[Federal Register Volume 90, Number 103 (Friday, May 30, 2025)]
[Rules and Regulations]
[Pages 22845-22848]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-09769]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0920; Project Identifier MCAI-2025-00933-T;
Amendment 39-23052; AD 2025-11-06]
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; request for comments.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2025-07-
04, which applied to all Airbus Canada Limited Partnership Model BD-
500-1A11 airplanes. AD 2025-07-04 required a review and disposition of
all existing repairs and damage assessments for affected structure,
corrective actions if necessary, and the prohibition of certain repair
engineering orders (REOs). Since the FAA issued AD 2025-07-04, the FAA
determined that the list of acceptable generic repair engineering
orders (GREOs) specified in table 1 to paragraph (h)(3) of AD 2025-07-
04 was added in error. This AD continues to require review and
disposition of all existing repairs and damage assessments for affected
structure, which includes GREOs that were identified in AD 2025-07-04,
corrective actions if necessary, and the prohibition of certain REOs.
The FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective June 16, 2025.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 27, 2025
(90 FR 16791, April 22, 2025).
The FAA must receive comments on this AD by July 14, 2025.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2025-0920; 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
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For Transport Canada material identified 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 at tc.canada.ca/en/
aviation.
For Airbus Canada material identified in this AD, 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.
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. It is also available at regulations.gov under
Docket No. FAA-2025-0920.
FOR FURTHER INFORMATION CONTACT: Stefanie Roesli, Aviation Safety
Engineer, FAA, FAA, 2200 South 216th St., Des Moines, WA 98198; phone:
206-231-3964; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments
about
[[Page 22846]]
this final rule. Send your comments using a method listed under the
ADDRESSES section. Include ``Docket No. FAA-2025-0920; Project
Identifier MCAI-2025-00933-T'' at the beginning of your comments. The
most helpful comments reference a specific portion of the final rule,
explain the reason for any recommended change, and include supporting
data. The FAA will consider all comments received by the closing date
and may amend this final rule because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this final rule.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this AD. Submissions containing CBI should be sent to
Stefanie Roesli, Aviation Safety Engineer, FAA, FAA, 2200 South 216th
St., Des Moines, WA 98198; phone: 206-231-3964; email:
[email protected]. Any commentary that the FAA receives which
is not specifically designated as CBI will be placed in the public
docket for this rulemaking.
Background
The FAA issued AD 2025-07-04, Amendment 39-23005 (90 FR 16791,
April 22, 2025) (AD 2025-07-04), for all Airbus Canada Limited
Partnership Model BD-500-1A11 airplanes. AD 2025-07-04 was prompted by
an MCAI originated by Transport Canada, which is the aviation authority
for Canada. Transport Canada issued AD CF-2023-70, dated October 5,
2023 (Transport Canada AD CF-2023-70), to correct an unsafe condition.
AD 2025-07-04 required a review and disposition of all existing
repairs and damage assessments for affected structure, corrective
actions if necessary, and the prohibition of certain REOs. The FAA
issued AD 2025-07-04 to address in-service repairs in some structural
areas that require verification and possibly further repair. The unsafe
condition, if not addressed, could result in negative margins for the
load envelopes.
Actions Since AD 2025-07-04 Was Issued
Since the FAA issued AD 2025-07-04, the FAA determined that the
list of acceptable GREOs specified in table 1 to paragraph (h)(3) of AD
2025-07-04 was added in error. In the final rule for AD 2025-07-04, the
FAA added paragraph (h)(3) to that AD to identify GREOs that were
acceptable to comply with the intent of the AD and identified GREOs
issued prior to September 22, 2022, as acceptable. However, those
identified GREOs are the ones that are deactivated and are not
acceptable since they require reassessment to the new loads. Only GREOs
with an issue date later than September 22, 2022, have been validated
by Airbus and are acceptable for use and therefore do not require
reassessment to the new loads.
The FAA has revised paragraph (h)(3) of this AD to remove the
reference to table 1 to paragraph (h)(3), which listed GREOs issued
prior to September 22, 2022, and instead identifies GREOs with an issue
date later than September 22, 2022, as those that have already been
validated and therefore do not require an additional approved
disposition.
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-2025-0920.
Material Incorporated by Reference Under 1 CFR Part 51
This AD requires Airbus Canada Limited Partnership Service Bulletin
BD500-530012, Issue 001, dated September 13, 2023; and Airbus Canada
Limited Partnership Service Bulletin BD500-530012, Issue 002, dated
March 6, 2024; and Transport Canada AD CF-2023-70, dated October 5,
2023; which the Director of the Federal Register approved for
incorporation by reference as of May 27, 2025 (90 FR 16791, April 22,
2025). 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.
FAA's Determination
These products have been approved by the civil 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, that authority has notified the FAA of the unsafe condition
described in the MCAI and material referenced above. The FAA is issuing
this AD after determining that the unsafe condition described
previously is likely to exist or develop on other products of the same
type design.
Requirements of This AD
This AD retains all requirements of AD 2025-07-04, except it
removes the list of GREOs specified in table 1 to paragraph (h)(3) of
AD 2025-07-04 that were added in error and must be reassessed. This AD
requires a review and disposition of all existing repairs and damage
assessments for affected structure, corrective actions if necessary,
and the prohibition of certain REOs.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
incorporation by reference of Transport Canada AD CF-2023-70 is
retained. This AD requires compliance with Transport Canada AD CF-2023-
70 in its entirety through that incorporation, except for any
differences identified as exceptions in the regulatory text of this AD.
Material required by Transport Canada AD CF-2023-70 for compliance will
be available at regulations.gov under Docket No. FAA-2025-0920 after
this AD is published.
FAA's Justification and Determination of the Effective Date
Section 553(b) of the Administrative Procedure Act (APA) (5 U.S.C.
