Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously Held by DG Flugzeugbau GmbH) Gliders, 79425-79428 [2024-22321]
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Federal Register / Vol. 89, No. 189 / Monday, September 30, 2024 / Rules and Regulations
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, International Validation
Branch, FAA; or the UK CAA; or BAE
Systems (Operations) Limited’s UK CAA’s
DOA. If approved by the DOA, the approval
must include the DOA-authorized signature.
(j) Additional Information
For more information about this AD,
contact Todd Thompson, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 206–
231–3228; email todd.thompson@faa.gov.
(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.
(i) BAE Systems (Operations) Limited
Inspection Service Bulletin ISB.53–249,
dated August 25, 2023.
(ii) [Reserved]
(3) For BAE Systems material identified in
this AD, contact BAE Systems (Operations)
Limited, Customer Information Department,
Prestwick International Airport, Ayrshire,
KA9 2RW, Scotland, United Kingdom;
telephone +44 1292 675207; fax +44 1292
675704; email RApublications@
baesystems.com; website baesystems.com/
en/our-company/our-businesses/regionalaircraft/about-us.
(4) 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.
(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 fr.inspection@nara.gov.
Issued on August 22, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–22319 Filed 9–27–24; 8:45 am]
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BILLING CODE 4910–13–P
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–2316; Project
Identifier MCAI–2024–00381–G; Amendment
39–22854; AD 2024–19–12]
RIN 2120–AA64
Airworthiness Directives; DG Aviation
GmbH (Type Certificate Previously
Held by DG Flugzeugbau GmbH)
Gliders
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
DG Aviation GmbH (type certificate
previously held by DG Flugzeugbau
GmbH) Model DG–400 gliders and all
Model DG–500 Elan Orion, DG–500
Elan Trainer, DG–500/20 Elan, DG–500/
22 Elan, DG–500M, DG–500MB, DG–
800A, DG–800B, DG–808C, DG–1000M,
DG–1000S, and DG–1000T gliders. This
AD was prompted by a report of a
broken rod end at the upper end of the
elevator pushrod in the fin (vertical tail)
of a DG Aviation GmbH Model DG–300
glider. Depending on the glider model,
this AD requires revising your existing
glider maintenance manual to
incorporate new procedures for elevator
control circuit free play adjustment,
performing an operational check of the
free play adjustment of the automatic
elevator hook-up, accomplishing
corrective actions as required, and
replacing the elevator pushrod end with
a new part. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective October 15,
2024.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of October 15, 2024.
The FAA must receive comments on
this AD by November 14, 2024.
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.
SUMMARY:
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79425
• 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–2024–2316; 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, Otto-Lilienthal Weg 2/
Am Flugplatz, 76646 Bruchsal,
Germany; phone: +49 (0) 7251 36660–
32; email: info@dg-aviation.de; website:
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–2024–2316.
Fred
Guerin, Aviation Safety Engineer, FAA,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (206) 231–
2346; email: fred.guerin@faa.gov.
FOR FURTHER INFORMATION CONTACT:
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 ADDRESSES.
Include ‘‘Docket No. FAA–2024–2316;
Project Identifier MCAI–2024–00381–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.
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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 Fred Guerin, 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.
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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
2024–0126, dated July 2, 2024 (EASA
AD 2024–0126) (also referred to as the
MCAI), to correct an unsafe condition
on the following DG Aviation GmbH
sailplanes (gliders):
• Model DG–100G, DG–100G ELAN,
DG–200, DG–200/17, DG–200/17C, DG–
300, DG–300 ELAN, DG–300 Club
ELAN, DG–300 ELAN ACRO, DG–300
Club ELAN ACRO, DG–400, DG–600,
DG–600/18, DG–600M, and DG–600/18
M sailplanes and powered sailplanes,
all serial numbers except those
equipped with l’Hotellier connections of
the elevator control.
• Model DG–500/22 ELAN, DG–500
ELAN Trainer, DG–500/20 ELAN, DG–
500 ELAN ORION, DG–500 M, and DG–
500 MB sailplanes and powered
sailplanes, all serial numbers.
• Model DG–800 A, DG–800 B, DG–
808C, DG–800 LA, DG–800 S, and DG–
808 S sailplanes and powered sailplanes
all serial numbers.
• Model DG–1000S, DG–1000T, DG–
1000M, and DG–1000E sailplanes and
powered sailplanes, all serial numbers.
