Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 1849-1851 [2024-00343]
Download as PDF
Federal Register / Vol. 89, No. 8 / Thursday, January 11, 2024 / Proposed Rules
Moines, WA 98198; phone: (781) 238–7743;
email: mehdi.lamnyi@faa.gov.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) CFM International, S.A. (CFM) Service
Bulletin LEAP–1A–72–00–0492–01A–930A–
D, Issue 001–00, dated April 6, 2023.
(ii) [Reserved]
(3) For service information identified in
this AD, contact CFM International, S.A.,
Aviation Operations Center, 1 Neumann
Way, M/D Room 285, Cincinnati, OH 45125;
phone: (877) 432–3272; email: fleetsupport@
ge.com.
(4) You may view this service information
at FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (817) 222–5110.
(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-locationsoremailfr.inspection@nara.gov.
Issued on January 5, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–00377 Filed 1–10–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–0026; Project
Identifier MCAI–2023–00776–T]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.)
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for all
MHI RJ Aviation ULC Model CL–600–
2E25 (Regional Jet Series 1000)
airplanes. This proposed AD was
prompted by a determination that new
or more restrictive airworthiness
limitations are necessary. This proposed
AD would require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
ddrumheller on DSK120RN23PROD with PROPOSALS1
SUMMARY:
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17:01 Jan 10, 2024
Jkt 262001
restrictive airworthiness limitations, as
specified in a Transport Canada AD,
which is proposed for incorporation by
reference (IBR). The FAA is proposing
this AD to address the unsafe condition
on these products.
DATES: The FAA must receive comments
on this proposed AD by February 26,
2024.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
regulations.gov. Follow the instructions
for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–0026; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this NPRM, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For Transport Canada material that
is proposed for IBR in this NPRM,
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. It is
also available at regulations.gov under
Docket No. FAA–2024–0026.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
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:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
PO 00000
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Sfmt 4702
1849
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2024–0026; Project Identifier
MCAI–2023–00776–T’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend this proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Fatin Saumik,
Aviation Safety Engineer, FAA, 1600
Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516–228–7300;
email 9-avs-nyaco-cos@faa.gov. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
Background
Transport Canada, which is the
aviation authority for Canada, has
issued AD CF–2023–43, dated June 21,
2023 (Transport Canada AD CF–2023–
43) (also referred to as the MCAI), to
correct an unsafe condition for all MHI
RJ Aviation ULC Model CL–600–2E25
(Regional Jet Series 1000) airplanes. The
MCAI states that new or more restrictive
airworthiness limitations have been
developed.
The FAA is proposing this AD to
prevent potential fatigue cracking and
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Federal Register / Vol. 89, No. 8 / Thursday, January 11, 2024 / Proposed Rules
damage in principal structural elements.
The unsafe condition, if not addressed,
could result in reduced structural
integrity of the airplane. You may
examine the MCAI in the AD docket at
regulations.gov under Docket No. FAA–
2024–0026.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Transport Canada
AD CF–2023–43, which specifies new or
more restrictive airworthiness
limitations for airplane structures and a
safe life limit. 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
ADDRESSES.
FAA’s Determination
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI referenced above. The FAA
is issuing this NPRM after determining
that the unsafe condition described
previously is likely to exist or develop
in other products of the same type
design.
ddrumheller on DSK120RN23PROD with PROPOSALS1
Proposed AD Requirements in This
NPRM
This proposed AD would require
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
airworthiness limitations, which are
specified in Transport Canada AD CF–
2023–43 described previously, as
incorporated by reference. Any
differences with Transport Canada AD
CF–2023–43 are identified as exceptions
in the regulatory text of this proposed
AD.
This proposed AD would require
revisions to certain operator
maintenance documents to include new
actions (e.g., inspections). Compliance
with these actions is required by 14 CFR
91.403(c). For airplanes that have been
previously modified, altered, or repaired
in the areas addressed by this proposed
AD, the operator may not be able to
accomplish the actions described in the
revisions. In this situation, to comply
with 14 CFR 91.403(c), the operator
must request approval for an alternative
method of compliance (AMOC)
according to paragraph (j)(1) of this
proposed AD.
