Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes, 3716-3719 [2022-01352]
Download as PDF
3716
Federal Register / Vol. 87, No. 16 / Tuesday, January 25, 2022 / Proposed Rules
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–0011; Project
Identifier MCAI–2021–00485–T]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.)
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain MHI RJ Aviation ULC Model
CL–600–2B19 (Regional Jet Series 100 &
440) airplanes, Model CL–600–2C10
(Regional Jet Series 700, 701 & 702)
airplanes, Model CL–600–2C11
(Regional Jet Series 550) airplanes,
Model CL–600–2D15 (Regional Jet
Series 705) airplanes, Model CL–600–
2D24 (Regional Jet Series 900) airplanes,
and Model CL–600–2E25 (Regional Jet
Series 1000) airplanes. This proposed
AD was prompted by reports of
corrosion on fuel clamshell couplings
installed in the fuel tank, and a
determination that new or more
restrictive airworthiness limitations are
necessary. This proposed AD would
require removing and replacing the fuel
clamshell couplings on certain
airplanes, and revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations.
The FAA is proposing this AD to
address the unsafe condition on these
products.
SUMMARY:
The FAA must receive comments
on this proposed AD by March 11, 2022.
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
https://www.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.
For service information identified in
this NPRM, contact MHI RJ Aviation
khammond on DSKJM1Z7X2PROD with PROPOSALS
DATES:
VerDate Sep<11>2014
16:04 Jan 24, 2022
Jkt 256001
ULC, 12655 Henri-Fabre Blvd., Mirabel,
Que´bec J7N 1E1 Canada; Widebody
Customer Response Center North
America toll-free telephone +1–844–
272–2720 or direct-dial telephone +1–
514–855–8500; fax +1–514–855–8501;
email thd.crj@mhirj.com; internet
https://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.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2022–
0011; 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, any
comments received, and other
information. The street address for
Docket Operations is listed above.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Jiwan Karunatilake, Aerospace
Engineer, Airframe and Propulsion
Section, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; fax 516–794–5531; email 9avs-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
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2022–0011; Project Identifier
MCAI–2021–00485–T’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend the proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this proposed
AD.
PO 00000
Frm 00018
Fmt 4702
Sfmt 4702
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 Jiwan Karunatilake,
Aerospace Engineer, Airframe and
Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590;
telephone 516–228–7300; fax 516–794–
5531; 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.
Discussion
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued TCCA AD CF–
2021–16, dated April 26, 2021 (TCCA
AD CF–2021–16) (also referred to after
this as the Mandatory Continuing
Airworthiness Information, or the
MCAI), to correct an unsafe condition
for certain MHI RJ Aviation ULC Model
CL–600–2B19 (Regional Jet Series 100 &
440) airplanes, Model CL–600–2C10
(Regional Jet Series 700, 701 & 702)
airplanes, Model CL–600–2C11
(Regional Jet Series 550) airplanes,
Model CL–600–2D15 (Regional Jet
Series 705) airplanes, Model CL–600–
2D24 (Regional Jet Series 900) airplanes,
and Model CL–600–2E25 (Regional Jet
Series 1000) airplanes. You may
examine the MCAI in the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2022–
0011.
This proposed AD was prompted by
reports of corrosion on fuel clamshell
couplings installed in the fuel tank, and
a determination that new or more
restrictive airworthiness limitations are
necessary. The FAA is proposing this
AD to address corroded fuel clamshell
couplings in the fuel tank, which, if not
removed and replaced, could reduce the
ability of the fuel coupling to conduct
E:\FR\FM\25JAP1.SGM
25JAP1
Federal Register / Vol. 87, No. 16 / Tuesday, January 25, 2022 / Proposed Rules
lightning current and possibly lead to
arcing and subsequent fuel tank ignition
in the event of a lightning strike. See the
MCAI for additional background
information.
Related Service Information Under 1
CFR Part 51
MHI RJ Aviation has issued Service
Bulletin 601R–28–068, Revision A,
dated December 21, 2020; and Service
Bulletin 670BA–28–041, Revision B,
dated January 27, 2021. This service
information describes procedures for
removing and replacing the fuel
clamshell couplings. These documents
are distinct because they apply to
different airplane models.
MHI RJ Aviation has also issued
Temporary Revision (TR) 2S4–002,
dated September 1, 2021. This service
information describes a Critical Design
Configuration Control Limitations
(CDCCL) item for bonding of fuel and
vent lines for lightning protection to
preclude a spark.
