Special Conditions: Canard Aerospace Corporation, DeHavilland Model DHC-8-400 Series Airplane; Electronic System Security Protection From Unauthorized External Access, 13055-13057 [2025-04664]
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Federal Register / Vol. 90, No. 53 / Thursday, March 20, 2025 / Rules and Regulations
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This document of the Department of
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Treena V. Garrett,
Federal Register Liaison Officer, U.S.
Department of Energy.
[FR Doc. 2025–04474 Filed 3–19–25; 8:45 am]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2025–0078; Special
Conditions No. 25–876–SC]
Special Conditions: Canard Aerospace
Corporation, DeHavilland Model DHC–
8–400 Series Airplane; Electronic
System Security Protection From
Unauthorized External Access
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for a supplemental type
certificate (STC) to install a digital
systems architecture on the DeHavilland
Model DHC–8–400 series airplane. This
airplane, as modified by the Canard
Aerospace Corporation (Canard), will
have a novel or unusual design feature
when compared to the state of
technology envisioned in the
airworthiness standards for transportcategory airplanes. This design feature
is the installation of a digital systems
architecture that will allow increased
connectivity to and access from external
network sources (e.g., operator
networks, wireless devices, internet
connectivity, service provider satellite
communications, electronic flight bags,
etc.) to the airplane’s previously isolated
electronic assets (networks, systems,
and databases). The applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for this design feature. These special
conditions contain the additional safety
standards that the Administrator
considers necessary to establish a level
of safety equivalent to that established
by the existing airworthiness standards.
DATES: This action is effective on
Canard on March 20, 2025. Send
comments on or before May 5, 2025.
ADDRESSES: Send comments identified
by Docket No. FAA–2025–0078 using
any of the following methods:
• Federal eRegulations Portal: Go to
www.regulations.gov and follow the
online instructions for sending your
comments electronically.
• Mail: Send comments to Docket
Operations, M–30, U.S. Department of
Transportation (DOT), 1200 New Jersey
Avenue SE, Room W12–140, West
Building Ground Floor, Washington, DC
20590–0001.
• Hand Delivery or Courier: Take
comments to Docket Operations in
Room W12–140 of the West Building
Ground Floor at 1200 New Jersey
SUMMARY:
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13055
Avenue SE, Washington, DC, between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays.
• Fax: Fax comments to Docket
Operations at 202–493–2251.
Docket: Background documents or
comments received may be read at
www.regulations.gov at any time.
Follow the online instructions for
accessing the docket or go to Docket
Operations in Room W12–140 of the
West Building Ground Floor at 1200
New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Thuan T. Nguyen, Avionics Software
and Components Unit, AIR–626D,
Technical Policy Branch, Aircraft
Certification Service, Federal Aviation
Administration, 2200 South 216th
Street, Des Moines, Washington 98198;
telephone (206) 231–3365; email:
Thuan.T.Nguyen@faa.gov.
SUPPLEMENTARY INFORMATION: The
substance of these special conditions
has been published in the Federal
Register for public comment in several
prior instances with no substantive
comments received. Therefore, the FAA
finds, pursuant to 14 CFR 11.38(b), that
new comments are unlikely, and notice
and comment prior to this publication
are unnecessary.
Privacy
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in title 14,
Code of Federal Regulations (14 CFR)
11.35, the FAA will post all comments
received without change to
www.regulations.gov, including any
personal information you provide. The
FAA will also post a report
summarizing each substantive verbal
contact received about these special
conditions.
Confidential Business Information
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 these special
conditions contain commercial or
financial information that is customarily
treated as private, that you actually treat
as private, and that is relevant or
responsive to these special conditions, 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
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Federal Register / Vol. 90, No. 53 / Thursday, March 20, 2025 / Rules and Regulations
will treat such marked submissions as
confidential under the FOIA, and the
indicated comments will not be placed
in the public docket of these special
conditions. Send submissions
containing CBI to the individual listed
in the FOR FURTHER INFORMATION
CONTACT section above. Comments the
FAA receives, which are not specifically
designated as CBI, will be placed in the
public docket for these special
conditions.
