Published 2023-10-05 · Federal Register document 2023-22086
Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500- 1A11 airplanes. This AD was prompted by a report the engine fire extinguishing control and indication system did not illuminate correctly. This AD requires installing a software update to the integrated cockpit control panel (ICCP) remote data concentrator (RDC), as specified in a Transport Canada AD, which is incorporated by reference. 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[280]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-20-01
- Effective date printed in this edition
- 2023-11-09
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective November 9, 2023.
Exact source excerpt. Text positions 10320–10410, end exclusive, in the original decoded publication. SHA-256: dfb0c508c4ca8baca0ab5e880b3ff4f13e8b08cba4211e4584e0dde9d0e2586a
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10410–10439, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Airbus Canada Limited Partnership (type
certificate previously held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11
airplanes, certificated in any category, as identified in Transport
Canada AD CF-2023-28, dated May 4, 2023 (Transport Canada AD CF-
2023-28).
Exact source excerpt. Text positions 10439–10799, end exclusive, in the original decoded publication. SHA-256: b49431033d5da1947f6d8319e191e68e095018aa1d21589c6b110e003c64fc88
Subject
(d) Subject
Air Transport Association (ATA) of America Code: 26, Fire
protection.
Exact source excerpt. Text positions 10799–10888, end exclusive, in the original decoded publication. SHA-256: 5e9470216303312357ce51bb4ae05a673a5538d9a75c65945d6f4beadd688f78
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report the engine fire extinguishing
control and indication system did not illuminate correctly. The FAA
is issuing this AD to address the misleading indication given by the
AVAIL legend on BTL 1 and BTL 2 push button annunciators (PBAs) that
will affect the crew's assessment of the situation. The unsafe
condition, if not addressed, could result in the crew hesitating to
extinguish an engine fire despite having access to a functional
engine fire extinguishing system, or reselecting the FIRE PBA,
resulting in loss of the ability to isolate and extinguish the fire.
Exact source excerpt. Text positions 10888–11519, end exclusive, in the original decoded publication. SHA-256: 9d260e4dbef2b05dbde55bad15fe06395453936da12ef852ab28f0407e7a71d4
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11519–11621, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, Transport Canada AD CF-2023-28.
[[Page 69020]]
Exact source excerpt. Text positions 11621–11835, end exclusive, in the original decoded publication. SHA-256: 38eda164ea8d83e1e58280ba2b775e9b7d69b43b86fee45ca429cdc67121ff20
Exceptions to Transport Canada AD CF-2023-28
(h) Exceptions to Transport Canada AD CF-2023-28
(1) Where Transport Canada AD CF-2023-28 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where Transport Canada AD CF-2023-28 specifies installing
software updates on the integrated cockpit control panel remote data
concentrator using a USB-type device, this AD also allows the use of
a portable maintenance access terminal (PMAT)-type device.
Note 1 to paragraph (h)(2): When using a PMAT-type device,
guidance for upgrading the software can be found in Airbus Canada
Limited Partnership Service Bulletin BD500-311001, Issue 001, dated
March 14, 2023.
Exact source excerpt. Text positions 11835–12498, end exclusive, in the original decoded publication. SHA-256: babded4d5c05aeda686c61369c7f2a2259abda5984e56fe50f31cf63f844054c
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 of the
International Validation Branch, mail it to the address identified
in paragraph (j)(1) 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 Airbus Canada
Limited Partnership's Transport Canada Design Approval Organization
(DAO). If approved by the DAO, the approval must include the DAO-
authorized signature.
(3) Required for Compliance (RC): Except as required by
paragraph (i)(2) of this AD, if any service information contains
procedures or tests that are identified as RC, those procedures and
tests must be done to comply with this AD; any procedures or tests
that are not identified as RC are recommended. Those procedures and
tests that are not identified as RC may be deviated from using
accepted methods in accordance with the operator's maintenance or
inspection program without obtaining approval of an AMOC, provided
the procedures and tests identified as RC can be done and the
airplane can be put back in an airworthy condition. Any
substitutions or changes to procedures or tests identified as RC
require approval of an AMOC.
Exact source excerpt. Text positions 12498–14516, end exclusive, in the original decoded publication. SHA-256: 244eb3a245dde207bf982f90c894e3671b67a07bcad2b4f1d10eaf4d4f10cb0b
Additional Information
(j) Additional Information
(1) For more information about this AD, contact William
Reisenauer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 516-228-7300; email: [email protected].