MHI RJ Aviation has also issued the
following TRs, which describe
airworthiness limitations for fuel tank
systems.
• TR 2S4–003, dated September 1,
2021; CRJ Series Regional Jet TR ALI–
0741, dated October 13, 2020; and
CRJ700/900/1000 Series Regional Jet TR
ALI–0751, dated April 8, 2021, describe
a procedure for removing and replacing
self-bonding couplings in the fuel tank.
• CRJ Series Regional Jet TR ALI–
0740, dated October 13, 2020, describes
a CDCCL item for bonding of fuel and
vent lines for lightning protection to
preclude a spark.
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.
FAA’s Determination
These products have been approved
by the aviation authority of another
country, and are approved for operation
in the United States. Pursuant to the
FAA’s bilateral agreement with the State
of Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI and service information
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 these same type designs.
Proposed Requirements of This NPRM
This proposed AD would require
removing and replacing the fuel
clamshell couplings on certain airplanes
and revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
airworthiness limitations.
This proposed AD would require
revisions to certain operator
maintenance documents to include new
actions (e.g., inspections) and CDCCLs.
Compliance with these actions and
CDCCLs 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 according to
paragraph (m)(1) of this proposed AD.
Differences Between This Proposed AD
and the MCAI or Service Information
The MCAI specifies to revise the
CDCCL Items as introduced by
Bombardier CL–600–2B19 TR 2D–009,
dated October 24, 2020, in Appendix
D—Fuel Systems Limitations of Part 2,
Airworthiness Requirements, of the MHI
RJ Maintenance Requirements Manual
(MRM). This proposed AD does not
require this action because the TR
references Appendix D—Fuel Systems
Limitations of Part 2, Airworthiness
Requirements, of the MHI RJ MRM,
3717
which is not applicable to U.S.
airplanes. As a result, this proposed AD
would require that the information
specified in MHI RJ TR 2S4–002, dated
September 1, 2021, is incorporated into
Supplement 4—FAA Fuel System
Limitations of Part 2, Airworthiness
Requirements, of the MHI RJ MRM as
required by paragraph (h)(1) of this
proposed AD. MHI RJ TR 2S4–002,
dated September 1, 2021, addresses the
unsafe condition with references that
apply to U.S. airplanes and provides the
same or better level of safety.
The MCAI also specifies to
incorporate the new Fuel System
Limitation Task 28–23–00–605 as
introduced by Bombardier CL–600–
2B19 TR 2D–008, dated October 24,
2020; and to revise the Task Description
Effectivity as amended by Bombardier
CL–600–2B19 TR 2D–010, dated April
8, 2021; in Appendix D—Fuel Systems
Limitations of Part 2, Airworthiness
Requirements, of the MHI RJ MRM. This
proposed AD does not require these
actions because these TRs also reference
Appendix D—Fuel Systems Limitations
of Part 2, Airworthiness Requirements,
of the MHI RJ MRM, which is not
applicable to U.S. airplanes. As a result,
this proposed AD would require that the
information specified in MHI RJ TR
2S4–003, dated September 1, 2021, is
incorporated into Supplement 4—FAA
Fuel System Limitations of Part 2,
Airworthiness Requirements, of the MHI
RJ MRM, as specified in paragraph (h)(2)
of this proposed AD. MHI RJ TR 2S4–
003, dated September 1, 2021, addresses
the unsafe condition with references
that apply to U.S. airplanes and
provides the same or better level of
safety.
Costs of Compliance
The FAA estimates that this proposed
AD affects 914 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS *
Labor cost
Parts cost
Cost per
product
Up to 21 work-hours × $85 per hour = $1,785 ...............................................................
Up to $5,837 ..
Up to $7,622 ..
Cost on U.S.
operators
Up to $6,966,508.
khammond on DSKJM1Z7X2PROD with PROPOSALS
* Table does not include estimated costs for revising the maintenance/inspection program.
The FAA has determined that revising
the maintenance or inspection program
takes an average of 90 work-hours per
operator, although the FAA recognizes
that this number may vary from operator
to operator. In the past, the FAA has
estimated that this action takes 1 workhour per airplane. Since operators
VerDate Sep<11>2014
16:04 Jan 24, 2022
Jkt 256001
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 FAA estimates the total cost per
operator to be $7,650 (90 work-hours ×
$85 per work-hour).
