Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes, 77763-77765 [2022-27565]
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Federal Register / Vol. 87, No. 243 / Tuesday, December 20, 2022 / Proposed Rules
A35.4 Airworthiness Limitations Section
[Applicable to Model M001]
Issued in Washington, DC, on December
12, 2022.
Victor W. Wicklund,
Acting Director, Policy and Innovation
Division, Aircraft Certification Service.
[FR Doc. 2022–27445 Filed 12–19–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1650; Project
Identifier MCAI–2022–00210–T]
RIN 2120–AA64
Airworthiness Directives; Airbus
Canada Limited Partnership (Type
Certificate Previously Held by C Series
Aircraft Limited Partnership (CSALP);
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 Airbus Canada Limited
Partnership Model BD–500–1A11
airplanes. This proposed AD was
prompted by a report that the nose
radome lightning diverter strips on
certain aircraft were painted in
production; paint on the diverter strips
can compromise the nose radome
lightning protection. This proposed AD
would require inspecting for paint on
the diverter strips on the nose radome,
and replacing the nose radome if
necessary, 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 3,
2023.
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
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SUMMARY:
VerDate Sep<11>2014
17:32 Dec 19, 2022
Jkt 259001
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1650; 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 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
AD-CN@tc.gc.ca; website tc.canada.ca/
en/aviation. It is also available at
regulations.gov under Docket No. FAA–
2022–1650.
• For service information identified
in this NPRM, contact Airbus Canada
Limited Partnership, 13100 Henri-Fabre
Boulevard, Mirabel, Que´bec, J7N 3C6,
Canada; telephone 450–476–7676; email
a220lcrc@abc.airbus; website
a220world.airbus.com.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical
Systems Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone
516–228–7367; 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
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2022–1650; Project Identifier
MCAI–2022–00210–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
PO 00000
Frm 00015
Fmt 4702
Sfmt 4702
77763
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 Steven Dzierzynski,
Aerospace Engineer, Avionics and
Electrical Systems Section, FAA, New
York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7367; 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 Transport Canada AD CF–2022–
04, dated February 14, 2022 (Transport
Canada AD CF–2022–04) (also referred
to as the MCAI), to correct an unsafe
condition for certain Airbus Canada
Limited Partnership Model BD–500–
1A11 airplanes. The MCAI states that
the radome lightning diverter strips on
certain aircraft were painted in
production; paint on the diverter strips
can compromise the radome lightning
protection. Reduced effectiveness of the
diverter strips can lead to the puncture
of the nose radome by lightning and
potential arc attachment to antennas,
structures, and other equipment in the
area of the radome. The unsafe
condition, if not addressed, could result
in damage to the localizer or glideslope
antennas, and consequent loss of
instrument landing system localizer
inputs or deviation information.
The FAA is proposing this AD to
address the unsafe condition on these
products. You may examine the MCAI
E:\FR\FM\20DEP1.SGM
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77764
Federal Register / Vol. 87, No. 243 / Tuesday, December 20, 2022 / Proposed Rules
in the AD docket at regulations.gov
under Docket No. FAA–2022–1650.
in the MCAI described 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.
Related Service Information Under 1
CFR Part 51
Transport Canada AD CF–2022–04
specifies procedures for inspecting for
paint on the lightning diverter strips on
the nose radome, and replacing the nose
radome if the lightning diverter strips
are painted.
The FAA also reviewed Airbus
Canada Limited Partnership A220
Service Bulletin BD500–538009, Issue
002, dated June 2, 2022. This service
information specifies procedures for
inspecting for paint on the lightning
diverter strips on the nose radome, and
replacing and painting the nose radome
if the lightning diverter strips are
painted.
This material is reasonably available
because the interested parties have
access to it through their normal course
of business or by the means identified
in ADDRESSES.
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
Transport Canada AD CF–2022–04
described previously, except for any
differences identified as exceptions in
the regulatory text of this proposed AD.
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 the State of
Design Authority, it has notified the
FAA of the unsafe condition described
Additional Method of Compliance
Transport Canada AD CF–2022–04
requires removing and replacing the
radome in accordance with certain
aircraft maintenance publication (AMP)
data modules (DM). After Transport
Canada issued AD CF–2022–04, Airbus
Canada issued Airbus Canada Limited
Partnership A220 Service Bulletin
BD500–538009, Issue 001, dated April
8, 2022; and Issue 002, dated June 2,
2022, which also describes procedures
for removing and replacing the radome.
