Airworthiness Directives; Bombardier, Inc., Airplanes, 22362-22364 [2023-07741]
Download as PDF
22362
Federal Register / Vol. 88, No. 71 / Thursday, April 13, 2023 / Rules and Regulations
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Validation Branch, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
In accordance with 14 CFR 39.19, send your
request to your principal inspector or
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
it to the attention of the person identified in
paragraph (k) of this AD. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or CAAI; or CAAI’s authorized
Designee. If approved by the CAAI Designee,
the approval must include the Designee’s
authorized signature.
(k) Additional Information
For more information about this AD,
contact Dan Rodina, Aerospace Engineer,
Large Aircraft Section, FAA, International
Validation Branch, FAA, 2200 South 216th
Street, Des Moines, WA 98198; telephone
206–231–3225; email dan.rodina@faa.gov.
lotter on DSK11XQN23PROD with RULES1
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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) Civil Aviation Authority of Israel (CAAI)
AD ISR I–57–2021–12–4, dated January 1,
2022.
(ii) [Reserved]
(3) For CAAI AD ISR I–57–2021–12–4,
contact Civil Aviation Authority of Israel
(CAAI), P.O. Box 1101, Golan Street, Airport
City, 70100, Israel; telephone 972–3–
9774665; fax 972–3–9774592; email aip@
mot.gov.il. You may find this CAAI AD on
the CAAI website at caa.gov.il.
(4) You may view this material at the FAA,
Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(5) You may view this material 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 March 17, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–07739 Filed 4–12–23; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
15:58 Apr 12, 2023
Jkt 259001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1654; Project
Identifier MCAI–2022–01165–T; Amendment
39–22390; AD 2023–06–04]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
Background
The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc., Model CL–600–1A11
(600), CL–600–2A12 (601), and CL–600–
2B16 (601–3A, 601–3R, and 604
Variants) airplanes. This AD was
prompted by reports of some passenger
oxygen mask dispensing units (MDUs)
with lanyards that are too long to meet
the proper length specifications of the
airplane. This AD requires replacing the
affected MDUs with units that meet the
proper length specifications, replacing
the placards, and re-identifying the
assemblies. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective May 18,
2023.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of May 18, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1654; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
Material Incorporated by Reference:
• For service information identified
in this final rule, 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; website
bombardier.com.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
SUMMARY:
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195. It is also available at
regulations.gov under Docket No. FAA–
2022–1654.
FOR FURTHER INFORMATION CONTACT:
Elizabeth M. Dowling, 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.
SUPPLEMENTARY INFORMATION:
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Bombardier, Inc., Model
CL–600–1A11 (600), CL–600–2A12
(601), and CL–600–2B16 (601–3A, 601–
3R, and 604 Variants) airplanes. The
NPRM published in the Federal
Register on December 27, 2022 (87 FR
79259). The NPRM was prompted by
AD CF–2022–50, dated August 25, 2022,
issued by Transport Canada, which is
the aviation authority for Canada
(referred to after this as the MCAI). The
MCAI states that lanyards of passenger
mask dispensing units installed in the
affected airplanes are too long to meet
the proper length specifications of the
aircraft. This condition, if not corrected,
could result in the inability to initiate
the flow of oxygen to the mask when
required in an emergency situation,
with no indication to the passenger that
they are not receiving oxygen.
In the NPRM, the FAA proposed to
require replacing the affected MDUs
with units that meet the proper length
specifications, replacing the placards,
and re-identifying the assemblies. The
FAA is issuing this AD to address the
unsafe condition on these products.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2022–1654.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
Conclusion
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI referenced above. The FAA
E:\FR\FM\13APR1.SGM
13APR1
Federal Register / Vol. 88, No. 71 / Thursday, April 13, 2023 / Rules and Regulations
reviewed the relevant data and
determined that air safety requires
adopting this AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on this
product. Except for minor editorial
changes, this AD is adopted as proposed
in the NPRM. None of the changes will
increase the economic burden on any
operator.
Related Service Information Under 1
CFR Part 51
The FAA reviewed following
Bombardier service information, which
specifies procedures for identifying part
numbers of the drop-down oxygen
boxes, performing drop-down oxygen
mask reach testing, marking failed seats
as inoperative with placards, and
replacing affected oxygen masks:
• Service Bulletin 600–0777, dated
December 13, 2021.
• Service Bulletin 601–1109, Revision
01, dated May 6, 2022.
• Service Bulletin 604–35–007,
Revision 01, dated May 6, 2022.