PO 00000
Frm 00019
Fmt 4702
Sfmt 4702
According to the manufacturer, some
or all of the costs of this proposed AD
may be covered under warranty, thereby
reducing the cost impact on affected
individuals. The FAA does not control
warranty coverage for affected
individuals. As a result, the FAA has
E:\FR\FM\25JAP1.SGM
25JAP1
3718
Federal Register / Vol. 87, No. 16 / Tuesday, January 25, 2022 / Proposed Rules
§ 39.13
included all known costs in the cost
estimate.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
Regulatory Findings
The FAA determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
khammond on DSKJM1Z7X2PROD with PROPOSALS
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.
VerDate Sep<11>2014
16:04 Jan 24, 2022
Jkt 256001
[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–2022–0011; Project
Identifier MCAI–2021–00485–T.
(a) Comments Due Date
The FAA must receive comments by March
11, 2022.
(b) Affected Airworthiness Directives (ADs)
None.
(c) Applicability
This AD applies to the MHI RJ Aviation
ULC airplanes, certificated in any category,
identified in paragraphs (c)(1) through (4) of
this AD.
(1) Model CL–600–2B19 (Regional Jet
Series 100 & 440) airplanes, serial numbers
7002 through 7990 inclusive and 8000
through 8112 inclusive.
(2) Model CL–600–2C10 (Regional Jet
Series 700, 701 & 702) and CL–600–2C11
(Regional Jet Series 550) airplanes, serial
numbers 10002 through 10347 inclusive.
(3) Model CL–600–2D15 (Regional Jet
Series 705) and CL–600–2D24 (Regional Jet
Series 900) airplanes, serial numbers 15001
through 15499 inclusive.
(4) Model CL–600–2E25 (Regional Jet
Series 1000) airplanes, serial numbers 19001
through 19064 inclusive.
(d) Subject
Air Transport Association (ATA) of
America Code 28, Fuel.
(e) Reason
This AD was prompted by reports of
corrosion on fuel clamshell couplings
installed in the fuel tank, and a
determination that new or more restrictive
airworthiness limitations are necessary. The
FAA is issuing this AD to address corroded
fuel clamshell couplings in the fuel tank,
which, if not removed and replaced, could
reduce the ability of the fuel coupling to
conduct lightning current and possibly lead
to arcing and subsequent fuel tank ignition in
the event of a lightning strike.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
revise the existing maintenance or inspection
program, as applicable, to incorporate the
information specified in paragraphs (h)(1)
and (2) of this AD into Supplement 4—FAA
Fuel System Limitations of Part 2,
Airworthiness Requirements, of the MHI RJ
Maintenance Requirements Manual (MRM).
(1) Critical Design Configuration Control
Limitation (CDCCL) Item as specified in MHI
RJ Temporary Revision (TR) 2S4–002, dated
September 1, 2021.
(2) Fuel System Limitation Task 28–23–00–
605 as specified in MHI RJ TR 2S4–003,
dated September 1, 2021.
(i) Clamshell Coupling Replacement: Model
CL–600–2C10, CL–600–2C11, CL–600–2D15,
CL–600–2D24, and CL–600–2E25 Airplanes
For Model CL–600–2C10 and CL–600–
2C11 airplanes; Model CL–600–2D15 and
CL–600–2D24 airplanes, serial numbers
15001 through 15494 inclusive; and Model
CL–600–2E25 airplanes: Within 8,800 flight
hours or 48 months, whichever occurs first
after the effective date of this AD, replace the
fuel clamshell couplings, in accordance with
Section 2.B. of the Accomplishment
Instructions of MHI RJ Service Bulletin
670BA–28–041, Revision B, dated January
27, 2021.
(j) Revision of the Existing Maintenance or
Inspection Program: Model CL–600–2C10,
CL–600–2C11, CL–600–2D15, CL–600–2D24,
and CL–600–2E25 Airplanes
For Model CL–600–2C10, CL–600–2C11,
CL–600–2D15, CL–600–2D24, and CL–600–
2E25 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 paragraphs (j)(1) and (2) of this
AD.