The MCAI states an occurrence was
reported of a broken rod end at the
upper end of the elevator pushrod in the
fin of a Model DG–300 sailplane. It was
determined that the elevator play
adjustment screw was screwed in too
far, which caused jamming of the roller
inside the funnel. Even with higher
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force, the roller could not be moved up
to the front of the funnel; therefore, each
time, when rigging and during normal
operation, a bending force affected the
rod end, causing fatigue failure. Further
investigation revealed that a significant
number of certain sailplane models
were operated with the elevator play
adjustment screw screwed in too far. It
was also determined that because of its
location, the elevator pushrod end
damage could not be detected using
visual or non-destructive testing to
identify fatigue cracks. This condition,
if not detected and corrected, could lead
to loss of pitch control of the (powered)
sailplane. Due to the similarity of
design, all DG sailplanes in the
applicability of the MCAI (if equipped
with automatic hook-up) could be
affected by the unsafe condition.
The MCAI requires a one-time
operational check of the free play
adjustment of the automatic elevator
hook-up and, depending on the
findings, replacement of the affected
parts, and for a certain group of
(powered) sailplanes, mandatory
replacement of the rod end. The MCAI
also requires following revised
applicable Maintenance Manual tasks.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2024–2316.
FAA’s Determination
These products have been approved
by the 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, it 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.
Material Incorporated by Reference
Under 1 CFR Part 51
The FAA reviewed the following
material that specifies revising your
existing glider maintenance manual and
specifies procedures for accomplishing
an operational check of the free play of
the automatic elevator hook-up and
installing new elevator pushrod ends
and new elevator rollers and adjusting
the free play, as applicable. These
documents are distinct since they apply
to different glider models.
• DG Aviation GmbH Technical Note
No. DG–SS–09, Doc. No. TMDG–SS–09
FE–29–01, Issue 01.f, dated March 5,
2024, for Model DG–400 gliders.
• DG Aviation GmbH Technical Note
No. 500/17, Doc. No. TM500–17 FE–29–
01, Issue 01.c, dated March 5, 2023, for
Model DG–500 gliders.
• DG Aviation GmbH Technical Note
No. 800/50, Doc. No. TM800–50 FE–29–
01, Issue 01.c, dated March 5, 2024, for
Model DG–800 gliders.
• DG Aviation GmbH Technical Note
No. 1000/50, Doc. No. TM1000–50 FE–
29–01, Issue 01.c, dated March 4, 2024,
for Model DG–1000 gliders.
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.
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 operating a glider with the
elevator play adjustment screw screwed
in too far could lead to a loss of pitch
control of the glider and loss of the
ability to control the glider in flight or
during landing. The FAA has
determined that certain gliders will
need an operational check within 3
months and immediate action if any
discrepancy is found and certain other
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AD Requirements
This AD requires accomplishing the
actions specified in the material already
described, except as discussed under
‘‘Differences Between this AD and the
MCAI.’’
Differences Between This AD and the
MCAI
The MCAI applies to Model DG–
100G, DG–100G ELAN, DG–200, DG–
200/17, DG–200/17C, DG–300, DG–300
ELAN, DG–300 Club ELAN, DG–300
ELAN ACRO, DG–300 Club ELAN
ACRO, DG–600, DG–600/18, DG–600M,
DG–600/18 M, DG–800 LA, DG–800 S,
DG–808 S, and DG–1000E gliders, but
this AD does not because these models
do not have an FAA type certificate.
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gliders will need replacement of an
affected part within 3 months after the
effective date of this AD. This
compliance time 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 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)
79427
cause to adopt this rule without prior
notice and comment, RFA analysis is
not required.
for making this amendment effective in
less than 30 days, for the same reasons
the FAA found good cause to forgo
notice and comment.
Costs of Compliance
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
The FAA estimates that this AD
affects 101 gliders of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Revise glider maintenance manual (Group 1 and
Group 2 gliders).
Perform operational check of the free play adjustment of the automatic elevator hook-up (Group 1
and Group 2 gliders).
Replace the elevator pushrod end (Group 1 gliders)
The FAA estimates the following
costs to do any necessary elevator roller
replacement (both Group 1 and Group 2
Cost per
product
Parts cost
Cost on U.S. operators
1 work-hour × $85 per
hour = $85.
1 work-hour × $85 per
hour = $85.
$0
85
8,585.
0
85
8,585.
2 work-hours × $85 per
hour = $170.