(2) For Airbus Canada Limited Partnership service information
identified in this AD that is not incorporated by reference, contact
Airbus Canada Limited Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Qu[eacute]bec J7N 3C6, Canada; telephone 450-476-7676;
email [email protected]; website a220world.airbus.com. This Airbus
Canada Limited Partnership service information is also available at
the address specified in paragraph (k)(4) of this AD.
Exact source excerpt. Text positions 14516–15210, end exclusive, in the original decoded publication. SHA-256: 65f20cec7ddaef2feaa38d1b8e78443f13b8b9a936dccdb799015c6aafb86c56
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) Transport Canada AD CF-2023-28, dated May 4, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF-2023-28, contact Transport
Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-
3639; email: [email protected]; website: tc.canada.ca/en/
aviation.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th Street, 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 15210–16458, end exclusive, in the original decoded publication. SHA-256: 35547f722d70423fbcce7492de052b969737184db03714c934c6c6d1b6527a89
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 2023-20-01 · 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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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: 61534d9e15d1b75f502a75ed7d3d291d6a390961166e0a2342019799cc42b7e1. Source manifest: cc2f3ef4d1c99593e590a28ced79bd80ba2c5204561f8bee2037f953b514ad93.
Official source · 2023-10-05
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 192 (Thursday, October 5, 2023)]
[Rules and Regulations]
[Pages 69018-69020]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-22086]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1501; Project Identifier MCAI-2023-00647-T;
Amendment 39-22560; AD 2023-20-01]
RIN 2120-AA64
Airworthiness Directives; Airbus Canada Limited Partnership (Type
Certificate Previously Held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-
1A11 airplanes. This AD was prompted by a report the engine fire
extinguishing control and indication system did not illuminate
correctly. This AD requires installing a software update to the
integrated cockpit control panel (ICCP) remote data concentrator (RDC),
as specified in a Transport Canada AD, which is incorporated by
reference. The FAA is issuing this AD to address the unsafe condition
on these products.
DATES: This AD is effective November 9, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 9,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1501; 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 material incorporated by reference in this AD, contact
Transport Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-
3639; email [email protected]; website tc.canada.ca/en/aviation.
<bullet> You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
Des Moines, WA. For information on the availability of this material at
the FAA, call 206-231-3195. It is also available in the AD docket at
regulations.gov under Docket No. FAA-2023-1501.
FOR FURTHER INFORMATION CONTACT: William Reisenauer, 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 Airbus Canada
Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. The
NPRM published in the Federal Register on July 20, 2023 (88 FR 46702).
The NPRM was prompted by AD CF-2023-28, dated May 4, 2023, issued by
Transport Canada, which is the aviation authority for Canada (Transport
Canada AD CF-2023-28) (also referred to as the MCAI). The MCAI states a
deficiency in the design of the engine fire extinguishing control and
indication system was discovered. After the loss of one hot battery DC
bus, the AVAIL legend on BTL 1 and BTL 2 push button annunciators
(PBAs) will not illuminate green upon pressing the corresponding ENG
FIRE PBA. This condition affects both L ENG FIRE and R ENG FIRE PBAs on
the overhead panel. The misleading indication given by the AVAIL legend
on BTL 1 and BTL 2 PBAs will affect the crew's assessment of the
situation. The crew may hesitate to extinguish an engine fire despite
having access to a functional engine fire extinguishing system, or may
reselect the FIRE PBA, resulting in loss of the ability to isolate and
extinguish the fire.
In the NPRM, the FAA proposed to require installing a software
update to the ICCP RDC, as specified in Transport Canada AD CF-2023-28.
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-2023-1501.
Discussion of Final Airworthiness Directive
Comments
The FAA received one comment from Air Line Pilots Association,
International (ALPA) who supported the NPRM without change.
The FAA received an additional comment from Delta Air Lines
(Delta). The following presents the comment received on the NPRM and
the FAA's response.
Request To Clarify Software Installation Requirements
Delta requested that an additional exception be added to paragraph
(h) of the proposed AD to clarify that it is acceptable to use a
different method of upgrading the software, using Airbus Canada Limited
Partnership Service Bulletin BD500-311001, Issue 001, dated March 14,
2023, only as a reference. Delta explained that it has a different
policy for installing software that requires the use of a Portable
Maintenance Access Terminal (PMAT), model PMAT2000, instead of a USB
device.
