Airworthiness Directives; Diamond Aircraft Industries Inc. Airplanes
Requires a continuity inspection of the D-sub connector of the Artex ELT 1000 and, if necessary, corrective actions.
[Federal Register Volume 91, Number 148 (Tuesday, August 4, 2026)]
[Rules and Regulations]
[Pages 49269-49271]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2026-15825]
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Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
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Federal Register / Vol. 91, No. 148 / Tuesday, August 4, 2026 / Rules
and Regulations
[[Page 49269]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2026-4636; Project Identifier MCAI-2026-00070-A;
Amendment 39-23430; AD 2026-15-18]
RIN 2120-AA64
Airworthiness Directives; Diamond Aircraft Industries Inc.
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Diamond Aircraft Industries Inc. (DAI) Model DA20-C1 airplanes.
This AD was prompted by a report of a certain emergency locator
transmitter (ELT) not activating due to a missing jumper wire. This AD
requires a continuity inspection of the D-sub connector of the Artex
ELT 1000 and, if necessary, corrective actions. The FAA is issuing this
AD to address the unsafe condition on these products.
DATES: This AD is effective September 8, 2026.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September 8,
2026.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2026-4636; 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-91, West Building Fifth Floor, Room W58-213, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For Diamond Aircraft Industries material identified in
this AD, contact DAI, 1560 Crumlin Sideroad, London, Ontario, Canada,
N5V 1S2; phone: (519) 457-4041, fax: (519) 457-4045; email: diamondaircraft.com">support-canada@diamondaircraft.com; website: diamondaircraft.com.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 1100 Main, Kansas City, MO
64105. For information on the availability of this material at the FAA,
call (817) 222-5110. It is also available at regulations.gov under
Docket No. FAA-2026-4636.
FOR FURTHER INFORMATION CONTACT: William Reisenauer, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (516) 228-7301; 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 DAI Model DA20-
C1 airplanes. The NPRM was published in the Federal Register on May 15,
2026 (91 FR 27871). The NPRM was prompted by Transport Canada AD CF-
2026-03, dated January 21, 2026 AD CF-2026-03) (referred to as the
MCAI), issued by Transport Canada, which is the aviation authority for
Canada to correct an unsafe condition on all DAI Model DA20-C1
airplanes having an Artex ELT 1000 installed. The MCAI states that DAI
received a report of an occurrence where the Artex ELT 1000 installed
in a DA20-C1 airplane did not perform as intended. Further
investigation by the manufacturer revealed that some Artex ELT 1000
units might not have a jumper wire between the D-sub pins 5 and 12,
which could prevent the ELT beacon from being activated by the internal
G-Switch and the aural alert buzzer from being activated in the event
of an accident.
In the NPRM, the FAA proposed to require a continuity inspection of
the D-sub connector of the Artex ELT 1000 and, if necessary, corrective
actions. 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-2026-4636.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
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 reviewed the relevant
data, considered any 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, this AD is adopted as proposed in the NPRM.
None of the changes will increase the economic burden on any operator.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed Diamond Aircraft Industries Mandatory Service
Bulletin No. DAC1-25-05 Rev. 1, dated July 19, 2024. This material
specifies procedures for performing a continuity inspection on the D-
sub connector of the Artex ELT 1000 and, if necessary, installing the
jumper wire into the D-sub connector.
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.
Differences Between This AD and the Referenced Material
Although step 14 of the Accomplishment/Instructions of Diamond
Aircraft Industries Mandatory Service Bulletin DAC1-25-05 Rev. 1, dated
July 19, 2024, requires completing and sending an execution report to
the manufacturer, this AD does not require that action.
Costs of Compliance
The FAA estimates that this AD affects 365 airplanes of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
[[Page 49270]]
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Continuity inspection and corrective 1 work-hour x $85 per hour $0 $85 $31,025
actions. = $85.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any repairs that would
be required based on the results of the inspection. The agency has no
way of determining the number of airplanes that might need these
repairs:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Action Labor cost Parts cost Cost per product
----------------------------------------------------------------------------------------------------------------
Install jumper wire.......................... 1 work-hour x $85 per hour = $85 $3 $88
----------------------------------------------------------------------------------------------------------------
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:
2026-15-18 Diamond Aircraft Industries Inc.: Amendment 39-23430;
Docket No. FAA-2026-4636; Project Identifier MCAI-2026-00070-A.
