Airworthiness Directives; Bombardier, Inc., Airplanes, 53421-53424 [2022-18750]
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Federal Register / Vol. 87, No. 168 / Wednesday, August 31, 2022 / Proposed Rules
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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
lotter on DSK11XQN23PROD with PROPOSALS1
The Boeing Company: Docket No. FAA–
2022–0874; Project Identifier AD–2022–
00337–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by October 17,
2022.
(b) Affected ADs
This AD affects AD 2020–10–10,
Amendment 39–19913 (85 FR 31046, May 22,
2020) (AD 2020–10–10).
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16:49 Aug 30, 2022
Jkt 256001
(c) Applicability
This AD applies to The Boeing Company
Model DC–9–81 (MD–81), DC–9–82 (MD–82),
DC–9–83 (MD–83), and DC–9–87 (MD–87)
airplanes; and Model MD–88 airplanes,
certificated in any category, as identified in
Boeing Alert Requirements Bulletin MD80–
57A246 RB, dated December 17, 2021.
(d) Subject
Air Transport Association (ATA) of
America Code 57, Wings.
(e) Unsafe Condition
This AD was prompted by an evaluation by
the design approval holder (DAH) indicating
that the center wing lower stringers S–11
through S–22 are subject to widespread
fatigue damage (WFD). The FAA is issuing
this AD to address fatigue cracking of the
right and left side center wing lower stringers
S–11 through S–22 between wing stations
Xcw=13 and Xcw=15. If not addressed,
undetected fatigue cracks could grow to a
critical length after the structural
modification point (SMP) at 81,740 total
flight cycles. Any undetected cracks in three
or more adjacent stringers in the right or left
side center wing lower stringers S–11
through S–22 may result in a principal
structural element’s inability to sustain limit
load, which could adversely affect the
structural integrity of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Except as specified by paragraph (h) of this
AD: At the applicable times specified in the
‘‘Compliance’’ paragraph of Boeing Alert
Requirements Bulletin MD80–57A246 RB,
dated December 17, 2021, do all applicable
actions identified in, and in accordance with,
the Accomplishment Instructions of Boeing
Alert Requirements Bulletin MD80–57A246
RB, dated December 17, 2021.
Note 1 to paragraph (g): Guidance for
accomplishing the actions required by this
AD can be found in Boeing Alert Service
Bulletin MD80–57A246, dated December 17,
2021, which is referred to in Boeing Alert
Requirements Bulletin MD80–57A246 RB,
dated December 17, 2021.
53421
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Los Angeles 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 the attention of
the person identified in paragraph (k)(1) of
this AD. Information may be emailed to: 9ANM-LAACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by The Boeing Company
Organization Designation Authorization
(ODA) that has been authorized by the
Manager, Los Angeles ACO Branch, FAA, to
make those findings. To be approved, the
repair method, modification deviation, or
alteration deviation must meet the
certification basis of the airplane, and the
approval must specifically refer to this AD.
(k) Related Information
(1) For more information about this AD,
contact Sean Newell, Aerospace Engineer,
Airframe Section, FAA, Los Angeles ACO
Branch, 3960 Paramount Boulevard,
Lakewood, CA 90712–4137; phone: 562–627–
5266; email: sean.m.newell@faa.gov.
(2) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd.,
MC 110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet https://
www.myboeingfleet.com. You may view this
referenced 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 July 8, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–18759 Filed 8–30–22; 8:45 am]
BILLING CODE 4910–13–P
(h) Exceptions to Service Information
Specifications
Where Boeing Alert Requirements Bulletin
MD80–57A246 RB, dated December 17, 2021,
specifies contacting Boeing for replacement
instructions: This AD requires doing the
replacement using a method approved in
accordance with the procedures specified in
paragraph (i) of this AD.
(i) Terminating Action for AD 2020–10–10
Accomplishment of the replacement
specified in the Accomplishment
Instructions of Boeing Alert Requirements
Bulletin MD80–57A246 RB, dated December
17, 2021, terminates all of the requirements
of AD 2020–10–10.
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1065; Project
Identifier MCAI–2022–00280–T]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), DOT.
AGENCY:
E:\FR\FM\31AUP1.SGM
31AUP1
53422
Federal Register / Vol. 87, No. 168 / Wednesday, August 31, 2022 / Proposed Rules
Notice of proposed rulemaking
(NPRM).