These documents are distinct since
they apply to different airplane models.
This service information is reasonably
22363
available because the interested parties
have access to it through their normal
course of business or by the means
identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD
affects 301 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
1 work-hour × $85 per hour = $85 ..............................................................................................
$0
$85
$25,585
The FAA estimates the following
costs to do any necessary on-condition
actions that would be required based on
the results of any required actions. The
FAA has no way of determining the
number of aircraft that might need these
on-condition actions:
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
Parts cost
Cost per
product
2 work-hours × $85 per hour = $170 ......................................................................................................................
$100
$270
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.
lotter on DSK11XQN23PROD with RULES1
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
VerDate Sep<11>2014
15:58 Apr 12, 2023
Jkt 259001
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2023–06–04 Bombardier, Inc.: Amendment
39–22390; Docket No. FAA–2022–1654;
Project Identifier MCAI–2022–01165–T.
(a) Effective Date
This airworthiness directive (AD) is
effective May 18, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc.,
airplanes, certificated in any category, with
serial numbers as identified in the service
information specified in paragraphs (c)(1)
through (4) of this AD.
(1) Model CL–600–1A11 (600) airplanes:
Bombardier Service Bulletin 600–0777, dated
December 13, 2021.
(2) Model CL–600–2A12 (601) airplanes:
Bombardier Service Bulletin 601–1109,
Revision 01, dated May 6, 2022.
(3) Model CL–600–2B16 (601–3A, 601–3R)
airplanes: Bombardier Service Bulletin 601–
1109, Revision 01, dated May 6, 2022.
(4) Model CL–600–2B16 (604) airplanes:
Bombardier Service Bulletin 604–35–007,
Revision 01, dated May 6, 2022.
(d) Subject
Air Transport Association (ATA) of
America Code 35, Oxygen System.
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13APR1
22364
Federal Register / Vol. 88, No. 71 / Thursday, April 13, 2023 / Rules and Regulations
(e) Unsafe Condition
This AD was prompted by reports of
passenger oxygen mask dispensing units
installed in the affected airplanes with
lanyards that are too long to meet the proper
length specifications of the airplane. The
FAA is issuing this AD to address the
inability to initiate flow of oxygen to the
mask. The unsafe condition, if not addressed,
could result in no indication to the passenger
that they are not receiving oxygen in an
emergency situation.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Inspection and Replacement
Within 5 years after the effective date of
this AD, determine the part number of the
drop-down oxygen box, in accordance with
Section 2.B. of the Accomplishment
Instructions of the applicable service
information identified in paragraphs (c)(1)
through (4) of this AD.
(1) If any drop-down oxygen box part
number (P/N) installed on the airplane
matches any P/N listed in Table 1 of Section
2.B. of the applicable service information:
Before further flight, perform drop-down
oxygen mask reach testing in accordance
with Section 2.B.(2) of the Accomplishment
Instructions of the applicable service
information identified in paragraphs (c)(1)
through (4) of this AD.
(i) If the test result is PASS: Before further
flight, replace the drop-down oxygen box
assembly in accordance with Section 2.C.,
and test the passenger oxygen supply system
in accordance with Section 2.D.(2), of the
applicable service information identified in
paragraphs (c)(1) through (4) of this AD.
(ii) If the test result is FAIL for any
individual seat: Before further flight, mark
the failed seat as inoperative in accordance
with Section 2.B.(3) of the applicable service
information specified in paragraphs (c)(1)
through (4) of this AD.
(2) If the part number of any drop-down
oxygen box assembly installed on the
airplane is not found in Table 1 of Section
2.B. of the applicable service information
identified in paragraphs (c)(1) through (4) of
this AD: Before further flight, do actions to
correct the unsafe condition using a method
approved in accordance with the procedures
specified in paragraph (i)(1) of this AD.
lotter on DSK11XQN23PROD with RULES1
(h) 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 Bombardier Service
Bulletin 601–1109, dated December 13, 2021;
or Bombardier Service Bulletin 604–35–007,
dated December 13, 2021; as applicable.
(i) 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
VerDate Sep<11>2014
15:58 Apr 12, 2023
Jkt 259001
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 New York ACO Branch,
mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address
identified in paragraph (j)(2) of this AD or
email to: 9-avs-nyaco-cos@faa.gov. If mailing
information, also submit information by
email. 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 Bombardier,
Inc.’s Transport Canada Design Approval
Organization (DAO). If approved by the DAO,
the approval must include the DAOauthorized signature.