(a) Effective Date
This airworthiness directive (AD) is effective September 8,
2026.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Diamond Aircraft Industries Inc. Model
DA20-C1 airplanes, certificated in any category, that have an Artex
emergency locator transmitter (ELT) 1000 installed.
(d) Subject
Joint Aircraft System Component (JASC) Code 2562, Emergency
Locator Beacon.
(e) Unsafe Condition
This AD was prompted by a report of a certain ELT not activating
due to a missing jumper wire. The FAA is issuing this AD to detect
and address a missing jumper wire on the Artex ELT 1000. The unsafe
condition, if not addressed, could result in the ELT beacon and
aural alert buzzer not activating in the event of an accident.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 3 months after the effective date of this AD, perform a
continuity inspection of the D-sub connector and accomplish all
required corrective actions in accordance with the Accomplishment/
Instructions, Paragraph I.9, of Diamond Aircraft Industries
Mandatory Service Bulletin No. DAC1-25-05 Rev. 1, dated July 19,
2024.
(h) No Reporting Requirement
Although step 14 of the Accomplishment/Instructions of Diamond
Aircraft Industries Mandatory Service Bulletin No. DAC1-25-05 Rev.
1, dated July 19, 2024, requires completing and sending an execution
report to the manufacturer, this AD does not include that
requirement.
(i) 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 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 (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 local flight standards district
office/certificate holding district office.
(j) Additional Information
For more information about this AD, contact William Reisenauer,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (516) 228-7301; email: [email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 the AD specifies otherwise.
(i) Diamond Aircraft Industries Mandatory Service Bulletin No.
DAC1-25-05 Rev. 1, dated July 19, 2024.
[[Page 49271]]
(ii) [Reserved]
(3) For Diamond Aircraft Industries material identified in this
AD, contact Diamond Aircraft Industries Inc., 1560 Crumlin Sideroad,
London, Ontario, Canada, N5V 1S2; phone: (519) 457-4041, fax: (519)
457-4045; email: diamondaircraft.com">support-canada@diamondaircraft.com; website:
diamondaircraft.com.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 1100 Main, Kansas City,
MO 64105. For information on the availability of this material at
the FAA, call (817) 222-5110.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on July 27, 2026.
Paul R. Bernado,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2026-15825 Filed 8-3-26; 8:45 am]
BILLING CODE 4910-13-P
Sources. Section 1 is written by AircraftDirectives from the record below and is a reading aid only. Section 2 is the United States Government's own text, reproduced without edit.
Federal Register: https://www.federalregister.gov/documents/2026/08/04/2026-15825/airworthiness-directives-diamond-aircraft-industries-inc-airplanes
Official PDF: https://www.govinfo.gov/content/pkg/FR-2026-08-04/pdf/2026-15825.pdf
FAA DRS record: https://drs.faa.gov/browse/excelExternalWindow/FR-ADFRAWD-2026-15825-0000000000.0001
Packet generated 2026-08-18 08:50 UTC.
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Section 1 is a reading aid, not the rule. It is our own plain-language condensation, written to help a reader find the relevant directive quickly. It is NOT a substitute for the regulation, it may omit conditions, exceptions, compliance times, alternative methods of compliance (AMOCs) and applicability limits, and it has no legal force whatsoever. Only the official text governs. Where Section 1 and Section 2 differ in any respect, Section 2 - and the official source it was retrieved from - controls absolutely.
Responsibility remains with the owner/operator. Under 14 CFR §91.403 and §91.417 the owner or operator is responsible for maintaining airworthiness and for required records; under §39.7 no person may operate a product to which an airworthiness directive applies except in accordance with that directive. Determining applicability to a specific serial number and configuration, and performing or supervising any required action, is the responsibility of the owner/operator and appropriately certificated personnel.
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