Comments Invited
The FAA invites interested people to
take part in this rulemaking by sending
written comments, data, or views. The
most helpful comments reference a
specific portion of the special
conditions, explain the reason for any
recommended change, and include
supporting data.
The FAA will consider all comments
received by the closing date for
comments. The FAA may change these
special conditions based on the
comments received.
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Background
On April 15, 2024, Canard applied for
a supplemental type certificate to install
a digital systems architecture on the
DeHavilland Model DHC–8–400 series
airplane that will allow increased
connectivity to and access from external
network sources (e.g., operator
networks, wireless devices, internet
connectivity, service provider satellite
communications, electronic flight bags,
etc.) to the airplane’s previously isolated
electronic assets (networks, systems,
and databases). The DeHavilland Model
DHC–8–400 series airplane is a twinengine airplane with a passenger
capacity of 68 and a maximum takeoff
weight of 61,700 pounds.
Type Certification Basis
Under the provisions of title 14, Code
of Federal Regulations (14 CFR) 21.101,
Canard must show that the Model
DeHavilland DHC–8–400 series
airplane, as changed, continues to meet
the applicable provisions of the
regulations listed in Type Certificate No.
A13NM or the applicable regulations in
effect on the date of application for the
change, except for earlier amendments
as agreed upon by the FAA.
If the Administrator finds that the
applicable airworthiness regulations
(e.g., 14 CFR part 25) do not contain
adequate or appropriate safety standards
for the listed airplanes because of a
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The Model DeHavilland DHC–8–400
series airplane, as modified by Canard,
will incorporate the following novel or
unusual design feature(s):
The installation of a digital systems
architecture that will allow increased
connectivity to and access from external
network sources, (e.g., operator
networks, wireless devices, internet
connectivity, service provider satellite
communications, electronic flight bags,
etc.) to the airplane’s previously isolated
electronic assets (networks, systems,
and databases).
and presents security vulnerabilities
related to the introduction of computer
viruses and worms, user errors, and
intentional sabotage of airplane
electronic assets (networks, systems,
and databases) critical to the safety and
maintenance of the airplane.
The existing FAA regulations did not
anticipate these networked airplanesystem architectures. Furthermore, these
regulations and the current guidance
material do not address potential
security vulnerabilities, which could be
exploited by unauthorized access to
airplane networks, data buses, and
servers. Therefore, these special
conditions ensure that the security (i.e.,
confidentiality, integrity, and
availability) of the airplane’s systems is
not compromised by unauthorized
wired or wireless electronic
connections. This includes ensuring
that the security of the airplane’s
systems is not compromised during
maintenance of the airplane’s electronic
systems. These special conditions also
require the applicant to provide
appropriate instructions to the operator
to maintain all electronic-system
safeguards that have been implemented
as part of the original network design so
that this feature does not allow or
introduce security threats.
These special conditions contain the
additional safety standards that the
Administrator considers necessary to
establish a level of safety equivalent to
that established by the existing
airworthiness standards.
Discussion
Applicability
The DeHavilland Model DHC–8–400
series airplanes electronic system
architecture and network configuration
change is novel or unusual for
commercial transport airplanes because
it may allow increased connectivity to
and access from external network
sources, airline operations, and
maintenance networks, to the airplane
control domain, and airline information
services domain. The airplane’s control
domain and airline information-services
domain perform functions required for
the safe operation and maintenance of
the airplane. Previously, these domains
had very limited connectivity with
external network sources. This data
network and design integration creates a
potential for unauthorized persons to
access the airplane’s control domain
and airline information-services domain
As discussed above, these special
conditions are applicable to the
DeHavilland DHC–8–400 series
airplane, as modified by Canard. Should
Canard apply at a later date for a
supplemental type certificate to modify
any other model included on Type
Certificate No. A13NM to incorporate
the same novel or unusual design
feature, these special conditions would
apply to that model as well.
novel or unusual design feature, special
conditions are prescribed under the
provisions of § 21.16.
