Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 21-23 [2023-28801]
Download as PDF
Federal Register / Vol. 89, No. 1 / Tuesday, January 2, 2024 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–1823; Project
Identifier MCAI–2023–00314–T; Amendment
39–22628; AD 2023–25–01]
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 Model 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
report of a passenger seat Y-belt (lap
belt) re-installed in the wrong
orientation, due to an incorrect
maintenance manual. This AD requires
inspecting certain Y-belts for correct
installation and damage and corrective
actions if necessary. This AD also
prohibits the use of certain revisions of
a maintenance task. The FAA is issuing
this AD to address the unsafe condition
on these products.
DATES: This AD is effective February 6,
2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of February 6, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1823; 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:
khammond on DSKJM1Z7X2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
14:37 Dec 29, 2023
Jkt 262001
• For MHI RJ 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–
2023–1823.
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:
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 Model 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
September 13, 2023 (88 FR 62709). The
NPRM was prompted by AD CF–2023–
10, dated February 17, 2023, issued by
Transport Canada, which is the aviation
authority for Canada (referred to after
this as the MCAI). The MCAI states that
following maintenance on a Model CL–
600–2C10 airplane, a Y-belt (also known
as lap belt) was re-installed in the wrong
orientation. The MCAI further states
that the instructions contained within
the aircraft maintenance manual (AMM)
on how to install the passenger seat Ybelts, showed an incorrect orientation of
the Y-belt assembly. The MCAI confirms
the manufacturer updated the AMM
tasks and these instructions have been
corrected. Y-belts installed in the wrong
orientation, if not corrected, could result
in passenger injury due to head impact
on the front monument during an
emergency landing.
In the NPRM, the FAA proposed to
require inspecting certain Y-belts for
correct installation and damage and
PO 00000
Frm 00017
Fmt 4700
Sfmt 4700
21
corrective actions if necessary. The FAA
also proposed to prohibit the use of
certain revisions of a maintenance task.
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–2023–1823.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
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 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 MHI RJ Service
Bulletin 670BA–25–135, Revision B,
dated November 25, 2022. This service
information specifies procedures to
inspect for correct installation (as
shown in certain maintenance tasks) of
each passenger seat Y-belt. This service
information also specifies corrective
actions, which include re-installing
each incorrectly installed Y-belt per
certain maintenance tasks and
addressing damage (includes dents or
misshapen hooks that attach the belt to
the seat).
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 606 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
E:\FR\FM\02JAR1.SGM
02JAR1
22
Federal Register / Vol. 89, No. 1 / Tuesday, January 2, 2024 / Rules and Regulations
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
2 work-hours × $85 per hour = $170 ..................................................................................................
$0
$170
$103,020
The FAA estimates the following
costs to do any necessary replacements
that would be required based on the
results of the inspection. The agency has
no way of determining the number of
aircraft that might need these
replacements.
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
Parts cost
Up to 0.5 work-hours × $85 per hour = $43 ....................
Up to $550 per Y-belt assembly .....................................
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.
khammond on DSKJM1Z7X2PROD with RULES
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.
VerDate Sep<11>2014
14:37 Dec 29, 2023
Jkt 262001
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
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:
■
2023–25–01 MHI RJ Aviation ULC (Type
Certificate Previously Held by
Bombardier, Inc.): Amendment 39–
22628; Docket No. FAA–2023–1823;
Project Identifier MCAI–2023–00314–T.
(a) Effective Date
This airworthiness directive (AD) is
effective February 6, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC
(Type Certificate previously held by
Bombardier, Inc.) airplanes, certificated in
any category, identified in paragraphs (c)(1)
through (3) of this AD.
(1) Model CL–600–2C10 (Regional Jet
Series 700, 701 & 702) and CL–600–2C11
(Regional Jet Series 550) airplanes, serial
numbers (S/N) 10001 through 10348
inclusive.
(2) Model CL–600–2D15 (Regional Jet
Series 705) and CL–600–2D24 (Regional Jet
Series 900) airplanes, S/N 15001 through
15499 inclusive.
(3) Model CL–600–2E25 (Regional Jet
Series 1000) airplanes, S/N 19001 through
19064 inclusive.
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Cost per product
Up to $593.
(d) Subject
Air Transport Association (ATA) of
America Code: 25, Equipment/Furnishings.
(e) Unsafe Condition
This AD was prompted by a report of a
passenger seat Y-belt (lap-belt) re-installed in
the wrong orientation, due to an incorrect
maintenance manual. The FAA is issuing this
AD to detect and address Y-belts that are
incorrectly installed. The unsafe condition, if
not addressed, could result in passenger
injury due to head impact on the front
monument during an emergency landing.
