833–990–7272 or direct-dial
telephone 450–990–7272; fax 514–855–8501;
email thd.crj@mhirj.com; website mhirj.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 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.
[Docket No. FAA–2023–1505; Project
Identifier MCAI–2023–00246–T; Amendment
39–22622; AD 2023–24–05]
of a certain publication listed in this AD
as of January 22, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1505; 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 service information identified
in this final rule, 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. It is also available at
regulations.gov under Docket No. FAA–
2023–1505.
FOR FURTHER INFORMATION CONTACT:
Gabriel Kim, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@
faa.gov.
RIN 2120–AA64
SUPPLEMENTARY INFORMATION:
Airworthiness Directives; Bombardier,
Inc., Airplanes
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 Bombardier, Inc., Model
CL–600–2B16 (604 Variant) airplanes.
The NPRM published in the Federal
Register on July 25, 2023 (88 FR 47827).
The NPRM was prompted by AD CF–
2023–06, dated February 9, 2023
(referred to after this as the MCAI),
issued by Transport Canada, which is
the aviation authority for Canada. The
MCAI states the sleeve loops on certain
passenger oxygen mask lanyards were
found to have improper crimping and
unsealed ends.
In the NPRM, the FAA proposed to
require an inspection of the passenger
oxygen mask lanyards and replacement
of defective oxygen mask lanyards. In
the NPRM, the FAA also proposed to
prohibit the installation of affected
parts. The FAA is issuing this AD to
Issued on November 29, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–27680 Filed 12–15–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc., Model CL–600–2B16
(604 Variant) airplanes. This AD was
prompted by sleeve loops on some
passenger oxygen mask lanyards that
had improper crimping and unsealed
ends. This AD requires an inspection of
the passenger oxygen mask lanyards and
replacement of defective oxygen mask
lanyards. This AD also prohibits the
installation of affected parts. The FAA
is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective January 22,
2024.
The Director of the Federal Register
approved the incorporation by reference
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SUMMARY:
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16:02 Dec 15, 2023
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address these defective oxygen mask
lanyards, which could result in no
oxygen flow to the mask during an
emergency.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–1505.
Discussion of Final Airworthiness
Directive
Comments
The FAA received a comment from
Bombardier. The following presents the
comment received on the NPRM and the
FAA’s response to the comment.
Request for Removal of Certain
Variants
Bombardier requested that the
proposed AD be revised to remove
reference to 601–3A and 601–3R
Variants. The commenter stated that the
proposed AD only applies to Model CL–
600–2B16 (604 Variant) airplanes
(Challenger 605 designation).
Bombardier noted that the airplane
serial numbers given in Bombardier
Service Bulletin 605–35–008, dated
October 28, 2022, and referenced in
Transport Canada AD CF–2023–06, are
all Model CL–600–2B16 (604 Variant)
airplanes.
The FAA agrees for the reasons
provided. The FAA revised the
Summary, Background, and paragraph
(c) of this AD accordingly.
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 comments 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, and any other
changes described previously, this AD is
adopted as proposed in the NPRM.
None of the changes will increase the
economic burden on any operator.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Bombardier
Service Bulletin 605–35–008, dated
October 28, 2022. This service
information specifies procedures for a
visual inspection of the existing
passenger oxygen mask lanyards
installed in the cabin or lavatory oxygen
box assemblies, and replacement of the
defective oxygen mask lanyards. The
E:\FR\FM\18DER1.SGM
18DER1
Agencies
[Federal Register Volume 88, Number 241 (Monday, December 18, 2023)]
[Rules and Regulations]
[Pages 87331-87334]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-27680]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1496; Project Identifier MCAI-2022-01059-T;
Amendment 39-22619; AD 2023-24-03]
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 all
MHI RJ Aviation ULC Model CL-600-2B19 (Regional Jet Series 100 & 440);
CL-600-2C10 (Regional Jet Series 700, 701, & 702); CL-600-2C11
(Regional Jet Series 550); CL-600-2D15 (Regional Jet Series 705); CL-
600-2D24 (Regional Jet Series 900); and CL-600-2E25 (Regional Jet
Series 1000) airplanes. This AD was prompted by a determination that
aircraft maintenance manual (AMM) tasks and certification maintenance
requirement (CMR) tasks are necessary. This AD requires revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive AMM and CMR tasks. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective January 22, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 22,
2024.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1496; or in person at Docket Operations between 9
a.m. and
[[Page 87332]]
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 service information identified in this final rule,
contact MHI RJ Aviation Group, Customer Response Center, 3655 Ave. des
Grandes-Tourelles, Suite 110, Boisbriand, Qu[eacute]bec J7H 0E2 Canada;
North America toll-free telephone 833-990-7272 or direct-dial telephone
450-990-7272; fax 514-855-8501; email mhirj.com">thd.crj@mhirj.com; website
mhirj.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. It is also available at
regulations.gov under Docket No. FAA-2023-1496.
FOR FURTHER INFORMATION CONTACT: Elizabeth Dowling, 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 all MHI RJ Aviation ULC
Model CL-600-2B19 (Regional Jet Series 100 & 440); CL-600-2C10
(Regional Jet Series 700, 701, & 702); CL-600-2C11 (Regional Jet Series
550); CL-600-2D15 (Regional Jet Series 705); CL-600-2D24 (Regional Jet
Series 900); and CL-600-2E25 (Regional Jet Series 1000) airplanes. The
NPRM published in the Federal Register on July 19, 2023 (88 FR 46118).