ACTION:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD–
700–2A12 airplanes. This proposed AD
was prompted by a report that the
flightcrew and passenger oxygen
system’s refill and capillary lines may
have been contaminated by sealant and
cotton fibers. This proposed AD would
require an inspection to determine the
serial numbers of the oxygen cylinders
installed and replacement of each
affected oxygen cylinder and regulator
assembly (OCRA). 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 October 17,
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
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 Bombardier
Business Aircraft Customer Response
Center, 400 Coˆte-Vertu Road West,
Dorval, Que´bec H4S 1Y9, Canada;
telephone 514–855–2999; email ac.yul@
aero.bombardier.com; internet
bombardier.com. You may view this
service information at the FAA,
Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
lotter on DSK11XQN23PROD with PROPOSALS1
SUMMARY:
Examining the AD Docket
You may examine the AD docket at
regulations.gov by searching for and
locating Docket No. FAA–2022–1065; 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.
FOR FURTHER INFORMATION CONTACT:
Gabriel Kim, Aerospace Engineer,
VerDate Sep<11>2014
16:49 Aug 30, 2022
Jkt 256001
Mechanical Systems and Administrative
Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone
516–228–7300; email 9-avs-nyaco-cos@
faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2022–1065; Project Identifier
MCAI–2022–00280–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
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 Gabriel Kim,
Aerospace Engineer, Mechanical
Systems and Administrative Services
Section, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@
faa.gov. Any commentary that the FAA
receives which is not specifically
designated as CBI will be placed in the
public docket for this rulemaking.
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Background
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued TCCA AD CF–
2022–07, dated March 1, 2022 (TCCA
AD CF–2022–07) (also referred to after
this as the MCAI), to correct an unsafe
condition for certain Bombardier, Inc.,
Model BD–700–2A12 airplanes. You
may examine the MCAI in the AD
docket at regulations.gov by searching
for and locating Docket No. FAA–2022–
1065.
This proposed AD was prompted by
a report that the flightcrew and
passenger oxygen system’s refill and
capillary lines may have been
contaminated by sealant and cotton
fibers. Any contamination is expected to
collect in the OCRA filters. The FAA is
proposing this AD to address the
contamination, which may cause a
blockage of the oxygen system
components and result in a reduction of
oxygen flow, reduce the total amount of
available oxygen, or create a fire hazard.
See the MCAI for additional background
information.
Related Service Information Under 1
CFR Part 51
Bombardier has issued Service
Bulletin 700–35–7502, dated January 26,
2022. This service information describes
procedures for an inspection to
determine the serial numbers of the
oxygen cylinders installed and
replacement of each affected OCRA with
a new or reworked OCRA. 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
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, the FAA has been
notified of the unsafe condition
described in the MCAI and service
information referenced above. The FAA
is proposing this AD because the FAA
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
the service information already
described.
E:\FR\FM\31AUP1.SGM
31AUP1
Federal Register / Vol. 87, No. 168 / Wednesday, August 31, 2022 / Proposed Rules
Difference Between This NPRM and the
MCAI
this proposed AD would include such a
prohibition.
Although TCCA AD CF–2022–07 does
not specify prohibiting the installation
of any affected oxygen cylinder having
certain serial numbers on any airplane,
Costs of Compliance
53423
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
The FAA estimates that this AD, if
adopted as proposed, would affect 16
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
5 work-hours × $85 per hour = $425 ..........................................................................................
$3,069
$3,494
$55,904
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.
under the criteria of the Regulatory
Flexibility Act.
Authority for This Rulemaking
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
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.
lotter on DSK11XQN23PROD with PROPOSALS1
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
VerDate Sep<11>2014
16:49 Aug 30, 2022
Jkt 256001
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Bombardier, Inc.: Docket No. FAA–2022–
1065; Project Identifier MCAI–2022–
00280–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by October 17,
2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc.,
Model BD–700–2A12 airplanes, certificated
in any category, having serial numbers
70006, 70008, 70009 through 70016
inclusive, 70019, 70020, 70025, 70026,
70028, 70032 through 70035 inclusive, 70038
through 70043 inclusive, 70046, 70048,
70050, 70051, 70054, 70063, and 70073.
(d) Subject
Air Transport Association (ATA) of
America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report that the
flightcrew and passenger oxygen system’s
refill and capillary lines may have been
contaminated by sealant and cotton fibers.
The FAA is issuing this AD to address the
contamination, which may cause a blockage
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Fmt 4702
Sfmt 4702
of the oxygen system components and result
in a reduction of oxygen flow, reduce the
total amount of available oxygen, or create a
fire hazard.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Inspection and Replacement
Within 36 months after the effective date
of this AD: Do an inspection to determine the
serial numbers of the oxygen cylinders
installed in accordance with the
Accomplishment Instructions of Bombardier
Service Bulletin 700–35–7502, dated January
26, 2022. If any affected oxygen cylinder and
regulator assembly (OCRA) is installed,
before further flight replace the affected part
with a new or reworked OCRA, in
accordance with the Accomplishment
Instructions of Bombardier Service Bulletin
700–35–7502, dated January 26, 2022.