(1) Fuel System Limitation Task 28–21–15–
601 as specified in [MHI RJ] CRJ Series
Regional Jet TR ALI–0741, dated October 13,
2020; and Description Applicability for
Airworthiness Limitation Task 28–21–15–
601 as amended by [MHI RJ] CRJ700/900/
1000 Series Regional Jet TR ALI–0751, dated
April 8, 2021; in Section 4–28 of Part 2,
Airworthiness Requirements, of the MHI RJ
MRM.
(2) CDCCL Item as specified in [MHI RJ]
CRJ Series Regional Jet TR ALI–0740, dated
October 13, 2020, in Section 5–00 of Part 2,
Airworthiness Requirements, of the MHI RJ
MRM.
(g) Clamshell Coupling Replacement: Model
CL–600–2B19 Airplanes
For Model CL–600–2B19 airplanes: Within
6,600 flight hours or 36 months, whichever
occurs first after the effective date of this AD,
remove and replace the fuel clamshell
couplings, in accordance with Section 2.B. of
the Accomplishment Instructions of MHI RJ
Service Bulletin 601R–28–068, Revision A,
dated December 21, 2020.
(k) No Alternative Actions, Intervals, or
CDCCLs
After the existing maintenance or
inspection program has been revised as
required by paragraphs (h) and (j) of this AD,
no alternative actions (e.g., inspections),
intervals, or CDCCLs may be used unless the
actions, intervals, and CDCCLs are approved
as an alternative method of compliance
(AMOC) in accordance with the procedures
specified in paragraph (m)(1) of this AD.
(h) Revision of the Existing Maintenance or
Inspection Program: Model CL–600–2B19
Airplanes
For Model CL–600–2B19 airplanes: Within
60 days after the effective date of this AD,
(l) Credit for Previous Actions
(1) 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 MHI RJ
PO 00000
Frm 00020
Fmt 4702
Sfmt 4702
E:\FR\FM\25JAP1.SGM
25JAP1
Federal Register / Vol. 87, No. 16 / Tuesday, January 25, 2022 / Proposed Rules
Service Bulletin 601R–28–068, dated
December 3, 2020.
(2) This paragraph provides credit for
actions required by paragraph (i) of this AD,
if those actions were performed before the
effective date of this AD using MHI RJ
Service Bulletin 670BA–28–041, dated
December 3, 2020; or Revision A, dated
December 21, 2020.
Issued on January 19, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–01352 Filed 1–24–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF THE TREASURY
(m) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York ACO
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, New
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
516–228–7300; fax 516–794–5531. 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, New York ACO Branch,
FAA; or Transport Canada Civil Aviation
(TCCA); or MHI RJ Aviation ULC’s TCCA
Design Approval Organization (DAO). If
approved by the DAO, the approval must
include the DAO-authorized signature.
khammond on DSKJM1Z7X2PROD with PROPOSALS
(n) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) TCCA AD
CF–2021–16, dated April 26, 2021, for related
information. This MCAI may be found in the
AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2022–0011.
(2) For more information about this AD,
contact Jiwan Karunatilake, Aerospace
Engineer, Airframe and Propulsion Section,
FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590;
telephone 516–228–7300; fax 516–794–5531;
email 9-avs-nyaco-cos@faa.gov.
(3) For service information identified in
this AD, contact MHI RJ Aviation ULC, 12655
Henri-Fabre Blvd., Mirabel, Que´bec J7N 1E1
Canada; Widebody Customer Response
Center North America toll-free telephone +1–
844–272–2720 or direct-dial telephone +1–
514–855–8500; fax +1–514–855–8501; email
thd.crj@mhirj.com; internet https://
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.
VerDate Sep<11>2014
16:04 Jan 24, 2022
Jkt 256001
Financial Crimes Enforcement Network
31 CFR Part 1010
Pilot Program on Sharing of
Suspicious Activity Reports and
Related Information With Foreign
Branches, Subsidiaries, and Affiliates
Financial Crimes Enforcement
Network (FinCEN), Treasury.
ACTION: Notice of proposed rulemaking.
AGENCY:
FinCEN is issuing this notice
of proposed rulemaking to seek public
comment on the proposed establishment
of a limited-duration pilot program,
subject to conditions set by FinCEN, to
permit a financial institution with a
suspicious activity report (SAR)
reporting obligation to share SARs and
information related to SARs with the
institution’s foreign branches,
subsidiaries, and affiliates for the
purpose of combating illicit finance risk,
in accordance with Section 6212(a) of
the Anti-Money Laundering Act of 2020
(AML Act).