Special conditions are initially
applicable to the model for which they
are issued. Should the applicant apply
for a supplemental type certificate to
modify any other model included on the
same type certificate to incorporate the
same novel or unusual design feature,
these special conditions would also
apply to the other model under § 21.101.
In addition to the applicable
airworthiness regulations and special
conditions, the DeHavilland DHC–8–
400 series airplane must comply with
the exhaust-emission requirements of 14
CFR part 34, and the noise-certification
requirements of 14 CFR part 36.
The FAA issues special conditions, as
defined in 14 CFR 11.19, in accordance
with § 11.38, and they become part of
the type certification basis under
§ 21.101.
Novel or Unusual Design Features
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Conclusion
This action affects only a certain
novel or unusual design feature for the
DeHavilland Model DHC–8–400 series
airplanes, modified by Canard. It is not
a rule of general applicability and
affects only the applicant who applied
to the FAA for approval of these features
on the airplane.
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Federal Register / Vol. 90, No. 53 / Thursday, March 20, 2025 / Rules and Regulations
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting
and recordkeeping requirements.
ACTION:
Authority: 49 U.S.C. 106(f), 40113, 44701,
44702, and 44704.
The Special Conditions
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the following special
conditions are issued as part of the type
certification basis for the DeHavilland
DHC–8–400 series airplanes, as
modified by Canard.
1. The applicant must ensure that the
airplane electronic system security is
protected from access by unauthorized
sources external to the airplane,
including those possibly caused by
maintenance activity.
2. The applicant must ensure that
electronic system security threats are
identified and assessed, and that
effective electronic system security
protection strategies are implemented to
protect the airplane from all adverse
impacts on safety, functionality, and
continued airworthiness.
3. The applicant must establish
appropriate procedures to allow the
operator to ensure that continued
airworthiness of the aircraft is
maintained, including all post type
certification modifications that may
have an impact on the approved
electronic system security safeguards.
Issued in Kansas City, Missouri, on March
14, 2025.
Patrick R. Mullen,
Manager, Technical Policy Branch, Policy and
Standards Division, Aircraft Certification
Service.
[FR Doc. 2025–04664 Filed 3–19–25; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2023–2194; Airspace
Docket No. 23–ASO–19]
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RIN 2120–AA66
Amendment of VOR Federal Airways
V–5, V–47, V–97, V–128, V–275, and V–
517, and United States Area Navigation
(RNAV) Route T–315, and Revocation
of VOR Federal Airway V–19 in the
Vicinity of Cincinnati, KY
Federal Aviation
Administration (FAA), DOT.
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This action amends Very High
Frequency Omnidirectional Range
(VOR) Federal Airways V–5, V–47, V–
97, V–128, V–275, and V–517, and
United States (U.S.) Area Navigation
(RNAV) Route T–315; and revokes VOR
Federal Airway V–19. The FAA is
taking this action due to the planned
decommissioning of the VOR portion of
the Cincinnati, KY (CVG), VOR/Tactical
Air Navigation (VORTAC) navigational
aid (NAVAID). The Cincinnati VOR is
being decommissioned in support of the
FAA’s VOR Minimum Operational
Network (MON) program.
DATES: Effective date 0901 UTC, June
12, 2025. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA
Order JO 7400.11 and publication of
conforming amendments.
ADDRESSES: A copy of the notice of
proposed rulemaking (NPRM), all
comments received, this final rule, and
all background material may be viewed
online at www.regulations.gov using the
FAA Docket number. Electronic
retrieval help and guidelines are
available on the website. It is available
24 hours each day, 365 days each year.
FAA Order JO 7400.11J, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at www.faa.gov/air_traffic/
publications/. You may also contact the
Rules and Regulations Group, Policy
Directorate, Federal Aviation
Administration, 600 Independence
Avenue SW, Washington, DC 20597;
telephone: (202) 267–8783.