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17:01 Jan 10, 2024
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Explanation of Required Compliance
Information
request an AMOC to use an alternative
action or interval.
In the FAA’s ongoing efforts to
improve the efficiency of the AD
process, the FAA developed a process to
use some civil aviation authority (CAA)
ADs as the primary source of
information for compliance with
requirements for corresponding FAA
ADs. The FAA has been coordinating
this process with manufacturers and
CAAs. As a result, the FAA proposes to
incorporate Transport Canada AD CF–
2023–43 by reference in the FAA final
rule. This proposed AD would,
therefore, require compliance with
Transport Canada AD CF–2023–43
through that incorporation, except for
any differences identified as exceptions
in the regulatory text of this proposed
AD. Service information required by
Transport Canada AD CF–2023–43 for
compliance will be available at
regulations.gov by searching for and
locating Docket No. FAA–2024–0026
after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 5
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
The FAA has determined that revising
the existing maintenance or inspection
program takes an average of 90 workhours 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).
Airworthiness Limitation ADs Using
the New Process
The FAA’s process of incorporating
by reference MCAI ADs as the primary
source of information for compliance
with corresponding FAA ADs has been
limited to certain MCAI ADs (primarily
those with service bulletins as the
primary source of information for
accomplishing the actions required by
the FAA AD). However, the FAA is now
expanding the process to include MCAI
ADs that require a change to
airworthiness limitation documents,
such as airworthiness limitation
sections.
For these ADs that incorporate by
reference an MCAI AD that changes
airworthiness limitations, the FAA
requirements are unchanged. Operators
must revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
the new airworthiness limitation
document. The airworthiness
limitations must be followed according
to 14 CFR 91.403(c) and 91.409(e).
The previous format of the
airworthiness limitation ADs included a
paragraph that specified that no
alternative actions (e.g., inspections) or
intervals may be used unless the actions
and intervals are approved as an AMOC
in accordance with the procedures
specified in the AMOC paragraph under
‘‘Additional AD Provisions.’’ This new
format includes a ‘‘New Provisions for
Alternative Actions and Intervals’’
paragraph that does not specifically
refer to AMOCs, but operators may still
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Fmt 4702
Sfmt 4702
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
Regulatory Findings
The FAA has determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would not have a significant
economic impact, positive or negative,
E:\FR\FM\11JAP1.SGM
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Federal Register / Vol. 89, No. 8 / Thursday, January 11, 2024 / Proposed Rules
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.):
Docket No. FAA–2024–0026; Project
Identifier MCAI–2023–00776–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by February 26,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all MHI RJ Aviation
ULC (Type Certificate previously held by
Bombardier, Inc.) Model CL–600–2E25
(Regional Jet Series 1000) airplanes,
certificated in any category.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time Limits/Maintenance
Checks.
ddrumheller on DSK120RN23PROD with PROPOSALS1
(e) Unsafe Condition
This AD was prompted by a determination
that new or more restrictive airworthiness
limitations are necessary. The FAA is issuing
this AD to prevent potential fatigue cracking
and damage in principal structural elements.
The unsafe condition, if not addressed, could
result in reduced structural integrity of the
airplane.
(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–
2023–43, dated June 21, 2023 (Transport
Canada AD CF–2023–43).
VerDate Sep<11>2014
17:01 Jan 10, 2024
Jkt 262001
(h) Exceptions to Transport Canada AD CF–
2023–43
(1) Where Transport Canada AD CF–2023–
43 refers to its effective date, this AD requires
using the effective date of this AD.
(2) Where paragraph 1. of Transport
Canada AD CF–2023–43 specifies to
‘‘incorporate the new and revised tasks
identified in Table 1 below, in the
appropriate chapter within Section 2 and
Section 3 of the MRM CSP B–053 Part 2
manual,’’ this AD requires replacing those
words with ‘‘revise the existing maintenance
or inspection program, as applicable, by
incorporating the new and revised tasks
identified in Table 1.’’
