[Federal Register Volume 90, Number 118 (Monday, June 23, 2025)]
[Rules and Regulations]
[Pages 26424-26427]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-11449]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-1111; Project Identifier MCAI-2025-00675-R;
Amendment 39-23067; AD 2025-13-01]
RIN 2120-AA64
Airworthiness Directives; Bell Textron Canada Limited Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Bell Textron Canada Limited (BTCL) Model 407 and 427 helicopters. This
AD was prompted by a report that certain expandable blade bolts
installed on the main rotor blade may not have received the correct
heat treatment, which could
[[Page 26425]]
result in stress corrosion cracking of the expandable blade bolts. This
AD requires removing the expandable blade bolts from service and
replacing them with a part eligible for installation. This AD also
prohibits the installation of an affected expandable blade bolt on any
helicopter. The FAA is issuing this AD to address the unsafe condition
on these products.
DATES: This AD is effective July 8, 2025.
The FAA must receive comments on this AD by August 7, 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-2025-1111; 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.
FOR FURTHER INFORMATION CONTACT: Adam Hein, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316)
946-4116; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2025-1111; Project
Identifier MCAI-2025-00675-R'' 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 Adam
Hein, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada AD CF-2025-21, dated April 22, 2025 (referred
to as ``the MCAI''), to address an unsafe condition on BTCL Model 407
and 427 helicopters. The MCAI states that part number 406-310-103-103
expandable blade bolts with certain serial numbers may not have
received the correct heat treatment, which could result in stress
corrosion cracking of the expandable blade bolts installed on the main
rotor blade. The MCAI requires replacing the expandable blade bolts
with serviceable expandable blade bolts. The MCAI also prohibits
installing the affected expandable blade bolts on BTCL Model 407 and
427 helicopters.
The FAA is issuing this AD to address the unsafe condition on these
products. The unsafe condition, if not addressed, could result in
failure of the main rotor blade assembly, detachment of the main rotor
blade, and consequent loss of control of the helicopter.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2025-1111.
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 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 requires removing the expandable blade bolts from service
and installing an expandable blade bolt that does not have an affected
serial number. This AD also prohibits installing an affected expandable
blade bolt on any helicopter.
Justification for Immediate Adoption 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 make rules effective in less than thirty days,
upon a finding of good cause.
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies forgoing notice and comment prior to adoption of this rule
because expandable blade bolts are critical components that, if
improperly heat-treated, could be subject to stress corrosion cracking.
Stress corrosion cracking of the expandable blade bolts could result in
the failure of the main rotor blade assembly, detachment of the main
rotor blade, and consequent loss of control of the helicopter. This
failure could happen at any time without any previous indications.
Additionally, the initial actions required by this AD must be
accomplished within 30 hours time-in-service or 30 days, whichever
occurs first, which is shorter than the time necessary for the public
to comment and for publication of the final rule. Accordingly, notice
and opportunity for prior public comment are impracticable
[[Page 26426]]
and contrary to the public interest pursuant to 5 U.S.C. 553(b).
In addition, 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,
for the same reasons the FAA found good cause to forgo notice and
comment.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (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 prior notice and
comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 946 helicopters of U.S.
registry. There are 20 expandable blade bolts identified as having this
unsafe condition, and up to 4 expandable blade bolts could be installed
per helicopter. The FAA has no way of knowing the number of helicopters
of U.S. registry that may have an affected expandable blade bolt
installed. The estimated cost on U.S. operators reflects the costs
based on the number of expandable blade bolts that need to be replaced.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
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Cost on U.S.
Action Labor cost Parts cost Cost per product operators
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Replace expandable blade bolt (up 2 work-hours x $85 $5,271 per bolt.... Up to $21,764...... $108,820
to four bolts per helicopter). per hour = $170.
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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 adding the following new airworthiness
directive:
2025-13-01 Bell Textron Canada Limited: Amendment 39-23067; Docket
No. FAA-2025-1111; Project Identifier MCAI-2025-00675-R.
(a) Effective Date
This airworthiness directive (AD) is effective July 8, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bell Textron Canada Limited Model 407 and 427
helicopters, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 6210, Main Rotor
Blades.
(e) Unsafe Condition
This AD was prompted by a report that certain expandable blade
bolts installed on the main rotor blade may not have received the
correct heat treatment, which could lead to stress corrosion
cracking of the expandable blade bolts. The FAA is issuing this AD
to prevent stress corrosion cracking of the expandable blade bolts
installed on the main rotor blade. The unsafe condition, if not
addressed, could result in failure of the main rotor blade assembly,
detachment of the main rotor blade, and consequent loss of control
of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 30 hours time-in-service or 30 days, whichever occurs
first after the effective date of this AD, remove from service each
affected part and replace with a part eligible for installation.
(h) Parts Installation Prohibition
As of the effective date of this AD, do not install an affected
part as defined in this AD on any helicopter.
(i) Definitions
For the purpose of this AD, the following definitions apply:
(1) An ``affected part'' is an expandable blade bolt having part
number (P/N) 406-310-103-103 and a serial number SLFS9386 through
SLFS9405 inclusive.
(2) A ``part eligible for installation'' is an expandable blade
bolt having P/N 406-310-103-103 that does not have a serial number
listed in paragraph (i)(1) of this AD.
(j) Alternative Methods of Compliance (AMOCs)
(1) 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 local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the International Validation Branch, send
it to the attention of the person identified in paragraph (k) of
this AD and email to: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
[[Page 26427]]
(k) Additional Information
For more information about this AD, contact Adam Hein, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; phone: (316) 946-4116; email: [email protected].
(l) Material Incorporated by Reference
None.
Issued on June 17, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-11449 Filed 6-18-25; 11:15 am]
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