Published 2023-12-18 · Federal Register document 2023-27679
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model CL-600-2B16 (604 Variant) airplanes. This AD was prompted by sleeve loops on some passenger oxygen mask lanyards that had improper crimping and unsealed ends. This AD requires an inspection of the passenger oxygen mask lanyards and replacement of defective oxygen mask lanyards. This AD also prohibits the installation of affected parts. 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[340]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-24-05
- Effective date printed in this edition
- 2024-01-22
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective January 22, 2024.
Exact source excerpt. Text positions 10583–10673, end exclusive, in the original decoded publication. SHA-256: 68bf451ca613015225dca1c1b7562f6119a6b9a7ddcc28f146fb8cba81609426
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10673–10702, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Bombardier, Inc., Model CL-600-2B16 (604
Variant) airplanes, certificated in any category, serial numbers
identified in Bombardier Service Bulletin 605-35-008, dated October
28, 2022.
Exact source excerpt. Text positions 10702–10932, end exclusive, in the original decoded publication. SHA-256: 0d9ffc08c967fbcfd3f7cd9f4be645fa0eb42473a3f2be7f6995c0102de486e5
Subject
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen
System.
Exact source excerpt. Text positions 10932–11018, end exclusive, in the original decoded publication. SHA-256: a551b7fc354bbde3ad1bd9d2887f908466428279296823a0e940907ebcb2de2b
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by sleeve loops on some passenger oxygen
mask lanyards that had improper crimping and unsealed ends. The FAA
is issuing this AD to address the defective oxygen mask lanyards.
The unsafe condition, if not addressed, could result in no oxygen
flow to the mask during an emergency.
Exact source excerpt. Text positions 11018–11349, end exclusive, in the original decoded publication. SHA-256: 40cfdcdf3a97835fb0a176a2cb64c4ebc29b542c48ce0df7d46225e9e686639a
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11349–11451, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Inspection of the Passenger Oxygen Mask Assemblies
(g) Inspection of the Passenger Oxygen Mask Assemblies
Within 48 months from the effective date of this AD, visually
inspect the passenger oxygen mask lanyards in the cabin or lavatory
oxygen box assemblies as applicable for crimped lanyards and sealed
ends, in accordance with paragraph 2.C. of the Accomplishment
Instructions of Bombardier Service Bulletin 605-35-008, dated
October 28, 2022.
(1) If all passenger oxygen mask lanyards are crimped and the
lanyard ends are sealed: No further action is required by this
paragraph.
(2) If any passenger oxygen mask lanyard is not crimped
properly, or any lanyard end is not sealed properly: Before further
flight, replace the passenger oxygen mask lanyard in accordance with
Section 2.D. of the Accomplishment Instructions of Bombardier
[[Page 87336]]
Service Bulletin 605-35-008, dated October 28, 2022.
Exact source excerpt. Text positions 11451–12331, end exclusive, in the original decoded publication. SHA-256: d4fea071bd9f9e0a11d5eb4a6598e4213a7ebb936de252b4b8ccfcf2c1b99683
Parts Installation Prohibition
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install, on
any airplane, a passenger oxygen mask lanyard assembly provided with
an oxygen box lanyard kit containing a lot number in paragraph
(h)(1) or (2) of this AD.
(1) Oxygen box lanyard kit part number (P/N) CDKC29-006-501, lot
number 2011007411, 2012010412, 2101018703, 2101035167, 2102030139,
2104003817, or 2105005522.
(2) Oxygen box lanyard kit P/N CDKC29-006-503, lot number
2011029525, 2012006900, 2103007412, or 2103029992.
Exact source excerpt. Text positions 12331–12875, end exclusive, in the original decoded publication. SHA-256: b7a1bbcbf8f9c084dc73228f0dc4b6996ed5448c58ffe3228933f67f60c825bd
Additional AD Provisions
(i) Additional AD Provisions
The following provisions also apply to this AD:
(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 manager,
International Validation Branch, mail it to 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, International
Validation 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 12875–14121, end exclusive, in the original decoded publication. SHA-256: ece3bcdc0653d5d59cd083f74781d97ad96ec4f45929364aee4599c84c39b62c
Additional Information
(j) Additional Information
(1) Refer to Transport Canada AD CF-2023-06, dated February 9,
2023, for related information. This Transport Canada AD may be found
in the AD docket at regulations.gov under Docket No. FAA-2023-1505.
(2) For more information about this AD, contact Gabriel Kim,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
Exact source excerpt. Text positions 14121–14555, end exclusive, in the original decoded publication. SHA-256: 48c62bb7204fab7b42b6d9e0a00bc8dfe548a9702b1232a1ad6b06c7a54926af
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 605-35-008, dated October 28,
2022.
(ii) [Reserved]
(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 material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit: www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Exact source excerpt. Text positions 14555–15790, end exclusive, in the original decoded publication. SHA-256: 3a7bf331b1673a05fac07f08b0b5e0416e498687fbff6f995e8452cd9d06bee2
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 2023-24-05 · 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.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 19df0b5b9c8f9187907166e7b0841b62d2df3863d3466c6c6e6a8b9cfe5a1924. Source manifest: 7e2ffc78a046c630bbc60230dec7bda35685db1726820d4a8b97bd5e1a8ae20d.