100
270
gliders) or elevator rod replacement
(Group 2 gliders) that would be required
based on the results of the operational
7,020 (26 gliders).
check. The agency has no way of
determining the number of gliders that
might need these replacements:
ON-CONDITION COSTS
Action
Labor cost
Replace the elevator roller with a new one and adjust free play (Group
1 and Group 2 gliders).
Replace the elevator pushrod end (Group 2 gliders) ................................
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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
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2 work-hours × $85 per hour =
$170.
2 work-hours × $85 per hour =
$170.
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:
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Parts cost
Sfmt 4700
Cost per
product
150
320
100
270
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2024–19–12 DG Aviation GmbH (Type
Certificate Previously Held by DG
Flugzeugbau GmbH): Amendment 39–
22854; Docket No. FAA–2024–2316;
Project Identifier MCAI–2024–00381–G.
(a) Effective Date
This airworthiness directive (AD) is
effective October 15, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the following:
(1) DG Aviation GmbH (type certificate
previously held by DG Flugzeugbau GmbH)
Model DG–400 gliders, all serial numbers,
certificated in any category, except those
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with l’Hotellier connections of the elevator
control installed; and
(2) DG Aviation GmbH (type certificate
previously held by DG Flugzeugbau GmbH)
Model DG–500 Elan Orion, DG–500 Elan
Trainer, DG–500/20 Elan, DG–500/22 Elan,
DG–500M, DG–500MB, DG–800A, DG–800B,
DG–808C, DG–1000M, DG–1000S, and DG–
1000T gliders, all serial numbers; certificated
in any category.
(d) Subject
Joint Aircraft System Component (JASC)
Code 2730, Elevator Control System.
(e) Unsafe Condition
This AD was prompted by a report of a
broken rod end at the upper end of the
elevator pushrod in the fin (vertical tail) of
a DG Aviation GmbH DG–300 glider. The
FAA is issuing this AD to detect and address
the unsafe condition. The unsafe condition,
if not addressed, could result in loss of pitch
control of the glider.
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(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Definitions
For the purposes of this AD the definitions
in paragraphs (g)(1) through (5) of this AD
apply.
(1) The ‘‘applicable technical note for your
glider’’ is:
(i) Model DG–400 gliders: DG Aviation
GmbH Technical Note No. DG–SS–09, Doc.
No. TMDG–SS–09 FE–29–01, Issue 01.f,
dated March 5, 2024.
(ii) Model DG–500 gliders: DG Aviation
GmbH Technical Note No. 500/17, Doc. No.
TM500–17 FE–29–01, Issue 01.c, dated
March 5, 2023.
(iii) Model DG–800 gliders: DG Aviation
GmbH Technical Note No. 800/50, Doc. No.
TM800–50 FE–29–01, Issue 01.c, dated
March 5, 2024.
(iv) Model DG–1000 gliders: DG Aviation
GmbH Technical Note No. 1000/50, Doc. No.
TM1000–50 FE–29–01, Issue 01.c, dated
March 4, 2024.
(2) A ‘‘new elevator pushrod end’’ is an
elevator pushrod with zero hours time-inservice (TIS) having a part number specified
in the applicable technical note for your
glider that has never been installed on any
glider.
(3) A ‘‘new elevator roller’’ is an elevator
roller with zero hours TIS having a part
number specified in the applicable technical
note for your glider that has never been
installed on any glider.
(4) Group 1 gliders: Model DG–400 gliders.
(5) Group 2 gliders: Model DG–500 Elan
Orion, DG–500 Elan Trainer, DG–500/20
Elan, DG–500/22 Elan, DG–500M, DG–
500MB, DG–800A, DG–800B, DG–808C, DG–
1000M, DG–1000S, and DG–1000T gliders.
(h) Required Actions
(1) Group 1 and Group 2 gliders: Within 3
months after the effective date of this AD,
revise your existing glider maintenance
manual in accordance with paragraph 1 of
the Instructions in the applicable technical
note for your glider.
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(2) Group 1 and Group 2 gliders: Within 3
months after the effective date of this AD,
accomplish an operational check of the free
play adjustment of the automatic elevator
hook-up in accordance with paragraph 2 of
the Instructions in the applicable technical
note for your glider.
(i) Group 1 gliders: If, during the
operational check required by paragraph
(h)(2) of this AD, any discrepancy as
described in paragraph 2 of the Instructions
in the applicable technical note for your
glider is detected, before further flight,
replace the elevator roller with a new
elevator roller and adjust free play in
accordance with paragraph 2 of the
Instructions in the applicable technical note
for your glider. Where the technical note for
your glider specifies to ‘‘mark the removed
rod end as [an] unserviceable part’’ this AD
requires ‘‘removing that elevator pushrod end
from service.’’ Where the technical note for
your glider specifies ‘‘If a new rod end is
needed, order it immediately at DG’’ this AD
only requires ‘‘replacing the elevator pushrod
end with a new elevator pushrod end.’’
