Published 2023-04-13 · Federal Register document 2023-07741
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[109]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-06-04
- Effective date printed in this edition
- 2023-05-18
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective May 18, 2023.
Exact source excerpt. Text positions 9833–9919, end exclusive, in the original decoded publication. SHA-256: 2844c2467bc9760770ff3ce82e23e561c2c52c24bbfeb16483685ba1efb7fb83
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 9919–9948, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 9948–10630, end exclusive, in the original decoded publication. SHA-256: ee42462b59027a2e73e6d0693a593518e45ebbc459d569df6eb249437ba586a9
Subject
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen
System.
[[Page 22364]]
Exact source excerpt. Text positions 10630–10732, end exclusive, in the original decoded publication. SHA-256: b7736ad6b534a328ad4db01787fb38a6ed4714f0af76e970aa83fa51a9aa6820
Unsafe Condition
(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.
Exact source excerpt. Text positions 10732–11206, end exclusive, in the original decoded publication. SHA-256: 09ae8d2af56992671693398c86022a3906380dc1d37bda99b9968ae9c2fe7ded
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11206–11308, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Inspection and Replacement
(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.
Exact source excerpt. Text positions 11308–12980, end exclusive, in the original decoded publication. SHA-256: 31acc1d3ca6bdb68c934d5052f27590e02f33ccd0d29b49d64e6b519ff12e572
Credit for Previous Actions
(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.
Exact source excerpt. Text positions 12980–13324, end exclusive, in the original decoded publication. SHA-256: e5daf981e3215ed5a841f0cbb76c320490e9d971b39a36923edbbf41b4408aea
Additional AD Provisions
(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.
Exact source excerpt. Text positions 13324–14599, end exclusive, in the original decoded publication. SHA-256: 7727a89f2d99bd1f3a8dc56714b7ac03bf2a116d38c3dc83298a23104e18763e
Additional Information
(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.
Exact source excerpt. Text positions 14599–15284, end exclusive, in the original decoded publication. SHA-256: 0ab44b1d99c184709b1382bf860453ed8a84dd22a7e1fda47bfde35ae9bac566
Material Incorporated by Reference
(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">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 the availability of this material at
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 15284–16707, end exclusive, in the original decoded publication. SHA-256: cf96064d69fba876ed25b0f6fde621ec5e7457c2a52ed92f936a7ff922029ef0
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2023-06-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: c1ed489de6d0580c2d6b7fbabcd3a5e5124f7966e3703bb8816785d0101dbc5c. Source manifest: bcd285b59a9f4a8497cf7f099de757477b47af2470cad8622a5fc62019e1f1d1.
Official source · 2023-04-13
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[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:
<bullet> 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">ac.yul@aero.bombardier.com; website
bombardier.com.
<bullet> 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:
<bullet> Service Bulletin 600-0777, dated December 13, 2021.
<bullet> Service Bulletin 601-1109, Revision 01, dated May 6, 2022.
<bullet> 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">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 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
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