(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: Within 24 months after the effective date
of this AD, inspect each Y-belt for correct
installation and damage and, if any incorrect
installation or damage is found, within 24
months after the effective date of this AD, do
all applicable corrective actions, in
accordance with paragraph B, ‘‘Procedure,’’
of the Accomplishment Instructions of MHI
RJ Service Bulletin 670BA–25–135, Revision
B, dated November 25, 2022. For this AD,
damage includes dents or misshapen hooks
that attach the belt to the seat.
Note 1 to paragraph (g): Y-belts are also
known as lap belts.
(h) Exceptions to Service Information
Where paragraph B, ‘‘Procedure,’’ of the
Accomplishment Instructions of MHI RJ
Service Bulletin 670BA–25–135, Revision B,
dated November 25, 2022, specifies to ‘‘refer
to AMM’’ replace those words with ‘‘in
accordance with AMM.’’
(i) Maintenance Task Prohibition
As of the effective date of this AD, it is
prohibited to use MHI RJ Aviation ULC
Aircraft Maintenance Manual (AMM) task
25–21–04–400–801, revision 69 or earlier.
(j) Credit for Previous Actions
This paragraph provides credit for actions
required by paragraph (g) of this AD, if those
actions were performed before the effective
date of this AD using the service information
E:\FR\FM\02JAR1.SGM
02JAR1
Federal Register / Vol. 89, No. 1 / Tuesday, January 2, 2024 / Rules and Regulations
identified in paragraph (j)(1) or (2) of this AD,
provided the actions were done using MHI RJ
AMM Revision 70, dated May 25, 2022, or
Revision 71, dated December 16, 2022.
(1) MHI RJ Service Bulletin 670BA–25–
135, dated June 1, 2022.
(2) MHI RJ Service Bulletin 670BA–25–
135, Revision A, dated August 30, 2022.
(k) 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 (l)(2) 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 MHI RJ
Aviation ULC’s Transport Canada Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
khammond on DSKJM1Z7X2PROD with RULES
(l) Additional Information
(1) Refer to Transport Canada AD CF–
2023–10, dated February 17, 2023, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2023–1823.
(2) 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.
(3) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (m)(3) and (4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) MHI RJ Service Bulletin 670BA–25–135,
Revision B, dated November 25, 2022.
(ii) [Reserved]
(3) For MHI RJ Aviation ULC 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 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.
VerDate Sep<11>2014
14:37 Dec 29, 2023
Jkt 262001
(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.
Issued on December 5, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–28801 Filed 12–29–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–1822; Project
Identifier MCAI–2023–00653–T; Amendment
39–22624; AD 2023–24–07]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus SAS Model A310 airplanes. This
AD was prompted by a determination
that new or more restrictive
airworthiness limitations are necessary.
This AD requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations, as
specified in a European Union Aviation
Safety Agency (EASA) 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 February 6,
2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of February 6, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1822; 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
SUMMARY:
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
23
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 EASA material incorporated by
reference in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
website easa.europa.eu. You may find
this material on the EASA website at
ad.easa.europa.eu.
• 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.
It is also available in the AD docket at
regulations.gov under Docket No. FAA–
2023–1822.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aviation Safety Engineer, FAA,
2200 South 216th Street, Des Moines,
WA 98198; telephone 206–231–3225;
email dan.rodina@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 Airbus SAS Model A310
series airplanes. The NPRM published
in the Federal Register on September 8,
2023 (88 FR 61990). The NPRM was
prompted by AD 2023–0092, dated May
5, 2023, issued by EASA, which is the
Technical Agent for the Member States
of the European Union (EASA AD 2023–
0092) (also referred to as the MCAI). The
MCAI states that new or more restrictive
airworthiness limitations have been
developed.
In the NPRM, the FAA proposed to
require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations, as
specified in EASA AD 2023–0092. The
FAA is issuing this AD to address
fatigue cracking, damage, or corrosion in
principal structural elements.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–1822.
Discussion of Final Airworthiness
Directive
Comments
The FAA received comments from
FedEx who supported the NPRM
without change.
Conclusion
This product has been approved by
the aviation authority of another
E:\FR\FM\02JAR1.SGM
02JAR1
Agencies
[Federal Register Volume 89, Number 1 (Tuesday, January 2, 2024)]
[Rules and Regulations]
[Pages 21-23]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-28801]
[[Page 21]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1823; Project Identifier MCAI-2023-00314-T;
Amendment 39-22628; AD 2023-25-01]
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 Model 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 report of a
passenger seat Y-belt (lap belt) re-installed in the wrong orientation,
due to an incorrect maintenance manual. This AD requires inspecting
certain Y-belts for correct installation and damage and corrective
actions if necessary. This AD also prohibits the use of certain
revisions of a maintenance task. The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective February 6, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of February 6,
2024.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1823; 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 MHI RJ 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-2023-1823.