(h) Parts Installation Prohibition
As of the effective date of this AD, no
person may install any affected oxygen
cylinder having a serial number specified in
paragraph 1.A. of Bombardier Service
Bulletin 700–35–7502, dated January 26,
2022, on any airplane.
(i) No Reporting Requirement
Although Bombardier Service Bulletin
700–35–7502, dated January 26, 2022,
specifies to report certain information to the
manufacturer, this AD does not include that
requirement.
(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. Before using any approved
AMOC, notify your appropriate principal
inspector, or lacking a principal inspector,
E:\FR\FM\31AUP1.SGM
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53424
Federal Register / Vol. 87, No. 168 / Wednesday, August 31, 2022 / Proposed Rules
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 Bombardier Inc.’s TCCA Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(k) Additional Information
(1) Refer to TCCA AD CF–2022–07, dated
March 1, 2022, for related information. This
TCCA AD may be found in the AD docket on
the internet at regulations.gov by searching
for and locating Docket No. FAA–2022–1065.
(2) For more information about this AD,
contact Gabriel Kim, Aerospace Engineer,
Mechanical Systems and Administrative
Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–228–
7300; email 9-avs-nyaco-cos@faa.gov.
(3) For service information identified in
this AD, contact Bombardier Business
Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9,
Canada; telephone 514–855–2999; email
ac.yul@aero.bombardier.com; internet
bombardier.com. You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety Branch,
2200 South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
Issued on August 25, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–18750 Filed 8–30–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Examining the AD Docket
[Docket No. FAA–2022–0672; Project
Identifier MCAI–2020–01606–T]
RIN 2120–AA64
Airworthiness Directives; De Havilland
Aircraft of Canada Limited (Type
Certificate Previously Held by
Bombardier, Inc.) Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Supplemental notice of
proposed rulemaking (SNPRM).
lotter on DSK11XQN23PROD with PROPOSALS1
AGENCY:
The FAA is revising a notice
of proposed rulemaking (NPRM) to
supersede Airworthiness Directive (AD)
2020–04–20, which applies to certain
De Havilland Aircraft of Canada Limited
Model DHC–8–400 series airplanes.
This action revises the NPRM by
SUMMARY:
VerDate Sep<11>2014
16:49 Aug 30, 2022
Jkt 256001
including an additional retained
requirement and revising the
terminating action to apply to additional
airplanes. The FAA is proposing this
AD to address the unsafe condition on
these products. Since these actions
would impose an additional burden
over those in the NPRM, the FAA is
reopening the comment period to allow
the public the chance to comment on
these changes.
DATES: The FAA must receive comments
on this SNPRM by October 17, 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
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 SNPRM, contact De Havilland
Aircraft of Canada Limited, Dash 8
Series Customer Response Centre, 5800
Explorer Drive, Mississauga, Ontario,
L4W 5K9, Canada; telephone North
America (toll-free): 855–310–1013,
Direct: 647–277–582; email thd@
dehavilland.com; internet
dehavilland.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.
You may examine the AD docket at
regulations.gov under Docket No. FAA–
2022–0672; or in person at Docket
Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The AD docket contains, the
NPRM, this SNPRM, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT:
Joseph Catanzaro, Aerospace Engineer,
Airframe and Propulsion Section, FAA,
New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7366; email
9-avs-nyaco-cos@faa.gov.
SUPPLEMENTARY INFORMATION:
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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–2022–0672; Project Identifier
MCAI–2020–01606–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 SNPRM.
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 SNPRM
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 SNPRM, 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 SNPRM. Submissions containing
CBI should be sent to Joseph Catanzaro,
Aerospace Engineer, Airframe and
Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590;
telephone 516–228–7366; email 9-avsnyaco-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
The FAA issued AD 2020–04–20,
Amendment 39–19857 (85 FR 17473,
March 30, 2020) (AD 2020–04–20) for
certain De Havilland Aircraft of Canada
Limited Model DHC–8–400 series
airplanes. AD 2020–04–20 requires
E:\FR\FM\31AUP1.SGM
31AUP1
Agencies
[Federal Register Volume 87, Number 168 (Wednesday, August 31, 2022)]
[Proposed Rules]
[Pages 53421-53424]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-18750]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1065; Project Identifier MCAI-2022-00280-T]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
[[Page 53422]]
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier, Inc., Model BD-700-2A12 airplanes. This
proposed AD was prompted by a report that the flightcrew and passenger
oxygen system's refill and capillary lines may have been contaminated
by sealant and cotton fibers. This proposed AD would require an
inspection to determine the serial numbers of the oxygen cylinders
installed and replacement of each affected oxygen cylinder and
regulator assembly (OCRA). 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 October 17,
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 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 Bombardier
Business Aircraft Customer Response Center, 400 C[ocirc]te-Vertu Road
West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-2999;
email bombardier.com">[email protected]bombardier.com; internet bombardier.com. You may view
this service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call 206-
231-3195.