The FAA partially agrees with the proposed changes. The FAA agrees
to clarify that the PMAT method is
[[Page 69019]]
permitted, but the FAA will not require the use of a specific model of
PMAT. Also, using the service information as a reference must be
specified in a note rather than in the paragraph itself. Therefore, a
single paragraph (h)(2) has been added to this AD to provide this
clarification, and a note has been added regarding the use of Airbus
Canada Limited Partnership Service Bulletin BD500-311001, Issue 001,
dated March 14, 2023, as a reference.
Conclusion
These products have been approved by the aviation authority of
another country and are 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 these products. 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
Transport Canada AD CF-2023-28 specifies procedures for installing
the software update to the ICCP RDC to restore the intended
functionality of the PBA green indications. This material is reasonably
available because the interested parties have access to it through
their normal course of business or by the means identified in the
ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 76 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
----------------------------------------------------------------------------------------------------------------
Up to 6 work-hours x $85 per hour Up to $7,500........ Up to $8,010....... Up to $608,760.
= Up to $510.
----------------------------------------------------------------------------------------------------------------
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:
2023-20-01 Airbus Canada Limited Partnership (Type Certificate
Previously Held by C Series Aircraft Limited Partnership (CSALP);
Bombardier, Inc.): Amendment 39-22560; Docket No. FAA-2023-1501;
Project Identifier MCAI-2023-00647-T.
(a) Effective Date
This airworthiness directive (AD) is effective November 9, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Canada Limited Partnership (type
certificate previously held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11
airplanes, certificated in any category, as identified in Transport
Canada AD CF-2023-28, dated May 4, 2023 (Transport Canada AD CF-
2023-28).
(d) Subject
Air Transport Association (ATA) of America Code: 26, Fire
protection.
(e) Unsafe Condition
This AD was prompted by a report the engine fire extinguishing
control and indication system did not illuminate correctly. The FAA
is issuing this AD to address the misleading indication given by the
AVAIL legend on BTL 1 and BTL 2 push button annunciators (PBAs) that
will affect the crew's assessment of the situation. The unsafe
condition, if not addressed, could result in the crew hesitating to
extinguish an engine fire despite having access to a functional
engine fire extinguishing system, or reselecting the FIRE PBA,
resulting in loss of the ability to isolate and extinguish the fire.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, Transport Canada AD CF-2023-28.
[[Page 69020]]
(h) Exceptions to Transport Canada AD CF-2023-28
(1) Where Transport Canada AD CF-2023-28 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where Transport Canada AD CF-2023-28 specifies installing
software updates on the integrated cockpit control panel remote data
concentrator using a USB-type device, this AD also allows the use of
a portable maintenance access terminal (PMAT)-type device.
Note 1 to paragraph (h)(2): When using a PMAT-type device,
guidance for upgrading the software can be found in Airbus Canada
Limited Partnership Service Bulletin BD500-311001, Issue 001, dated
March 14, 2023.
(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 of the
International Validation Branch, mail it to the address identified
in paragraph (j)(1) 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 Airbus Canada
Limited Partnership's Transport Canada Design Approval Organization
(DAO). If approved by the DAO, the approval must include the DAO-
authorized signature.
(3) Required for Compliance (RC): Except as required by
paragraph (i)(2) of this AD, if any service information contains
procedures or tests that are identified as RC, those procedures and
tests must be done to comply with this AD; any procedures or tests
that are not identified as RC are recommended. Those procedures and
tests that are not identified as RC may be deviated from using
accepted methods in accordance with the operator's maintenance or
inspection program without obtaining approval of an AMOC, provided
the procedures and tests identified as RC can be done and the
airplane can be put back in an airworthy condition. Any
substitutions or changes to procedures or tests identified as RC
require approval of an AMOC.
(j) Additional Information
(1) For more information about this AD, contact William
Reisenauer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 516-228-7300; email: [email protected].
(2) For Airbus Canada Limited Partnership service information
identified in this AD that is not incorporated by reference, contact
Airbus Canada Limited Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Qu[eacute]bec J7N 3C6, Canada; telephone 450-476-7676;
email [email protected]; website a220world.airbus.com. This Airbus
Canada Limited Partnership service information is also available at
the address specified in paragraph (k)(4) of this AD.
(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) Transport Canada AD CF-2023-28, dated May 4, 2023.
(ii) [Reserved]
(3) For Transport Canada AD CF-2023-28, contact Transport
Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-663-
3639; email: [email protected]; website: tc.canada.ca/en/
aviation.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th Street, 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 September 25, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-22086 Filed 10-4-23; 8:45 am]
BILLING CODE 4910-13-P
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- Text SHA-256
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