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 Model
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 September 13,
2023 (88 FR 62709). The NPRM was prompted by AD CF-2023-10, dated
February 17, 2023, issued by Transport Canada, which is the aviation
authority for Canada (referred to after this as the MCAI). The MCAI
states that following maintenance on a Model CL-600-2C10 airplane, a Y-
belt (also known as lap belt) was re-installed in the wrong
orientation. The MCAI further states that the instructions contained
within the aircraft maintenance manual (AMM) on how to install the
passenger seat Y-belts, showed an incorrect orientation of the Y-belt
assembly. The MCAI confirms the manufacturer updated the AMM tasks and
these instructions have been corrected. Y-belts installed in the wrong
orientation, if not corrected, could result in passenger injury due to
head impact on the front monument during an emergency landing.
In the NPRM, the FAA proposed to require inspecting certain Y-belts
for correct installation and damage and corrective actions if
necessary. The FAA also proposed to prohibit the use of certain
revisions of a maintenance task. 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-2023-1823.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
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 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 MHI RJ Service Bulletin 670BA-25-135, Revision B,
dated November 25, 2022. This service information specifies procedures
to inspect for correct installation (as shown in certain maintenance
tasks) of each passenger seat Y-belt. This service information also
specifies corrective actions, which include re-installing each
incorrectly installed Y-belt per certain maintenance tasks and
addressing damage (includes dents or misshapen hooks that attach the
belt to the seat).
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 606 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
[[Page 22]]
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
2 work-hours x $85 per hour = $170................................. $0 $170 $103,020
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
inspection. The agency has no way of determining the number of aircraft
that might need these replacements.
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
Up to 0.5 work-hours x $85 per Up to $550 per Y-belt Up to $593.
hour = $43. assembly.
------------------------------------------------------------------------
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.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2023-25-01 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22628; Docket No. FAA-2023-1823;
Project Identifier MCAI-2023-00314-T.
(a) Effective Date
This airworthiness directive (AD) is effective February 6, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC (Type Certificate
previously held by Bombardier, Inc.) airplanes, certificated in any
category, identified in paragraphs (c)(1) through (3) of this AD.
(1) Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) and
CL-600-2C11 (Regional Jet Series 550) airplanes, serial numbers (S/
N) 10001 through 10348 inclusive.
(2) Model CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24
(Regional Jet Series 900) airplanes, S/N 15001 through 15499
inclusive.
(3) Model CL-600-2E25 (Regional Jet Series 1000) airplanes, S/N
19001 through 19064 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code: 25, Equipment/
Furnishings.
(e) Unsafe Condition
This AD was prompted by a report of a passenger seat Y-belt
(lap-belt) re-installed in the wrong orientation, due to an
incorrect maintenance manual. The FAA is issuing this AD to detect
and address Y-belts that are incorrectly installed. The unsafe
condition, if not addressed, could result in passenger injury due to
head impact on the front monument during an emergency landing.
(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: Within 24
months after the effective date of this AD, inspect each Y-belt for
correct installation and damage and, if any incorrect installation
or damage is found, within 24 months after the effective date of
this AD, do all applicable corrective actions, in accordance with
paragraph B, ``Procedure,'' of the Accomplishment Instructions of
MHI RJ Service Bulletin 670BA-25-135, Revision B, dated November 25,
2022. For this AD, damage includes dents or misshapen hooks that
attach the belt to the seat.
Note 1 to paragraph (g): Y-belts are also known as lap belts.
(h) Exceptions to Service Information
Where paragraph B, ``Procedure,'' of the Accomplishment
Instructions of MHI RJ Service Bulletin 670BA-25-135, Revision B,
dated November 25, 2022, specifies to ``refer to AMM'' replace those
words with ``in accordance with AMM.''
(i) Maintenance Task Prohibition
As of the effective date of this AD, it is prohibited to use MHI
RJ Aviation ULC Aircraft Maintenance Manual (AMM) task 25-21-04-400-
801, revision 69 or earlier.
(j) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using the service information
[[Page 23]]
identified in paragraph (j)(1) or (2) of this AD, provided the
actions were done using MHI RJ AMM Revision 70, dated May 25, 2022,
or Revision 71, dated December 16, 2022.
(1) MHI RJ Service Bulletin 670BA-25-135, dated June 1, 2022.
(2) MHI RJ Service Bulletin 670BA-25-135, Revision A, dated
August 30, 2022.
(k) 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 (l)(2) 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; 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.
(l) Additional Information
(1) Refer to Transport Canada AD CF-2023-10, dated February 17,
2023, for related information. This Transport Canada AD may be found
in the AD docket at regulations.gov under Docket No. FAA-2023-1823.
(2) 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].
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(3) and (4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) MHI RJ Service Bulletin 670BA-25-135, Revision B, dated
November 25, 2022.
(ii) [Reserved]
(3) For MHI RJ Aviation ULC 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 December 5, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-28801 Filed 12-29-23; 8:45 am]
BILLING CODE 4910-13-P