Examining the AD Docket
You may examine the AD docket at regulations.gov by searching for
and locating Docket No. FAA-2022-1065; 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.
FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2022-1065; Project Identifier
MCAI-2022-00280-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
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
Gabriel Kim, Aerospace Engineer, Mechanical Systems and Administrative
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516-228-7300; email [email protected]. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2022-07, dated March 1,
2022 (TCCA AD CF-2022-07) (also referred to after this as the MCAI), to
correct an unsafe condition for certain Bombardier, Inc., Model BD-700-
2A12 airplanes. You may examine the MCAI in the AD docket at
regulations.gov by searching for and locating Docket No. FAA-2022-1065.
This proposed AD was prompted by a report that the flightcrew and
passenger oxygen system's refill and capillary lines may have been
contaminated by sealant and cotton fibers. Any contamination is
expected to collect in the OCRA filters. The FAA is proposing this AD
to address the contamination, which may cause a blockage of the oxygen
system components and result in a reduction of oxygen flow, reduce the
total amount of available oxygen, or create a fire hazard. See the MCAI
for additional background information.
Related Service Information Under 1 CFR Part 51
Bombardier has issued Service Bulletin 700-35-7502, dated January
26, 2022. This service information describes procedures for an
inspection to determine the serial numbers of the oxygen cylinders
installed and replacement of each affected OCRA with a new or reworked
OCRA. 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
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,
the FAA has been notified of the unsafe condition described in the MCAI
and service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the service information already described.
[[Page 53423]]
Difference Between This NPRM and the MCAI
Although TCCA AD CF-2022-07 does not specify prohibiting the
installation of any affected oxygen cylinder having certain serial
numbers on any airplane, this proposed AD would include such a
prohibition.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 16 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
----------------------------------------------------------------------------------------------------------------
5 work-hours x $85 per hour = $425........................... $3,069 $3,494 $55,904
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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.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Bombardier, Inc.: Docket No. FAA-2022-1065; Project Identifier MCAI-
2022-00280-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by October 17, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-2A12
airplanes, certificated in any category, having serial numbers
70006, 70008, 70009 through 70016 inclusive, 70019, 70020, 70025,
70026, 70028, 70032 through 70035 inclusive, 70038 through 70043
inclusive, 70046, 70048, 70050, 70051, 70054, 70063, and 70073.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report that the flightcrew and
passenger oxygen system's refill and capillary lines may have been
contaminated by sealant and cotton fibers. The FAA is issuing this
AD to address the contamination, which may cause a blockage of the
oxygen system components and result in a reduction of oxygen flow,
reduce the total amount of available oxygen, or create a fire
hazard.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Replacement
Within 36 months after the effective date of this AD: Do an
inspection to determine the serial numbers of the oxygen cylinders
installed in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 700-35-7502, dated January 26, 2022. If
any affected oxygen cylinder and regulator assembly (OCRA) is
installed, before further flight replace the affected part with a
new or reworked OCRA, in accordance with the Accomplishment
Instructions of Bombardier Service Bulletin 700-35-7502, dated
January 26, 2022.
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install any
affected oxygen cylinder having a serial number specified in
paragraph 1.A. of Bombardier Service Bulletin 700-35-7502, dated
January 26, 2022, on any airplane.
(i) No Reporting Requirement
Although Bombardier Service Bulletin 700-35-7502, dated January
26, 2022, specifies to report certain information to the
manufacturer, this AD does not include that requirement.
(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. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector,
[[Page 53424]]
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
Bombardier Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(k) Additional Information
(1) Refer to TCCA AD CF-2022-07, dated March 1, 2022, for
related information. This TCCA AD may be found in the AD docket on
the internet at regulations.gov by searching for and locating Docket
No. FAA-2022-1065.
(2) For more information about this AD, contact Gabriel Kim,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">[email protected]bombardier.com; internet
bombardier.com. You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
Issued on August 25, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-18750 Filed 8-30-22; 8:45 am]
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