FOR FURTHER INFORMATION CONTACT:
Colby Abbott, Rules and Regulations
Group, Policy Directorate, Federal
Aviation Administration, 600
Independence Avenue SW, Washington,
DC 20597; telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Authority Citation
The authority citation for these
special conditions is as follows:
AGENCY:
Final rule.
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of the airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
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13057
scope of that authority as it modifies the
Air Traffic Service (ATS) route structure
as necessary to preserve the safe and
efficient flow of air traffic within the
National Airspace System.
History
The FAA published an NPRM for
Docket No. FAA–2023–2194 in the
Federal Register (88 FR 77238;
November 9, 2023), proposing to amend
VOR Federal Airways V–5, V–47, V–97,
V–128, V–275, and V–517, and U.S.
RNAV Route T–315; and revoke VOR
Federal Airway V–19 due to the
planned decommissioning of the VOR
portion of the Cincinnati, KY, VORTAC
NAVAID. Interested parties were invited
to participate in this rulemaking effort
by submitting written comments on the
proposal. No comments were received.
Differences From the NPRM
Subsequent the NPRM, the FAA
published a final rule for Docket No.
FAA–2023–1737 in the Federal Register
(89 FR 42795; May 16, 2024), amending
VOR Federal Airway V–128 by
removing the airway segment between
the Cincinnati, KY (reflected as OH in
that final rule), VORTAC and the
Charleston, WV, VORTAC.
Additionally, that final rule amended
U.S. RNAV Route T–315 by extending
the route westward from the JARLO,
WV, Waypoint (WP) to the JIMUR, KY,
Fix and included the CALIF, KY, Fix
and the ILILE, OH, WP in the extension.
Those route amendments were effective
July 11, 2024, and are included in this
final rule.
Additionally, subsequent the NPRM,
the FAA published a final rule for
Docket No. FAA–2024–1848 in the
Federal Register (90 FR 9216; February
10, 2025), amending VOR Federal
Airway V–97 by removing the airway
segment between the Dolphin, FL,
VORTAC and the St. Petersburg, FL,
VORTAC. That airway amendment is
effective April 17, 2025, and is also
included in this final rule.
Finally, the NPRM addressed the VOR
Federal Airway V–97 proposed airway
amendments in the preamble, but the
‘‘as amended’’ airway information did
not match the description in the
regulatory text for the airway. The
proposed amendments to V–97 removed
the airway segment between the
Lexington, KY, VOR/Distance
Measuring Equipment (VOR/DME) and
the intersection of the Chicago Heights,
IL, VORTAC 358° and DuPage, IL, VOR/
DME 101° radials (NILES Fix). As
amended, the correct V–97 airway
description in the NPRM should have
reflected the airway would extend
between the Dolphin VORTAC and the
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]]>Agencies
[Federal Register Volume 90, Number 53 (Thursday, March 20, 2025)]
[Rules and Regulations]
[Pages 13055-13057]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-04664]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2025-0078; Special Conditions No. 25-876-SC]
Special Conditions: Canard Aerospace Corporation, DeHavilland
Model DHC-8-400 Series Airplane; Electronic System Security Protection
From Unauthorized External Access
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for a supplemental type
certificate (STC) to install a digital systems architecture on the
DeHavilland Model DHC-8-400 series airplane. This airplane, as modified
by the Canard Aerospace Corporation (Canard), will have a novel or
unusual design feature when compared to the state of technology
envisioned in the airworthiness standards for transport-category
airplanes. This design feature is the installation of a digital systems
architecture that will allow increased connectivity to and access from
external network sources (e.g., operator networks, wireless devices,
internet connectivity, service provider satellite communications,
electronic flight bags, etc.) to the airplane's previously isolated
electronic assets (networks, systems, and databases). The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These special conditions contain the
additional safety standards that the Administrator considers necessary
to establish a level of safety equivalent to that established by the
existing airworthiness standards.
DATES: This action is effective on Canard on March 20, 2025. Send
comments on or before May 5, 2025.