Official source · 2023-12-18
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 241 (Monday, December 18, 2023)]
[Rules and Regulations]
[Pages 87334-87336]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-27679]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1505; Project Identifier MCAI-2023-00246-T;
Amendment 39-22622; AD 2023-24-05]
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-600-2B16 (604 Variant) airplanes.
This AD was prompted by sleeve loops on some passenger oxygen mask
lanyards that had improper crimping and unsealed ends. This AD requires
an inspection of the passenger oxygen mask lanyards and replacement of
defective oxygen mask lanyards. This AD also prohibits the installation
of affected parts. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective January 22, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 22,
2024.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1505; 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-2023-1505.
FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aviation Safety Engineer,
FAA, 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-600-2B16 (604 Variant) airplanes. The NPRM published in
the Federal Register on July 25, 2023 (88 FR 47827). The NPRM was
prompted by AD CF-2023-06, dated February 9, 2023 (referred to after
this as the MCAI), issued by Transport Canada, which is the aviation
authority for Canada. The MCAI states the sleeve loops on certain
passenger oxygen mask lanyards were found to have improper crimping and
unsealed ends.
In the NPRM, the FAA proposed to require an inspection of the
passenger oxygen mask lanyards and replacement of defective oxygen mask
lanyards. In the NPRM, the FAA also proposed to prohibit the
installation of affected parts. The FAA is issuing this AD to address
these defective oxygen mask lanyards, which could result in no oxygen
flow to the mask during an emergency.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1505.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Bombardier. The following presents
the comment received on the NPRM and the FAA's response to the comment.
Request for Removal of Certain Variants
Bombardier requested that the proposed AD be revised to remove
reference to 601-3A and 601-3R Variants. The commenter stated that the
proposed AD only applies to Model CL-600-2B16 (604 Variant) airplanes
(Challenger 605 designation). Bombardier noted that the airplane serial
numbers given in Bombardier Service Bulletin 605-35-008, dated October
28, 2022, and referenced in Transport Canada AD CF-2023-06, are all
Model CL-600-2B16 (604 Variant) airplanes.
The FAA agrees for the reasons provided. The FAA revised the
Summary, Background, and paragraph (c) of this AD accordingly.
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 reviewed the relevant data, considered the
comments received, 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, and any other changes described previously, 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 Bombardier Service Bulletin 605-35-008, dated
October 28, 2022. This service information specifies procedures for a
visual inspection of the existing passenger oxygen mask lanyards
installed in the cabin or lavatory oxygen box assemblies, and
replacement of the defective oxygen mask lanyards. The
[[Page 87335]]
defective oxygen mask lanyards had improperly crimped sleeve loops and
unsealed ends.
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 120 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.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspection............................ 1 work-hour x $85 per $0 $85 $10,200
hour = $85.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition action 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 this on-condition action:
Estimated Costs of On-Condition Actions
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replacement................................ 2 work-hours x $85 per hour = $170. $1,149 $1,319
----------------------------------------------------------------------------------------------------------------
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all costs of this 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
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:
2023-24-05 Bombardier, Inc.: Amendment 39-22622; Docket No. FAA-
2023-1505; Project Identifier MCAI-2023-00246-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 22, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model CL-600-2B16 (604
Variant) airplanes, certificated in any category, serial numbers
identified in Bombardier Service Bulletin 605-35-008, dated October
28, 2022.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen
System.
(e) Unsafe Condition
This AD was prompted by sleeve loops on some passenger oxygen
mask lanyards that had improper crimping and unsealed ends. The FAA
is issuing this AD to address the defective oxygen mask lanyards.
The unsafe condition, if not addressed, could result in no oxygen
flow to the mask during an emergency.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection of the Passenger Oxygen Mask Assemblies
Within 48 months from the effective date of this AD, visually
inspect the passenger oxygen mask lanyards in the cabin or lavatory
oxygen box assemblies as applicable for crimped lanyards and sealed
ends, in accordance with paragraph 2.C. of the Accomplishment
Instructions of Bombardier Service Bulletin 605-35-008, dated
October 28, 2022.
(1) If all passenger oxygen mask lanyards are crimped and the
lanyard ends are sealed: No further action is required by this
paragraph.
(2) If any passenger oxygen mask lanyard is not crimped
properly, or any lanyard end is not sealed properly: Before further
flight, replace the passenger oxygen mask lanyard in accordance with
Section 2.D. of the Accomplishment Instructions of Bombardier
[[Page 87336]]
Service Bulletin 605-35-008, dated October 28, 2022.
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install, on
any airplane, a passenger oxygen mask lanyard assembly provided with
an oxygen box lanyard kit containing a lot number in paragraph
(h)(1) or (2) of this AD.
(1) Oxygen box lanyard kit part number (P/N) CDKC29-006-501, lot
number 2011007411, 2012010412, 2101018703, 2101035167, 2102030139,
2104003817, or 2105005522.
(2) Oxygen box lanyard kit P/N CDKC29-006-503, lot number
2011029525, 2012006900, 2103007412, or 2103029992.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(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 manager,
International Validation Branch, mail it to 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, International
Validation 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-2023-06, dated February 9,
2023, for related information. This Transport Canada AD may be found
in the AD docket at regulations.gov under Docket No. FAA-2023-1505.
(2) For more information about this AD, contact Gabriel Kim,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 605-35-008, dated October 28,
2022.
(ii) [Reserved]
(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 material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit: www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on November 29, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-27679 Filed 12-15-23; 8:45 am]
BILLING CODE 4910-13-P
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- Text SHA-256
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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