[Federal Register Volume 90, Number 130 (Thursday, July 10, 2025)]
[Rules and Regulations]
[Pages 30575-30577]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-12875]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-1119; Project Identifier MCAI-2025-00914-G;
Amendment 39-23074; AD 2025-13-08]
RIN 2120-AA64
Airworthiness Directives; DG Aviation GmbH (Type Certificate
Previously Held by DG Flugzeugbau GmbH) Gliders
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
DG Aviation GmbH (type certificate previously held by DG Flugzeugbau
GmbH) Model DG-1000T gliders. This AD was prompted by reports of
propeller separation. This AD requires revising the glider flight
manual and installing ``Motor INOP'' placards to prohibit operation
with the powerplant. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective July 25, 2025.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 25,
2025.
The FAA must receive comments on this AD by August 25, 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-2025-1119; 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 DG Aviation GmbH material identified in this AD,
contact DG Aviation GmbH, Rita Rodrigues, Otto Lilienthal Weg 2/Am
Flugplatz, Bruchsal, Germany; phone: +49 (0) 7251 36660-32; email:
[email protected]; website: https://www.dg-aviation.de/en/dg-flugzeugbau/contact.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 901 Locust, Kansas City,
MO 64106. 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-2025-1119.
FOR FURTHER INFORMATION CONTACT: Dan McCully, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (404)
474-5548; 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 using a method listed under
the ADDRESSES section. Include ``Docket No. FAA-2025-1119; Project
Identifier MCAI-2025-00914-G'' 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
[[Page 30576]]
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 Dan McCully, 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
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2025-0112-E, dated May 14, 2025 (referred to as ``the MCAI''),
to correct an unsafe condition on all DG Aviation GmbH Model DG-1000T
powered sailplanes (gliders).
The MCAI states two occurrences were reported of propeller
separation from DG Aviation GmbH Model DG-1000T gliders. In both
reports, the rubber of the damper element sheared off completely. The
investigation to determine the root cause is ongoing. This condition,
if not detected and corrected, could lead to separation of the
propeller, which could result in reduced or loss of control of the
glider or the propeller impacting the glider, passengers in the glider,
or people on the ground.
The MCAI prohibits use of the glider's powerplant and requires
revising the glider flight manual and installing ``Motor INOP''
placards. The MCAI also provides removal of the powerplant as an
acceptable alternative method of compliance.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2025-1119.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed DG aviation GmbH Service Information No. 116-25,
Issue 01.b, dated May 12, 2025. This material specifies procedures for
revising the DG Aviation GmbH Model DG-1000T glider flight manual,
emptying the fuel tank, and installing ``Motor INOP'' placards. 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 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.
AD Requirements
This AD requires accomplishing the actions specified in the
material already described, except as discussed under ``Differences
Between this AD and the Referenced Material.''
The owner/operator (pilot) holding at least a private pilot
certificate may revise the existing glider flight manual and must enter
compliance with the applicable paragraph of this AD into the glider
maintenance records in accordance with 14 CFR 43.9(a) and
91.417(a)(2)(v). The pilot may perform this action because it only
involves revising the flight manual. This action could be performed
equally well by a pilot or a mechanic. This is an exception to the
FAA's standard maintenance regulations.
Differences Between This AD and the Referenced Material
The service information specifies compliance before the next engine
use, but this AD requires compliance within 3 days after the effective
date of this AD.
Although the service information specifies emptying the fuel tank,
this AD does not require this action because this action is not
required to address the unsafe condition identified in this AD.
Interim Action
The FAA considers that this AD is an interim action. If final
action is later identified, the FAA might consider further rulemaking.
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 the 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 the propeller separating from the glider could damage the
aircraft structure and result in reduced control of the glider.
Additionally, the corrective actions to prohibit operating the glider
using the powerplant must be accomplished within 3 days after the
effective date of this AD. Accordingly, notice and opportunity for
prior public comment are impracticable 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 2 gliders of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Revise glider flight manual............... 1 work-hour x $85 per hour = $0 $85 $170
$85.
Fabricate and install placards............ 1 work-hour x $85 per hour = 35 120 240
$85.
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[[Page 30577]]
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:
2025-13-08 DG Aviation GmbH (Type Certificate Previously Held by DG
Flugzeugbau GmbH): Amendment 39-23074; Docket No. FAA-2025-1119;
Project Identifier MCAI-2025-00914-G.
(a) Effective Date
This airworthiness directive (AD) is effective July 25, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to DG Aviation GmbH (type certificate previously
held by DG Flugzeugbau GmbH) Model DG-1000T gliders, certificated in
any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 7100, Powerplant
System.
(e) Unsafe Condition
This AD was prompted by reports of propeller separation. The FAA
is issuing this AD to detect and address failure of a propeller. The
unsafe condition, if not addressed, could lead to separation of the
propeller, which could result in reduced or loss of control of the
glider or the propeller impacting the glider, passengers in the
glider, or people on the ground.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 3 days after the effective date of this AD, comply with
either paragraph (g)(1) or (2) of this AD.
(1) Revise the flight manual for your glider and install ``Motor
INOP'' placards in accordance with paragraphs 1 and 3 of the
Instructions in DG aviation GmbH Service Information No. 116-25,
Issue 01.b, dated May 12, 2025. The owner/operator (pilot) holding
at least a private pilot certificate may revise the existing flight
manual and must enter compliance with the applicable paragraph of
this AD into the glider maintenance records in accordance with 14
CFR 43.9(a) and 91.417(a)(2)(v). The record must be maintained as
required by 14 CFR 91.417, 121.380, or 135.439.
(2) Remove the powerplant from the glider.
(h) Credit for Previous Actions
This paragraph provides credit for the actions required by
paragraph (g)(1) of this AD, if those actions were performed before
the effective date of this AD using DG aviation GmbH Service
Information No. 116-25, Doc No. SI 116-25 FE-30-01, Issue 01.a,
dated May 5, 2025.
(i) Special Flight Permits
Special flight permits are prohibited.
(j) 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 (k) 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.
(k) Additional Information
For more information about this AD, contact Dan McCully,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (404) 474-5548; email:
[email protected].
(l) 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) DG aviation GmbH Service Information No. 116-25, Issue 01.b,
dated May 12, 2025.
(ii) [Reserved]
(3) For DG Aviation GmbH material identified in this AD, contact
DG Aviation GmbH, Rita Rodrigues, Otto Lilienthal Weg 2/Am
Flugplatz, Bruchsal, Germany; phone: +49 (0) 7251 36660-32; email:
[email protected]; website: https://www.dg-aviation.de/en/dg-flugzeugbau/contact.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 901 Locust, Kansas
City, MO 64106. 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 June 27, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-12875 Filed 7-8-25; 4:15 pm]
BILLING CODE 4910-13-P