ADDRESSES: Send comments identified by Docket No. FAA-2025-0078 using
any of the following methods:
Federal eRegulations Portal: Go to www.regulations.gov and
follow the online instructions for sending your comments
electronically.
Mail: Send comments to Docket Operations, M-30, U.S.
Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room
W12-140, West Building Ground Floor, Washington, DC 20590-0001.
Hand Delivery or Courier: Take comments to Docket
Operations in Room W12-140 of the West Building Ground Floor at 1200
New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Fax: Fax comments to Docket Operations at 202-493-2251.
Docket: Background documents or comments received may be read at
www.regulations.gov at any time. Follow the online instructions for
accessing the docket or go to Docket Operations in Room W12-140 of the
West Building Ground Floor at 1200 New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays.
FOR FURTHER INFORMATION CONTACT: Thuan T. Nguyen, Avionics Software and
Components Unit, AIR-626D, Technical Policy Branch, Aircraft
Certification Service, Federal Aviation Administration, 2200 South
216th Street, Des Moines, Washington 98198; telephone (206) 231-3365;
email: [email protected].
SUPPLEMENTARY INFORMATION: The substance of these special conditions
has been published in the Federal Register for public comment in
several prior instances with no substantive comments received.
Therefore, the FAA finds, pursuant to 14 CFR 11.38(b), that new
comments are unlikely, and notice and comment prior to this publication
are unnecessary.
Privacy
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in title
14, Code of Federal Regulations (14 CFR) 11.35, the FAA will post all
comments received without change to www.regulations.gov, including any
personal information you provide. The FAA will also post a report
summarizing each substantive verbal contact received about these
special conditions.
Confidential Business Information
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
these special conditions contain commercial or financial information
that is customarily treated as private, that you actually treat as
private, and that is relevant or responsive to these special
conditions, 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
[[Page 13056]]
will treat such marked submissions as confidential under the FOIA, and
the indicated comments will not be placed in the public docket of these
special conditions. Send submissions containing CBI to the individual
listed in the For Further Information Contact section above. Comments
the FAA receives, which are not specifically designated as CBI, will be
placed in the public docket for these special conditions.
Comments Invited
The FAA invites interested people to take part in this rulemaking
by sending written comments, data, or views. The most helpful comments
reference a specific portion of the special conditions, explain the
reason for any recommended change, and include supporting data.
The FAA will consider all comments received by the closing date for
comments. The FAA may change these special conditions based on the
comments received.
Background
On April 15, 2024, Canard applied for a supplemental type
certificate to install a digital systems architecture on the
DeHavilland Model DHC-8-400 series airplane that will allow increased
connectivity to and access from external network sources (e.g.,
operator networks, wireless devices, internet connectivity, service
provider satellite communications, electronic flight bags, etc.) to the
airplane's previously isolated electronic assets (networks, systems,
and databases). The DeHavilland Model DHC-8-400 series airplane is a
twin-engine airplane with a passenger capacity of 68 and a maximum
takeoff weight of 61,700 pounds.
Type Certification Basis
Under the provisions of title 14, Code of Federal Regulations (14
CFR) 21.101, Canard must show that the Model DeHavilland DHC-8-400
series airplane, as changed, continues to meet the applicable
provisions of the regulations listed in Type Certificate No. A13NM or
the applicable regulations in effect on the date of application for the
change, except for earlier amendments as agreed upon by the FAA.
If the Administrator finds that the applicable airworthiness
regulations (e.g., 14 CFR part 25) do not contain adequate or
appropriate safety standards for the listed airplanes because of a
novel or unusual design feature, special conditions are prescribed
under the provisions of Sec. 21.16.
Special conditions are initially applicable to the model for which
they are issued. Should the applicant apply for a supplemental type
certificate to modify any other model included on the same type
certificate to incorporate the same novel or unusual design feature,
these special conditions would also apply to the other model under
Sec. 21.101.