This proposed AD would therefore also
allow accomplishing those actions in
accordance with Airbus Canada Limited
Partnership A220 Service Bulletin
BD500–538009, Issue 002, dated June 2,
2022.
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–
2022–04 by reference in the FAA final
rule. This proposed AD would,
therefore, require compliance with
Transport Canada AD CF–2022–04 in its
entirety 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–
2022–04 for compliance will be
available at regulations.gov under
Docket No. FAA–2022–1650 after the
FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 7
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
6 work-hours × $85 per hour = $510 ..........................................................................................
* $0
$510
$3,570
* The FAA has received no definitive data on which to base the parts cost estimate for the radome replacement.
The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some or all
of the costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
operators.
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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
VerDate Sep<11>2014
17:32 Dec 19, 2022
Jkt 259001
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,
PO 00000
Frm 00016
Fmt 4702
Sfmt 4702
(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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
E:\FR\FM\20DEP1.SGM
20DEP1
Federal Register / Vol. 87, No. 243 / Tuesday, December 20, 2022 / Proposed Rules
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Airbus Canada Limited Partnership (Type
Certificate Previously Held by C Series
Aircraft Limited Partnership (CSALP);
Bombardier, Inc.): Docket No. FAA–
2022–1650; Project Identifier MCAI–
2022–00210–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by February 3,
2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Canada Limited
Partnership Model BD–500–1A11 airplanes,
certificated in any category, as identified in
Transport Canada AD CF–2022–04, dated
February 14, 2022 (Transport Canada AD CF–
2022–04).
(d) Subject
Air Transport Association (ATA) of
America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by a report that the
radome lightning diverter strips on certain
aircraft were painted in production; paint on
the diverter strips can compromise the
radome lightning protection. The FAA is
issuing this AD to address reduced
effectiveness of the diverter strips, which can
lead to the puncture of the nose radome by
lightning and potential arc attachment to
antennas, structures, and other equipment in
the area of the radome. The unsafe condition,
if not addressed, could result in damage to
the localizer or glideslope antennas, and
consequent loss of instrument landing system
localizer inputs or deviation information.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
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(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–
2022–04.
(h) Exceptions To Transport Canada AD CF–
2022–04
(1) Where Transport Canada AD CF–2022–
04 refers to its effective date, this AD requires
using the effective date of this AD.
(2) Where Transport Canada AD CF–2022–
04 specifies removing and installing a
radome using certain aircraft maintenance
publication data modules, this AD also
allows accomplishing those actions in
accordance with Airbus Canada Limited
Partnership A220 Service Bulletin BD500–
538009, Issue 002, dated June 2, 2022.
(i) Credit for Previous Actions
This paragraph provides credit for actions
required by paragraph (g) of this AD, if those
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17:32 Dec 19, 2022
Jkt 259001
actions were performed before the effective
date of this AD using Airbus Canada Limited
Partnership A220 Service Bulletin BD500–
538009, Issue 001, dated May 9, 2022.
(j) Additional 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 or email 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, New York ACO Branch,
FAA; or Transport Canada; or Airbus Canada
Limited Partnership’s Transport Canada
Design Approval Organization (DAO). If
approved by the DAO, the approval must
include the DAO-authorized signature.
(3) Required for Compliance (RC): Except
as required by paragraph (j)(2) of this AD, if
any service information contains procedures
or tests that are identified as RC, those
procedures and tests must be done to comply
with this AD; any procedures or tests that are
not identified as RC are recommended. Those
procedures and tests that are not identified
as RC may be deviated from using accepted
methods in accordance with the operator’s
maintenance or inspection program without
obtaining approval of an AMOC, provided
the procedures and tests identified as RC can
be done and the airplane can be put back in
an airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(k) Additional Information
For more information about this AD,
contact Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical Systems
Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7367; email 9-avsnyaco-cos@faa.gov.
(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) Airbus Canada Limited Partnership
A220 Service Bulletin BD500–538009, Issue
002, dated June 2, 2022.
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Frm 00017
Fmt 4702
Sfmt 4702
77765
(ii) Transport Canada AD CF–2022–04,
dated February 14, 2022.