DATES: Written comments on this
proposed rule must be received on or
before March 28, 2022.
ADDRESSES: Comments may be
submitted by any of the following
methods:
• Federal E-rulemaking Portal: https://
www.regulations.gov. Follow the
instructions for submitting comments.
Refer to Docket Number FINCEN–2022–
0002 and RIN 1506–AB51.
• Mail: Policy Division, Financial
Crimes Enforcement Network, P.O. Box
39, Vienna, VA 22183. Refer to Docket
Number FINCEN–2022–0002 and RIN
1506–AB51.
FOR FURTHER INFORMATION CONTACT: The
FinCEN Regulatory Support Section at
1–800–767–2825 or electronically at
https://fincen.gov/contact.
SUPPLEMENTARY INFORMATION:
SUMMARY:
I. Scope of Notice of Proposed
Rulemaking (NPRM)
FinCEN is issuing this NPRM
pursuant to 31 U.S.C. 5318(g)(8), as
added by section 6212 of the AML Act,1
1 The AML Act was enacted as Division F,
sections 6001–6511, of the William M. (Mac)
Frm 00021
Fmt 4702
which requires the Secretary of the
Treasury (the Secretary) to issue rules
establishing a pilot program that permits
a financial institution subject to a SAR
reporting requirement under 31 U.S.C.
5318(g) to share SARs and related
information, including the fact that a
SAR has been filed, with the
institution’s foreign branches,
subsidiaries, and affiliates for the
purpose of combating illicit finance
risks.2
II. Background
RIN 1506–AB51
PO 00000
3719
Sfmt 4702
A. The Bank Secrecy Act (BSA)
Enacted in 1970 and amended most
recently by the AML Act, the BSA aids
in the prevention of money laundering,
terrorism financing, and other illicit
financial activity, and the protection of
U.S. national security.3 The purposes of
the BSA include, among other things,
‘‘requir[ing] certain reports or records
that are highly useful in—(A) criminal,
tax, or regulatory investigations, risk
assessments, or proceedings; or (B)
intelligence or counterintelligence
activities, including analysis, to protect
against terrorism’’ and ‘‘establish[ing]
appropriate frameworks for information
sharing’’ among financial institutions
and government authorities, among
others.4
The Secretary is authorized to require
domestic financial institutions or
nonfinancial trades or businesses to
maintain appropriate procedures to
ensure compliance with the BSA and
the regulations promulgated thereunder
or to guard against money laundering,
the financing of terrorism, and other
forms of illicit finance.5 The Secretary
has delegated to the Director of FinCEN
the authority to implement, administer,
and enforce compliance with the BSA
and associated regulations.6
The BSA authorizes the Secretary to
require the reporting of suspicious
Thornberry National Defense Authorization Act for
Fiscal Year 2021, Public Law 116–283, 134 Stat
3388 (2021).
2 For purposes of this NPRM, ‘‘SARs and related
information’’ means a report filed pursuant to 31
U.S.C. 5318(g) and any information that would
reveal the existence of such a report. Because SARs
filed on insider abuse are filed under Federal
banking agency regulations (see, e.g., 12 CFR
21.11(c)(1)), and are not part of FinCEN’s SAR
regulations, they are not included in this definition
and are not permitted to be shared under the pilot
program FinCEN is proposing to establish by this
NPRM.
3 The BSA is codified at 12 U.S.C. 1829b, 1951–
1959 and 31 U.S.C. 5311–5314, 5316–5336.
Implementing regulations are codified at 31 CFR
Chapter X. Section 6212 of the AML Act amends
31 U.S.C. 5318 by adding Section 5318(g)(8).
4 31 U.S.C. 5311(1), (5).
5 31 U.S.C. 5318(a)(2).
6 31 U.S.C. 310(b)(2); Treasury Order 180–01,
(Jan. 14, 2020).
E:\FR\FM\25JAP1.SGM
25JAP1
Agencies
[Federal Register Volume 87, Number 16 (Tuesday, January 25, 2022)]
[Proposed Rules]
[Pages 3716-3719]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-01352]
[[Page 3716]]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0011; Project Identifier MCAI-2021-00485-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 certain MHI RJ Aviation ULC Model CL-600-2B19 (Regional Jet Series
100 & 440) airplanes, Model CL-600-2C10 (Regional Jet Series 700, 701 &
702) airplanes, Model CL-600-2C11 (Regional Jet Series 550) airplanes,
Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-
2D24 (Regional Jet Series 900) airplanes, and Model CL-600-2E25
(Regional Jet Series 1000) airplanes. This proposed AD was prompted by
reports of corrosion on fuel clamshell couplings installed in the fuel
tank, and a determination that new or more restrictive airworthiness
limitations are necessary. This proposed AD would require removing and
replacing the fuel clamshell couplings on certain airplanes, and
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations. 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 March 11,
2022.