(3) The initial compliance time for doing
the tasks specified in paragraph 1. of
Transport Canada AD CF–2023–43 is at the
applicable ‘‘thresholds’’ and ‘‘discard times’’
as specified in the service information
referenced in paragraph 1. of Transport
Canada AD CF–2023–43, or within 60 days
after the effective date of this AD, whichever
occurs later.
(4) This AD does not adopt paragraph 2. of
Transport Canada AD CF–2023–43.
(i) Provisions for Alternative Actions and
Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) and
intervals are allowed unless they are
approved as specified in the provisions of the
‘‘Corrective Actions’’ section of Transport
Canada AD CF–2023–43.
(j) 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 (k) of this AD. Information may be
emailed to 9-AVS-NYACO-COS@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or Transport Canada; or MHI
RJ Aviation ULC’s Transport Canada Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(k) Additional Information
For more information about this AD,
contact Fatin Saumik, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@faa.gov.
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1851
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Transport Canada AD CF–2023–43,
dated June 21, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF–2023–43,
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 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 January 5, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–00343 Filed 1–10–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2023–2493; Airspace
Docket No. 23–AGL–25]
RIN 2120–AA66
Amendment of Jet Route J–89 and
VOR Federal Airway V–161, and
Establishment of Canadian RNAV
Routes Q–834 and T–765; Northcentral
United States
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
amend Jet Route J–89 and Very High
Frequency Omnidirectional Range
(VOR) Federal Airway V–161 and to
establish Canadian Area Navigation
(RNAV) routes Q–834 and T–765 in
United States (U.S.) airspace. The FAA
is proposing this action due to the
planned decommissioning of the
Winnipeg, Manitoba (MB), Canada,
SUMMARY:
E:\FR\FM\11JAP1.SGM
11JAP1
Agencies
[Federal Register Volume 89, Number 8 (Thursday, January 11, 2024)]
[Proposed Rules]
[Pages 1849-1851]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-00343]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-0026; Project Identifier MCAI-2023-00776-T]
RIN 2120-AA64
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all MHI RJ Aviation ULC Model CL-600-2E25 (Regional Jet Series
1000) airplanes. This proposed AD was prompted by a determination that
new or more restrictive airworthiness limitations are necessary. This
proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations, as specified in a Transport
Canada AD, which is proposed for incorporation by reference (IBR). The
FAA is proposing this AD to address the unsafe condition on these
products.
DATES: The FAA must receive comments on this proposed AD by February
26, 2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-0026; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For Transport Canada material that is proposed for IBR in
this NPRM, contact Transport Canada, Transport Canada National Aircraft
Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada;
telephone 888-663-3639; email [email protected]; website tc.canada.ca/en/aviation.
It is also available at regulations.gov under Docket No. FAA-2024-0026.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195.
FOR FURTHER INFORMATION CONTACT: Fatin Saumik, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-0026; Project Identifier
MCAI-2023-00776-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Fatin
Saumik, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected]. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
Transport Canada, which is the aviation authority for Canada, has
issued AD CF-2023-43, dated June 21, 2023 (Transport Canada AD CF-2023-
43) (also referred to as the MCAI), to correct an unsafe condition for
all MHI RJ Aviation ULC Model CL-600-2E25 (Regional Jet Series 1000)
airplanes. The MCAI states that new or more restrictive airworthiness
limitations have been developed.
The FAA is proposing this AD to prevent potential fatigue cracking
and
[[Page 1850]]
damage in principal structural elements. The unsafe condition, if not
addressed, could result in reduced structural integrity of the
airplane. You may examine the MCAI in the AD docket at regulations.gov
under Docket No. FAA-2024-0026.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Transport Canada AD CF-2023-43, which specifies
new or more restrictive airworthiness limitations for airplane
structures and a safe life limit. 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
ADDRESSES.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA is issuing this NPRM after determining that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations, which are specified in Transport
Canada AD CF-2023-43 described previously, as incorporated by
reference. Any differences with Transport Canada AD CF-2023-43 are
identified as exceptions in the regulatory text of this proposed AD.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance (AMOC) according to
paragraph (j)(1) of this proposed AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate Transport Canada AD CF-2023-43 by reference
in the FAA final rule. This proposed AD would, therefore, require
compliance with Transport Canada AD CF-2023-43 through that
incorporation, except for any differences identified as exceptions in
the regulatory text of this proposed AD. Service information required
by Transport Canada AD CF-2023-43 for compliance will be available at
regulations.gov by searching for and locating Docket No. FAA-2024-0026
after the FAA final rule is published.