(3) For Transport Canada AD CF–2022–04,
contact Transport Canada, Transport Canada
National Aircraft Certification, 159 Cleopatra
Drive, Nepean, Ontario K1A 0N5, Canada;
telephone 888–663–3639; email AD-CN@
tc.gc.ca; website tc.canada.ca/en/aviation.
(4) For service information identified in
this AD, contact Airbus Canada Limited
Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Que´bec, J7N 3C6, Canada; telephone
450–476–7676; email a220_
website a220world.airbus.com.
(5) 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.
(6) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on December 15, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–27565 Filed 12–19–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Office of the Secretary
14 CFR Part 399
[Docket No. DOT–OST–2022–0109]
RIN 2105–AF10
Enhancing Transparency of Airline
Ancillary Service Fees
Office of the Secretary (OST),
Department of Transportation (DOT or
the Department).
ACTION: Extension of comment period.
AGENCY:
The U.S. Department of
Transportation (Department or DOT) is
extending through January 23, 2023, the
period for interested persons to submit
comments to its proposed rule on
Enhancing Transparency of Airline
Ancillary Service Fees.
DATES: Comments should be filed by
January 23, 2023. Late-filed comments
will be considered to the extent
practicable. Petitions for a hearing
pursuant to 14 CFR 399.75(b)(1) must
also be filed by January 23, 2023.
ADDRESSES: You may file comments
identified by the docket number DOT–
OST–2022–0109 by any of the following
methods:
• Federal eRulemaking Portal: go to
https://www.regulations.gov and follow
SUMMARY:
E:\FR\FM\20DEP1.SGM
20DEP1
Agencies
[Federal Register Volume 87, Number 243 (Tuesday, December 20, 2022)]
[Proposed Rules]
[Pages 77763-77765]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-27565]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1650; Project Identifier MCAI-2022-00210-T]
RIN 2120-AA64
Airworthiness Directives; Airbus Canada Limited Partnership (Type
Certificate Previously Held by C Series Aircraft Limited Partnership
(CSALP); 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 Airbus Canada Limited Partnership Model BD-500-1A11
airplanes. This proposed AD was prompted by a report that the nose
radome lightning diverter strips on certain aircraft were painted in
production; paint on the diverter strips can compromise the nose radome
lightning protection. This proposed AD would require inspecting for
paint on the diverter strips on the nose radome, and replacing the nose
radome if necessary, 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 3,
2023.
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-2022-1650; 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 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-
2022-1650.
For service information identified in this NPRM, contact
Airbus Canada Limited Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Qu[eacute]bec, J7N 3C6, Canada; telephone 450-476-7676; email
[email protected]; website a220world.airbus.com.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195.
FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical Systems Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7367; 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-2022-1650; Project Identifier
MCAI-2022-00210-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
Steven Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7367; 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 Transport Canada AD CF-2022-04, dated February 14, 2022
(Transport Canada AD CF-2022-04) (also referred to as the MCAI), to
correct an unsafe condition for certain Airbus Canada Limited
Partnership Model BD-500-1A11 airplanes. The MCAI states that the
radome lightning diverter strips on certain aircraft were painted in
production; paint on the diverter strips can compromise the radome
lightning protection. Reduced effectiveness of the diverter strips can
lead to the puncture of the nose radome by lightning and potential arc
attachment to antennas, structures, and other equipment in the area of
the radome. The unsafe condition, if not addressed, could result in
damage to the localizer or glideslope antennas, and consequent loss of
instrument landing system localizer inputs or deviation information.
The FAA is proposing this AD to address the unsafe condition on
these products. You may examine the MCAI
[[Page 77764]]
in the AD docket at regulations.gov under Docket No. FAA-2022-1650.
Related Service Information Under 1 CFR Part 51
Transport Canada AD CF-2022-04 specifies procedures for inspecting
for paint on the lightning diverter strips on the nose radome, and
replacing the nose radome if the lightning diverter strips are painted.
The FAA also reviewed Airbus Canada Limited Partnership A220
Service Bulletin BD500-538009, Issue 002, dated June 2, 2022. This
service information specifies procedures for inspecting for paint on
the lightning diverter strips on the nose radome, and replacing and
painting the nose radome if the lightning diverter strips are painted.
This material is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in 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 the State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
described 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 accomplishing the actions specified
in Transport Canada AD CF-2022-04 described previously, except for any
differences identified as exceptions in the regulatory text of this
proposed AD.