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 https://www.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.
For service information identified in this NPRM, contact MHI RJ
Aviation ULC, 12655 Henri-Fabre Blvd., Mirabel, Qu[eacute]bec J7N 1E1
Canada; Widebody Customer Response Center North America toll-free
telephone +1-844-272-2720 or direct-dial telephone +1-514-855-8500; fax
+1-514-855-8501; email [email protected]; internet https://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.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-
0011; 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, any comments received, and other information. The street
address for Docket Operations is listed above. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Jiwan Karunatilake, Aerospace
Engineer, Airframe and Propulsion Section, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-
7300; fax 516-794-5531; 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-2022-0011; Project Identifier
MCAI-2021-00485-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this proposed AD.
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 Jiwan
Karunatilake, Aerospace Engineer, Airframe and Propulsion Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7300; fax 516-794-5531; 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.
Discussion
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2021-16, dated April 26,
2021 (TCCA AD CF-2021-16) (also referred to after this as the Mandatory
Continuing Airworthiness Information, or the MCAI), to correct an
unsafe condition for certain MHI RJ Aviation ULC Model CL-600-2B19
(Regional Jet Series 100 & 440) airplanes, Model CL-600-2C10 (Regional
Jet Series 700, 701 & 702) airplanes, Model CL-600-2C11 (Regional Jet
Series 550) airplanes, Model CL-600-2D15 (Regional Jet Series 705)
airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and
Model CL-600-2E25 (Regional Jet Series 1000) airplanes. You may examine
the MCAI in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-
0011.
This proposed AD was prompted by reports of corrosion on fuel
clamshell couplings installed in the fuel tank, and a determination
that new or more restrictive airworthiness limitations are necessary.
The FAA is proposing this AD to address corroded fuel clamshell
couplings in the fuel tank, which, if not removed and replaced, could
reduce the ability of the fuel coupling to conduct
[[Page 3717]]
lightning current and possibly lead to arcing and subsequent fuel tank
ignition in the event of a lightning strike. See the MCAI for
additional background information.
Related Service Information Under 1 CFR Part 51
MHI RJ Aviation has issued Service Bulletin 601R-28-068, Revision
A, dated December 21, 2020; and Service Bulletin 670BA-28-041, Revision
B, dated January 27, 2021. This service information describes
procedures for removing and replacing the fuel clamshell couplings.
These documents are distinct because they apply to different airplane
models.
MHI RJ Aviation has also issued Temporary Revision (TR) 2S4-002,
dated September 1, 2021. This service information describes a Critical
Design Configuration Control Limitations (CDCCL) item for bonding of
fuel and vent lines for lightning protection to preclude a spark.
MHI RJ Aviation has also issued the following TRs, which describe
airworthiness limitations for fuel tank systems.
TR 2S4-003, dated September 1, 2021; CRJ Series Regional
Jet TR ALI-0741, dated October 13, 2020; and CRJ700/900/1000 Series
Regional Jet TR ALI-0751, dated April 8, 2021, describe a procedure for
removing and replacing self-bonding couplings in the fuel tank.
CRJ Series Regional Jet TR ALI-0740, dated October 13,
2020, describes a CDCCL item for bonding of fuel and vent lines for
lightning protection to preclude a spark.
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.
FAA's Determination
These products have been approved by the aviation authority of
another country, and are approved for operation in the United States.
Pursuant to the FAA's bilateral agreement with the State of Design
Authority, it has notified the FAA of the unsafe condition described in
the MCAI and service information 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 these
same type designs.
Proposed Requirements of This NPRM
This proposed AD would require removing and replacing the fuel
clamshell couplings on certain airplanes and revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections) and
CDCCLs. Compliance with these actions and CDCCLs 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 according to
paragraph (m)(1) of this proposed AD.