The NPRM was prompted by AD CF-2022-42, dated August 8, 2022, issued by
Transport Canada, which is the aviation authority for Canada (referred
to after this as the MCAI). The MCAI states that operators have
reported frequent flight interruptions and high lavatory smoke detector
removal rates due to the frequent testing of the smoke detector self-
test switch by the flight crew using unsuitable objects. The MCAI also
states there is a potential dormant failure of the lavatory smoke
detector if the self-test switch check is not performed in accordance
with revised procedures.
In the NPRM, the FAA proposed to require revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive AMM and CMR tasks. The FAA is issuing this AD to
address a potential dormant failure of the lavatory smoke detector if
the self-test switch check is not performed in accordance with revised
AMM or CMR tasks. If these maintenance task changes are not
implemented, and in combination with a fire in the lavatory, this may
lead to a delay in the reaction time to address smoke/fire in the
lavatory.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1496.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Air Line Pilots Association,
International, who supported the NPRM without change.
The FAA received an additional comment from MHI RJ Aviation. The
following presents the comment received on the NPRM and the FAA's
response.
Request To Identify Corrected Revisions
MHI RJ requested that the corrected revisions for Aircraft
Maintenance Manual (AMM) Tasks 26-16-00-710-804-A01 and 26-16-00-710-
803-A01 be identified as found in AMM CSP B-001, Revision 71. The
commenter stated that the Maintenance Task Card Manual (MTCM) Task Card
updates were also implemented in AMM Tasks 26-16-00-710-804-A01 and 26-
16-00-710-803-A01, but references to the AMM tasks in the proposed AD
do not indicate the corrected revision.
The FAA agrees with the requested change since it provides a means
for operators to ensure the revised maintenance tasks are included in
the AMM revision they are using. Therefore, figure 1 to paragraph (h)
of this AD has been changed to specify AMM Rev 68 or later approved
revisions.
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 Service Information Under 1 CFR Part 51
The FAA reviewed Bombardier Temporary Revision 2A-75, dated May 28,
2020. This service information specifies new or more restrictive CMR
tasks. 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.
Costs of Compliance
The FAA estimates that this AD affects 1,024 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
agency recognizes that this number may vary from operator to operator.
Since operators incorporate maintenance or inspection program changes
for their affected fleet(s), the FAA has determined that a per-operator
estimate is more accurate than a per-airplane estimate. Therefore, the
agency estimates the average total cost per operator to be $7,650 (90
work-hours x $85 per work-hour).
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
[[Page 87333]]
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.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2023-24-03 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22619; Docket No. FAA-2023-1496;
Project Identifier MCAI-2022-01059-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 22, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all MHI RJ Aviation ULC (Type Certificate
previously held by Bombardier, Inc.) airplanes identified in
paragraphs (c)(1) through (6) of this AD, certificated in any
category.
(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes.
(2) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702)
airplanes.
(3) Model CL-600-2C11 (Regional Jet Series 550) airplanes.
(4) Model CL-600-2D15 (Regional Jet Series 705) airplanes.
(5) Model CL-600-2D24 (Regional Jet Series 900) airplanes.
(6) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 26, Fire
Protection.
(e) Reason
This AD was prompted by a determination that new or more
restrictive aircraft maintenance manual (AMM) tasks and
certification maintenance requirement (CMR) tasks are necessary. The
FAA is issuing this AD to address a potential dormant failure of the
lavatory smoke detector if the self-test switch check is not
performed in accordance with the revised AMM or CMR tasks. If these
maintenance task changes are not implemented, and in combination
with a fire in the lavatory, this may lead to a delay in the
reaction time to address smoke/fire in the lavatory.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision for Model CL-600-2B19
(Regional Jet Series 100 & 440) Airplanes
For Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes:
Within 60 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Bombardier Temporary
Revision 2A-75, dated May 28, 2020. The initial compliance time is
within 12 months after the effective date of this AD.
(h) Maintenance or Inspection Program Revision for Other Airplanes
For airplanes identified in paragraphs (c)(2) through (6) of
this AD: Within 60 days after the effective date of this AD, revise
the existing maintenance or inspection program, as applicable, to
incorporate the information specified in Figure 1 to paragraph (h)
of this AD. The initial compliance time for doing the tasks is
within 12 months after the effective date of this AD.
Figure 1 to Paragraph (h)--AMM task for an operational check of the
lavatory smoke detector (forward and aft)
[GRAPHIC] [TIFF OMITTED] TR18DE23.016
(i) No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) or (h) of this AD, no
alternative actions (e.g., inspections) or intervals may be used
unless the actions, and intervals are approved as an alternative
method of compliance (AMOC) in accordance with the procedures
specified in paragraph (j)(1) of this AD.
(j) Other FAA 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
certification office, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, International Validation Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-
7300. 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.
(k) Additional Information
(1) Refer to Transport Canada AD CF-2022-42, dated August 8,
2022, for related information. This Transport Canada AD may be found
in the AD docket at regulations.gov under Docket No. FAA-2023-1496.
(2) For more information about this AD, contact Elizabeth
Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference
[[Page 87334]]
(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 to do the actions
required by this AD, unless this AD specifies otherwise.
(i) Bombardier Temporary Revision 2A-75, dated May 28, 2020.
(ii) [Reserved]
(3) For service information identified in this AD, contact MHI
RJ Aviation Group, Customer Response Center, 3655 Ave. des Grandes-
Tourelles, Suite 110, Boisbriand, Qu[eacute]bec J7H 0E2 Canada;
North America toll-free telephone 833-990-7272 or direct-dial
telephone 450-990-7272; fax 514-855-8501; email mhirj.com">thd.crj@mhirj.com;
website mhirj.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 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 November 29, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-27680 Filed 12-15-23; 8:45 am]
BILLING CODE 4910-13-P