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
(j) Additional Information
(1) Refer to Transport Canada AD CF–
2022–50, dated August 25, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2022–1654.
(2) For more information about this AD,
contact Elizabeth M. Dowling, 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) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
Airworthiness Directives; De Havilland
Aircraft of Canada Limited (Type
Certificate Previously Held by
Bombardier, Inc.) Airplanes
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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) Bombardier Service Bulletin 600–0777,
dated December 13, 2021.
(ii) Bombardier Service Bulletin 601–1109,
Revision 01, dated May 6, 2022.
(iii) Bombardier Service Bulletin 604–35–
007, Revision 01, dated May 6, 2022.
(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; website
bombardier.com.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
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Fmt 4700
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Issued on March 14, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–07741 Filed 4–12–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1482; Project
Identifier MCAI–2022–00697–T; Amendment
39–22389; AD 2023–06–03]
RIN 2120–AA64
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
De Havilland Aircraft of Canada Limited
Model DHC–8–401 and –402 airplanes.
This AD was prompted by an
investigation of incorrectly
manufactured sleeves that were
potentially installed in the main landing
gear (MLG) forward door linkage
assembly. This AD requires review of
technical records and inspections to
determine if a discrepant sleeve is
installed, replacement of any discrepant
sleeve and re-identification of the MLG
forward door linkage assembly. This AD
also prohibits the installation of affected
parts. The FAA is issuing this AD to
address the unsafe condition on these
products.
SUMMARY:
This AD is effective May 18,
2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of May 18, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at under Docket No. FAA–2022–
1482; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the mandatory continuing airworthiness
information (MCAI), any comments
received, and other information. The
address for Docket Operations is U.S.
Department of Transportation, Docket
DATES:
E:\FR\FM\13APR1.SGM
13APR1
Agencies
[Federal Register Volume 88, Number 71 (Thursday, April 13, 2023)]
[Rules and Regulations]
[Pages 22362-22364]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-07741]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1654; Project Identifier MCAI-2022-01165-T;
Amendment 39-22390; AD 2023-06-04]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model CL-600-1A11 (600), CL-600-2A12 (601),
and CL-600-2B16 (601-3A, 601-3R, and 604 Variants) airplanes. This AD
was prompted by reports of some passenger oxygen mask dispensing units
(MDUs) with lanyards that are too long to meet the proper length
specifications of the airplane. This AD requires replacing the affected
MDUs with units that meet the proper length specifications, replacing
the placards, and re-identifying the assemblies. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective May 18, 2023.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 18, 2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1654; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For service information identified in this final rule,
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; website
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. It is also available at
regulations.gov under Docket No. FAA-2022-1654.
FOR FURTHER INFORMATION CONTACT: Elizabeth M. Dowling, 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:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Bombardier,
Inc., Model CL-600-1A11 (600), CL-600-2A12 (601), and CL-600-2B16 (601-
3A, 601-3R, and 604 Variants) airplanes. The NPRM published in the
Federal Register on December 27, 2022 (87 FR 79259). The NPRM was
prompted by AD CF-2022-50, dated August 25, 2022, issued by Transport
Canada, which is the aviation authority for Canada (referred to after
this as the MCAI). The MCAI states that lanyards of passenger mask
dispensing units installed in the affected airplanes are too long to
meet the proper length specifications of the aircraft. This condition,
if not corrected, could result in the inability to initiate the flow of
oxygen to the mask when required in an emergency situation, with no
indication to the passenger that they are not receiving oxygen.
In the NPRM, the FAA proposed to require replacing the affected
MDUs with units that meet the proper length specifications, replacing
the placards, and re-identifying the assemblies. The FAA is issuing
this AD to address the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1654.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA
[[Page 22363]]
reviewed the relevant data and determined that air safety requires
adopting this AD as proposed. Accordingly, the FAA is issuing this AD
to address the unsafe condition on this product. Except for minor
editorial changes, this AD is adopted as proposed in the NPRM. None of
the changes will increase the economic burden on any operator.
Related Service Information Under 1 CFR Part 51
The FAA reviewed following Bombardier service information, which
specifies procedures for identifying part numbers of the drop-down
oxygen boxes, performing drop-down oxygen mask reach testing, marking
failed seats as inoperative with placards, and replacing affected
oxygen masks:
Service Bulletin 600-0777, dated December 13, 2021.
Service Bulletin 601-1109, Revision 01, dated May 6, 2022.