Differences Between This Proposed AD and the MCAI or Service
Information
The MCAI specifies to revise the CDCCL Items as introduced by
Bombardier CL-600-2B19 TR 2D-009, dated October 24, 2020, in Appendix
D--Fuel Systems Limitations of Part 2, Airworthiness Requirements, of
the MHI RJ Maintenance Requirements Manual (MRM). This proposed AD does
not require this action because the TR references Appendix D--Fuel
Systems Limitations of Part 2, Airworthiness Requirements, of the MHI
RJ MRM, which is not applicable to U.S. airplanes. As a result, this
proposed AD would require that the information specified in MHI RJ TR
2S4-002, dated September 1, 2021, is incorporated into Supplement 4--
FAA Fuel System Limitations of Part 2, Airworthiness Requirements, of
the MHI RJ MRM as required by paragraph (h)(1) of this proposed AD. MHI
RJ TR 2S4-002, dated September 1, 2021, addresses the unsafe condition
with references that apply to U.S. airplanes and provides the same or
better level of safety.
The MCAI also specifies to incorporate the new Fuel System
Limitation Task 28-23-00-605 as introduced by Bombardier CL-600-2B19 TR
2D-008, dated October 24, 2020; and to revise the Task Description
Effectivity as amended by Bombardier CL-600-2B19 TR 2D-010, dated April
8, 2021; in Appendix D--Fuel Systems Limitations of Part 2,
Airworthiness Requirements, of the MHI RJ MRM. This proposed AD does
not require these actions because these TRs also reference Appendix D--
Fuel Systems Limitations of Part 2, Airworthiness Requirements, of the
MHI RJ MRM, which is not applicable to U.S. airplanes. As a result,
this proposed AD would require that the information specified in MHI RJ
TR 2S4-003, dated September 1, 2021, is incorporated into Supplement
4--FAA Fuel System Limitations of Part 2, Airworthiness Requirements,
of the MHI RJ MRM, as specified in paragraph (h)(2) of this proposed
AD. MHI RJ TR 2S4-003, dated September 1, 2021, addresses the unsafe
condition with references that apply to U.S. airplanes and provides the
same or better level of safety.
Costs of Compliance
The FAA estimates that this proposed AD affects 914 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:
Estimated Costs for Required Actions *
----------------------------------------------------------------------------------------------------------------
Labor cost Parts cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 21 work-hours x $85 per Up to $5,837.......... Up to $7,622.......... Up to $6,966,508.
hour = $1,785.
----------------------------------------------------------------------------------------------------------------
* Table does not include estimated costs for revising the maintenance/inspection program.
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
FAA recognizes that this number may vary from operator to operator. In
the past, the FAA has estimated that this action takes 1 work-hour per
airplane. 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 FAA estimates the total cost per operator to be $7,650
(90 work-hours x $85 per work-hour).
According to the manufacturer, some or all of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected individuals. The FAA does not control warranty
coverage for affected individuals. As a result, the FAA has
[[Page 3718]]
included all known costs in the cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier,
Inc.): Docket No. FAA-2022-0011; Project Identifier MCAI-2021-00485-
T.
(a) Comments Due Date
The FAA must receive comments by March 11, 2022.
(b) Affected Airworthiness Directives (ADs)
None.
(c) Applicability
This AD applies to the MHI RJ Aviation ULC airplanes,
certificated in any category, identified in paragraphs (c)(1)
through (4) of this AD.
(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes,
serial numbers 7002 through 7990 inclusive and 8000 through 8112
inclusive.
(2) Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) and
CL-600-2C11 (Regional Jet Series 550) airplanes, serial numbers
10002 through 10347 inclusive.
(3) Model CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24
(Regional Jet Series 900) airplanes, serial numbers 15001 through
15499 inclusive.
(4) Model CL-600-2E25 (Regional Jet Series 1000) airplanes,
serial numbers 19001 through 19064 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 28, Fuel.
(e) Reason
This AD was prompted by reports of corrosion on fuel clamshell
couplings installed in the fuel tank, and a determination that new
or more restrictive airworthiness limitations are necessary. The FAA
is issuing this AD to address corroded fuel clamshell couplings in
the fuel tank, which, if not removed and replaced, could reduce the
ability of the fuel coupling to conduct lightning current and
possibly lead to arcing and subsequent fuel tank ignition in the
event of a lightning strike.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Clamshell Coupling Replacement: Model CL-600-2B19 Airplanes
For Model CL-600-2B19 airplanes: Within 6,600 flight hours or 36
months, whichever occurs first after the effective date of this AD,
remove and replace the fuel clamshell couplings, in accordance with
Section 2.B. of the Accomplishment Instructions of MHI RJ Service
Bulletin 601R-28-068, Revision A, dated December 21, 2020.