551 et seq.) authorizes agencies to dispense with notice and comment
procedures for rules when the agency, for ``good cause,'' finds that
those procedures are ``impracticable, unnecessary, or contrary to the
public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to
[[Page 22847]]
make rules effective in less than thirty days, upon a finding of good
cause.
The FAA determined that the list of acceptable GREOs specified in
table 1 to paragraph (h)(3) of AD 2025-07-04, which is effective May
27, 2025, was added in error. Instead of specifying only GREOs issued
later than September 22, 2022, which are acceptable, the list of GREOs
in table 1 included those issued before September 22, 2022, which have
not been validated and are not acceptable. Therefore, the FAA is
superseding AD 2025-07-04 to correct this error and ensure deactivated
GREOs are reassessed. Accordingly, notice and opportunity for prior
public comment are impractical and unnecessary, pursuant to 5 U.S.C.
553(b).
In addition, for the foregoing reason(s), the FAA finds that good
cause exists pursuant to 5 U.S.C. 553(d) for making this amendment
effective in less than 30 days.
Regulatory Flexibility Act (RFA)
The requirements of the RFA do not apply when an agency finds good
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and
comment. Because the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 71 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
----------------------------------------------------------------------------------------------------------------
2 work-hours x $85 per hour = $170............ $0 $170 $12,070
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The FAA has received no definitive data on which to base the cost
estimates for the on-condition actions specified in this AD.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the 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, and
(2) Will not affect intrastate aviation in Alaska.
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:
0
a. Removing Airworthiness Directive (AD) 2025-07-04, Amendment 39-23005
(90 FR 16791, April 22, 2025); and
0
b. Adding the following new AD:
2025-11-06 Airbus Canada Limited Partnership (Type Certificate
Previously Held by C Series Aircraft Limited Partnership (CSALP);
Bombardier, Inc.): Amendment 39-23052; Docket No. FAA-2025-0920;
Project Identifier MCAI-2025-00933-T.
(a) Effective Date
This airworthiness directive (AD) is effective June 16, 2025.
(b) Affected ADs
This AD replaces AD 2025-07-04, Amendment 39-23005 (90 FR 16791,
April 22, 2025) (AD 2025-07-04).
(c) Applicability
This AD applies to all Airbus Canada Limited Partnership (Type
Certificate previously held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD-500-1A11 airplanes, certificated
in any category.
(d) Subject
Air Transport Association (ATA) of America Code 51, Standard
practices/structures.
(e) Unsafe Condition
This AD was prompted by a design review of aircraft structural
and stress reports that resulted in a revision of operational loads
for some aircraft flight phases, affecting certain aircraft
sections. The FAA is issuing this AD to address in-service repairs
in some structural areas that require verification and possibly
further repair. The unsafe condition, if not addressed, could result
in negative margins for the load envelopes.
(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-2023-70, dated October 5,
2023 (Transport Canada AD CF-2023-70).
(h) Exceptions to Transport Canada AD CF-2023-70
(1) Where Transport Canada AD CF-2023-70 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where the definition of ``Affected Structure'' in Transport
Canada AD CF-2023-70 specifies ``as identified in Service Bulletin
(SB) BD500-530012, Issue 001, dated 13 September 2023 or later
revisions approved by the Chief, Continuing Airworthiness, Transport
Canada'', this AD requires replacing that text with ``as identified
in Airbus Canada Limited Partnership Service Bulletin BD500-530012,
[[Page 22848]]
Issue 001, dated September 13, 2023; or Airbus Canada Limited
Partnership Service Bulletin BD500-530012, Issue 002, dated March 6,
2024''.
(3) Where paragraph 1.2.1 of Airbus Canada Limited Partnership
Service Bulletin BD500-530012, Issue 001, dated September 13, 2023,
specifies ``Airbus Canada specific Repair Engineering Order (REO)
with an issue date later than December 31, 2022 have already been
validated and therefore do not require an additional approved
disposition'', and where paragraph 1.2.1 of Airbus Canada Limited
Partnership Service Bulletin BD500-530012, Issue 002, dated March 6,
2024, specifies ``Airbus Canada specific Repair Engineering Orders
(REO) with an issue date later than December 31, 2022 have already
been validated and therefore do not require an additional approved
disposition'', this AD requires replacing that text with ``Airbus
Canada specific Repair Engineering Orders (REOs) with an issue date
later than December 31, 2022, and Generic Repair Engineering Orders
(GREOs) with an issue date later than September 22, 2022, have
already been validated and therefore do not require an additional
approved disposition''.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): AIR-520,
Continued Operational Safety Branch, 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
AIR-520, Continued Operational Safety Branch, send it to the
attention of the person identified in paragraph (j) of this AD and
email to: [email protected]. 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, AIR-520,
Continued Operational Safety 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.
(j) Additional Information
For more information about this AD, contact Stefanie Roesli,
Aviation Safety Engineer, FAA, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone: 206-231-3964; email:
[email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the material listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(3) The following material was approved for IBR on May 27, 2025
(90 FR 16791, April 22, 2025).
(i) Airbus Canada Limited Partnership Service Bulletin BD500-
530012, Issue 001, dated September 13, 2023.
(ii) Airbus Canada Limited Partnership Service Bulletin BD500-
530012, Issue 002, dated March 6, 2024.
(iii) Transport Canada AD CF-2023-70, dated October 5, 2023.
(4) For Airbus Canada material identified in this AD, 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.
(5) For Transport Canada material identified 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.
(6) 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.
(7) 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 May 23, 2025.
Lona C. Saccomando,
Acting Deputy Director, Integrated Certificate Management Division,
Aircraft Certification Service.
[FR Doc. 2025-09769 Filed 5-27-25; 11:15 am]
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