Airworthiness Limitation ADs Using the New Process
The FAA's process of incorporating by reference MCAI ADs as the
primary source of information for compliance with corresponding FAA ADs
has been limited to certain MCAI ADs (primarily those with service
bulletins as the primary source of information for accomplishing the
actions required by the FAA AD). However, the FAA is now expanding the
process to include MCAI ADs that require a change to airworthiness
limitation documents, such as airworthiness limitation sections.
For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged.
Operators must revise the existing maintenance or inspection program,
as applicable, to incorporate the information specified in the new
airworthiness limitation document. The airworthiness limitations must
be followed according to 14 CFR 91.403(c) and 91.409(e).
The previous format of the airworthiness limitation ADs included a
paragraph that specified that no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and intervals
are approved as an AMOC in accordance with the procedures specified in
the AMOC paragraph under ``Additional AD Provisions.'' This new format
includes a ``New Provisions for Alternative Actions and Intervals''
paragraph that does not specifically refer to AMOCs, but operators may
still request an AMOC to use an alternative action or interval.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 5 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
The FAA has determined that revising the existing 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
The FAA has determined that this proposed AD would not have
federalism implications under Executive Order 13132. This proposed AD
would not have a substantial direct effect on the States, on the
relationship between the national Government and the States, or on the
distribution of power and responsibilities among the various levels of
government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative,
[[Page 1851]]
on a substantial number of small entities under the criteria of the
Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier,
Inc.): Docket No. FAA-2024-0026; Project Identifier MCAI-2023-00776-
T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 26, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all MHI RJ Aviation ULC (Type Certificate
previously held by Bombardier, Inc.) Model CL-600-2E25 (Regional Jet
Series 1000) airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Unsafe Condition
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to prevent potential fatigue cracking and damage in
principal structural elements. The unsafe condition, if not
addressed, could result in reduced structural integrity of the
airplane.
(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-2023-43, dated June 21, 2023
(Transport Canada AD CF-2023-43).
(h) Exceptions to Transport Canada AD CF-2023-43
(1) Where Transport Canada AD CF-2023-43 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where paragraph 1. of Transport Canada AD CF-2023-43
specifies to ``incorporate the new and revised tasks identified in
Table 1 below, in the appropriate chapter within Section 2 and
Section 3 of the MRM CSP B-053 Part 2 manual,'' this AD requires
replacing those words with ``revise the existing maintenance or
inspection program, as applicable, by incorporating the new and
revised tasks identified in Table 1.''
(3) The initial compliance time for doing the tasks specified in
paragraph 1. of Transport Canada AD CF-2023-43 is at the applicable
``thresholds'' and ``discard times'' as specified in the service
information referenced in paragraph 1. of Transport Canada AD CF-
2023-43, or within 60 days after the effective date of this AD,
whichever occurs later.
(4) This AD does not adopt paragraph 2. of Transport Canada AD
CF-2023-43.
(i) Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals are allowed unless they
are approved as specified in the provisions of the ``Corrective
Actions'' section of Transport Canada AD CF-2023-43.
(j) 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 (k) of this AD. Information may be emailed to 9-AVS-
[email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or Transport Canada; or MHI RJ Aviation
ULC's Transport Canada Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(k) 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].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Transport Canada AD CF-2023-43, dated June 21, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF-2023-43, contact Transport
Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-
3639; email [email protected]; website tc.canada.ca/en/
aviation.
(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 January 5, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-00343 Filed 1-10-24; 8:45 am]
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