(h) Revision of the Existing Maintenance or Inspection Program: Model
CL-600-2B19 Airplanes
For Model CL-600-2B19 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 paragraphs (h)(1) and (2) of this AD into Supplement
4--FAA Fuel System Limitations of Part 2, Airworthiness
Requirements, of the MHI RJ Maintenance Requirements Manual (MRM).
(1) Critical Design Configuration Control Limitation (CDCCL)
Item as specified in MHI RJ Temporary Revision (TR) 2S4-002, dated
September 1, 2021.
(2) Fuel System Limitation Task 28-23-00-605 as specified in MHI
RJ TR 2S4-003, dated September 1, 2021.
(i) Clamshell Coupling Replacement: Model CL-600-2C10, CL-600-2C11, CL-
600-2D15, CL-600-2D24, and CL-600-2E25 Airplanes
For Model CL-600-2C10 and CL-600-2C11 airplanes; Model CL-600-
2D15 and CL-600-2D24 airplanes, serial numbers 15001 through 15494
inclusive; and Model CL-600-2E25 airplanes: Within 8,800 flight
hours or 48 months, whichever occurs first after the effective date
of this AD, replace the fuel clamshell couplings, in accordance with
Section 2.B. of the Accomplishment Instructions of MHI RJ Service
Bulletin 670BA-28-041, Revision B, dated January 27, 2021.
(j) Revision of the Existing Maintenance or Inspection Program: Model
CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25
Airplanes
For Model CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24,
and CL-600-2E25 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
paragraphs (j)(1) and (2) of this AD.
(1) Fuel System Limitation Task 28-21-15-601 as specified in
[MHI RJ] CRJ Series Regional Jet TR ALI-0741, dated October 13,
2020; and Description Applicability for Airworthiness Limitation
Task 28-21-15-601 as amended by [MHI RJ] CRJ700/900/1000 Series
Regional Jet TR ALI-0751, dated April 8, 2021; in Section 4-28 of
Part 2, Airworthiness Requirements, of the MHI RJ MRM.
(2) CDCCL Item as specified in [MHI RJ] CRJ Series Regional Jet
TR ALI-0740, dated October 13, 2020, in Section 5-00 of Part 2,
Airworthiness Requirements, of the MHI RJ MRM.
(k) No Alternative Actions, Intervals, or CDCCLs
After the existing maintenance or inspection program has been
revised as required by paragraphs (h) and (j) of this AD, no
alternative actions (e.g., inspections), intervals, or CDCCLs may be
used unless the actions, intervals, and CDCCLs are approved as an
alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (m)(1) of this AD.
(l) Credit for Previous Actions
(1) 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 MHI RJ
[[Page 3719]]
Service Bulletin 601R-28-068, dated December 3, 2020.
(2) This paragraph provides credit for actions required by
paragraph (i) of this AD, if those actions were performed before the
effective date of this AD using MHI RJ Service Bulletin 670BA-28-
041, dated December 3, 2020; or Revision A, dated December 21, 2020.
(m) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO 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, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; fax 516-794-5531. 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, New York ACO
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or MHI RJ
Aviation ULC's TCCA Design Approval Organization (DAO). If approved
by the DAO, the approval must include the DAO-authorized signature.
(n) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) TCCA AD CF-2021-16, dated April 26, 2021, for related
information. This MCAI may be found in the AD docket on the internet
at https://www.regulations.gov by searching for and locating Docket
No. FAA-2022-0011.
(2) For more information about this AD, contact Jiwan
Karunatilake, Aerospace Engineer, Airframe and Propulsion Section,
FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7300; fax 516-794-5531; email [email protected].
(3) For service information identified in this AD, contact MHI
RJ Aviation ULC, 12655 Henri-Fabre Blvd., Mirabel, Qu[eacute]bec J7N
1E1 Canada; Widebody Customer Response Center North America toll-
free telephone +1-844-272-2720 or direct-dial telephone +1-514-855-
8500; fax +1-514-855-8501; email [email protected]; internet https://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.
Issued on January 19, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-01352 Filed 1-24-22; 8:45 am]
BILLING CODE 4910-13-P