In addition to the applicable airworthiness regulations and special
conditions, the DeHavilland DHC-8-400 series airplane must comply with
the exhaust-emission requirements of 14 CFR part 34, and the noise-
certification requirements of 14 CFR part 36.
The FAA issues special conditions, as defined in 14 CFR 11.19, in
accordance with Sec. 11.38, and they become part of the type
certification basis under Sec. 21.101.
Novel or Unusual Design Features
The Model DeHavilland DHC-8-400 series airplane, as modified by
Canard, will incorporate the following novel or unusual design
feature(s):
The installation of a digital systems architecture that will allow
increased connectivity to and access from external network sources,
(e.g., operator networks, wireless devices, internet connectivity,
service provider satellite communications, electronic flight bags,
etc.) to the airplane's previously isolated electronic assets
(networks, systems, and databases).
Discussion
The DeHavilland Model DHC-8-400 series airplanes electronic system
architecture and network configuration change is novel or unusual for
commercial transport airplanes because it may allow increased
connectivity to and access from external network sources, airline
operations, and maintenance networks, to the airplane control domain,
and airline information services domain. The airplane's control domain
and airline information-services domain perform functions required for
the safe operation and maintenance of the airplane. Previously, these
domains had very limited connectivity with external network sources.
This data network and design integration creates a potential for
unauthorized persons to access the airplane's control domain and
airline information-services domain and presents security
vulnerabilities related to the introduction of computer viruses and
worms, user errors, and intentional sabotage of airplane electronic
assets (networks, systems, and databases) critical to the safety and
maintenance of the airplane.
The existing FAA regulations did not anticipate these networked
airplane-system architectures. Furthermore, these regulations and the
current guidance material do not address potential security
vulnerabilities, which could be exploited by unauthorized access to
airplane networks, data buses, and servers. Therefore, these special
conditions ensure that the security (i.e., confidentiality, integrity,
and availability) of the airplane's systems is not compromised by
unauthorized wired or wireless electronic connections. This includes
ensuring that the security of the airplane's systems is not compromised
during maintenance of the airplane's electronic systems. These special
conditions also require the applicant to provide appropriate
instructions to the operator to maintain all electronic-system
safeguards that have been implemented as part of the original network
design so that this feature does not allow or introduce security
threats.
These special conditions contain the additional safety standards
that the Administrator considers necessary to establish a level of
safety equivalent to that established by the existing airworthiness
standards.
Applicability
As discussed above, these special conditions are applicable to the
DeHavilland DHC-8-400 series airplane, as modified by Canard. Should
Canard apply at a later date for a supplemental type certificate to
modify any other model included on Type Certificate No. A13NM to
incorporate the same novel or unusual design feature, these special
conditions would apply to that model as well.
Conclusion
This action affects only a certain novel or unusual design feature
for the DeHavilland Model DHC-8-400 series airplanes, modified by
Canard. It is not a rule of general applicability and affects only the
applicant who applied to the FAA for approval of these features on the
airplane.
[[Page 13057]]
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
Authority Citation
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(f), 40113, 44701, 44702, and 44704.
The Special Conditions
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special conditions are issued as part of
the type certification basis for the DeHavilland DHC-8-400 series
airplanes, as modified by Canard.
1. The applicant must ensure that the airplane electronic system
security is protected from access by unauthorized sources external to
the airplane, including those possibly caused by maintenance activity.
2. The applicant must ensure that electronic system security
threats are identified and assessed, and that effective electronic
system security protection strategies are implemented to protect the
airplane from all adverse impacts on safety, functionality, and
continued airworthiness.
3. The applicant must establish appropriate procedures to allow the
operator to ensure that continued airworthiness of the aircraft is
maintained, including all post type certification modifications that
may have an impact on the approved electronic system security
safeguards.
Issued in Kansas City, Missouri, on March 14, 2025.
Patrick R. Mullen,
Manager, Technical Policy Branch, Policy and Standards Division,
Aircraft Certification Service.
[FR Doc. 2025-04664 Filed 3-19-25; 8:45 am]
BILLING CODE 4910-13-P