Service Bulletin 604-35-007, Revision 01, dated May 6,
2022.
These documents are distinct since they apply to different airplane
models. This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 301 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. $0 $85 $25,585
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need these on-condition actions:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Cost per
Labor cost Parts cost product
------------------------------------------------------------------------
2 work-hours x $85 per hour = $170.... $100 $270
------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2023-06-04 Bombardier, Inc.: Amendment 39-22390; Docket No. FAA-
2022-1654; Project Identifier MCAI-2022-01165-T.
(a) Effective Date
This airworthiness directive (AD) is effective May 18, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., airplanes, certificated in
any category, with serial numbers as identified in the service
information specified in paragraphs (c)(1) through (4) of this AD.
(1) Model CL-600-1A11 (600) airplanes: Bombardier Service
Bulletin 600-0777, dated December 13, 2021.
(2) Model CL-600-2A12 (601) airplanes: Bombardier Service
Bulletin 601-1109, Revision 01, dated May 6, 2022.
(3) Model CL-600-2B16 (601-3A, 601-3R) airplanes: Bombardier
Service Bulletin 601-1109, Revision 01, dated May 6, 2022.
(4) Model CL-600-2B16 (604) airplanes: Bombardier Service
Bulletin 604-35-007, Revision 01, dated May 6, 2022.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen
System.
[[Page 22364]]
(e) Unsafe Condition
This AD was prompted by reports of passenger oxygen mask
dispensing units installed in the affected airplanes with lanyards
that are too long to meet the proper length specifications of the
airplane. The FAA is issuing this AD to address the inability to
initiate flow of oxygen to the mask. The unsafe condition, if not
addressed, could result in no indication to the passenger that they
are not receiving oxygen in an emergency situation.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Replacement
Within 5 years after the effective date of this AD, determine
the part number of the drop-down oxygen box, in accordance with
Section 2.B. of the Accomplishment Instructions of the applicable
service information identified in paragraphs (c)(1) through (4) of
this AD.
(1) If any drop-down oxygen box part number (P/N) installed on
the airplane matches any P/N listed in Table 1 of Section 2.B. of
the applicable service information: Before further flight, perform
drop-down oxygen mask reach testing in accordance with Section
2.B.(2) of the Accomplishment Instructions of the applicable service
information identified in paragraphs (c)(1) through (4) of this AD.
(i) If the test result is PASS: Before further flight, replace
the drop-down oxygen box assembly in accordance with Section 2.C.,
and test the passenger oxygen supply system in accordance with
Section 2.D.(2), of the applicable service information identified in
paragraphs (c)(1) through (4) of this AD.
(ii) If the test result is FAIL for any individual seat: Before
further flight, mark the failed seat as inoperative in accordance
with Section 2.B.(3) of the applicable service information specified
in paragraphs (c)(1) through (4) of this AD.
(2) If the part number of any drop-down oxygen box assembly
installed on the airplane is not found in Table 1 of Section 2.B. of
the applicable service information identified in paragraphs (c)(1)
through (4) of this AD: Before further flight, do actions to correct
the unsafe condition using a method approved in accordance with the
procedures specified in paragraph (i)(1) of this AD.
(h) 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 Bombardier Service Bulletin 601-1109, dated
December 13, 2021; or Bombardier Service Bulletin 604-35-007, dated
December 13, 2021; as applicable.
(i) 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 New York ACO
Branch, mail it to ATTN: Program Manager, Continuing Operational
Safety, at the address identified in paragraph (j)(2) of this AD or
email to: [email protected]. If mailing information, also
submit information by email. 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 Bombardier, Inc.'s Transport
Canada Design Approval Organization (DAO). If approved by the DAO,
the approval must include the DAO-authorized signature.
(j) Additional Information
(1) Refer to Transport Canada AD CF-2022-50, dated August 25,
2022, for related information. This Transport Canada AD may be found
in the AD docket at regulations.gov under Docket No. FAA-2022-1654.
(2) For more information about this AD, contact Elizabeth M.
Dowling, 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) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) Bombardier Service Bulletin 600-0777, dated December 13,
2021.
(ii) Bombardier Service Bulletin 601-1109, Revision 01, dated
May 6, 2022.
(iii) Bombardier Service Bulletin 604-35-007, Revision 01, dated
May 6, 2022.
(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; website
bombardier.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(5) You may view this 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 March 14, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-07741 Filed 4-12-23; 8:45 am]
BILLING CODE 4910-13-P