Additional Method of Compliance
Transport Canada AD CF-2022-04 requires removing and replacing the
radome in accordance with certain aircraft maintenance publication
(AMP) data modules (DM). After Transport Canada issued AD CF-2022-04,
Airbus Canada issued Airbus Canada Limited Partnership A220 Service
Bulletin BD500-538009, Issue 001, dated April 8, 2022; and Issue 002,
dated June 2, 2022, which also describes procedures for removing and
replacing the radome. This proposed AD would therefore also allow
accomplishing those actions in accordance with Airbus Canada Limited
Partnership A220 Service Bulletin BD500-538009, Issue 002, dated June
2, 2022.
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-2022-04 by reference
in the FAA final rule. This proposed AD would, therefore, require
compliance with Transport Canada AD CF-2022-04 in its entirety 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-2022-04 for compliance will be
available at regulations.gov under Docket No. FAA-2022-1650 after the
FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 7 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
6 work-hours x $85 per hour = $510........................... * $0 $510 $3,570
----------------------------------------------------------------------------------------------------------------
* The FAA has received no definitive data on which to base the parts cost estimate for the radome replacement.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed AD may be covered under warranty, thereby reducing the
cost impact on affected operators.
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.
[[Page 77765]]
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Airbus Canada Limited Partnership (Type Certificate Previously Held
by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.):
Docket No. FAA-2022-1650; Project Identifier MCAI-2022-00210-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 3, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Canada Limited Partnership Model BD-
500-1A11 airplanes, certificated in any category, as identified in
Transport Canada AD CF-2022-04, dated February 14, 2022 (Transport
Canada AD CF-2022-04).
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by a report that the radome lightning
diverter strips on certain aircraft were painted in production;
paint on the diverter strips can compromise the radome lightning
protection. The FAA is issuing this AD to address reduced
effectiveness of the diverter strips, which can lead to the puncture
of the nose radome by lightning and potential arc attachment to
antennas, structures, and other equipment in the area of the radome.
The unsafe condition, if not addressed, could result in damage to
the localizer or glideslope antennas, and consequent loss of
instrument landing system localizer inputs or deviation information.
(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-2022-04.
(h) Exceptions To Transport Canada AD CF-2022-04
(1) Where Transport Canada AD CF-2022-04 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where Transport Canada AD CF-2022-04 specifies removing and
installing a radome using certain aircraft maintenance publication
data modules, this AD also allows accomplishing those actions in
accordance with Airbus Canada Limited Partnership A220 Service
Bulletin BD500-538009, Issue 002, dated June 2, 2022.
(i) 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 Airbus Canada Limited Partnership A220 Service
Bulletin BD500-538009, Issue 001, dated May 9, 2022.
(j) Additional 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 or email 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, New York ACO
Branch, FAA; or Transport Canada; or Airbus Canada Limited
Partnership's Transport Canada Design Approval Organization (DAO).
If approved by the DAO, the approval must include the DAO-authorized
signature.
(3) Required for Compliance (RC): Except as required by
paragraph (j)(2) of this AD, if any service information contains
procedures or tests that are identified as RC, those procedures and
tests must be done to comply with this AD; any procedures or tests
that are not identified as RC are recommended. Those procedures and
tests that are not identified as RC may be deviated from using
accepted methods in accordance with the operator's maintenance or
inspection program without obtaining approval of an AMOC, provided
the procedures and tests identified as RC can be done and the
airplane can be put back in an airworthy condition. Any
substitutions or changes to procedures or tests identified as RC
require approval of an AMOC.
(k) Additional Information
For more information about this AD, contact Steven Dzierzynski,
Aerospace Engineer, Avionics and Electrical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7367; 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) Airbus Canada Limited Partnership A220 Service Bulletin
BD500-538009, Issue 002, dated June 2, 2022.
(ii) Transport Canada AD CF-2022-04, dated February 14, 2022.
(3) For Transport Canada AD CF-2022-04, 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) For service information identified in this AD, contact
Airbus Canada Limited Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Qu[eacute]bec, J7N 3C6, Canada; telephone 450-476-7676;
email [email protected]; website a220world.airbus.com.
(5) 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.
(6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on December 15, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-27565 Filed 12-19-22; 8:45 am]
BILLING CODE 4910-13-P