(ii) Group 2 gliders: If, during the
operational check required by paragraph
(h)(2) of this AD, any discrepancy, as
described in paragraph 2 of the Instructions
of the applicable technical note for your
glider is detected, before further flight,
replace either the elevator pushrod end or
elevator roller or both, as applicable, with a
new elevator pushrod end and new elevator
roller and adjust the free play in accordance
with paragraph 2 of the Instructions in the
applicable technical note for your glider.
Where the technical note for your glider
specifies to ‘‘mark the removed rod end as
[an] unserviceable part’’ this AD requires
‘‘removing that elevator pushrod end from
service.’’ Where the technical note for your
glider specifies ‘‘If a new rod end is needed,
order it immediately at DG’’ this AD only
requires ‘‘replacing the elevator pushrod end
with a new elevator pushrod end.’’
(3) Group 1 gliders: Within 3 months after
the effective date of this AD, replace the
elevator pushrod end with a new elevator
pushrod end in accordance with paragraph 2
of the Instructions in the applicable technical
note for your glider.
(i) Reporting Not Required
Although the Remarks section of the
material specified in paragraph (g)(1) of this
AD states to report ‘‘any damaged parts, false
adjustment of the elevator control, or false
installation of parts’’ and ‘‘If you find that
airworthiness may be affected this has to be
reported to the competent authority,’’ this AD
does not require those actions.
(j) Special Flight Permit
Special flight permits are prohibited.
(k) 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
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to the manager of the International Validation
Branch, send it to the attention of the person
identified in paragraph (l) of this AD and
email to: AMOC@faa.gov. 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.
(l) Additional Information
For more information about this AD,
contact Fred Guerin, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; phone: (206) 231–
2346; email: fred.guerin@faa.gov.
(m) 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 the AD specifies otherwise.
(i) DG Aviation GmbH Technical Note No.
DG–SS–09, Doc. No. TMDG–SS–09 FE–29–
01, Issue 01.f, dated March 5, 2024.
(ii) DG Aviation GmbH Technical Note No.
500/17, Doc. No. TM500–17 FE–29–01, Issue
01.c, dated March 5, 2023.
(iii) DG Aviation GmbH Technical Note
No. 800/50, Doc. No. TM800–50 FE–29–01,
Issue 01.c, dated March 5, 2024.
(iv) DG Aviation GmbH Technical Note No.
1000/50, Doc. No. TM1000–50 FE–29–01,
Issue 01.c, dated March 4, 2024.
(3) For DG Aviation GmbH material
identified in this AD, contact DG Aviation
GmbH, Otto-Lilienthal Weg 2/Am Flugplatz,
76646 Bruchsal, Germany; phone: +49 (0)
7251 36660–32; email: info@dg-aviation.de;
website: 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 fr.inspection@nara.gov.
Issued on September 19, 2024.
Steven W. Thompson,
Acting Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2024–22321 Filed 9–25–24; 4:15 pm]
BILLING CODE 4910–13–P
E:\FR\FM\30SER1.SGM
30SER1
Agencies
[Federal Register Volume 89, Number 189 (Monday, September 30, 2024)]
[Rules and Regulations]
[Pages 79425-79428]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-22321]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2316; Project Identifier MCAI-2024-00381-G;
Amendment 39-22854; AD 2024-19-12]
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.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain DG Aviation GmbH (type certificate previously held by DG
Flugzeugbau GmbH) Model DG-400 gliders and all Model DG-500 Elan Orion,
DG-500 Elan Trainer, DG-500/20 Elan, DG-500/22 Elan, DG-500M, DG-500MB,
DG-800A, DG-800B, DG-808C, DG-1000M, DG-1000S, and DG-1000T gliders.
This AD was prompted by a report of a broken rod end at the upper end
of the elevator pushrod in the fin (vertical tail) of a DG Aviation
GmbH Model DG-300 glider. Depending on the glider model, this AD
requires revising your existing glider maintenance manual to
incorporate new procedures for elevator control circuit free play
adjustment, performing an operational check of the free play adjustment
of the automatic elevator hook-up, accomplishing corrective actions as
required, and replacing the elevator pushrod end with a new part. The
FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective October 15, 2024.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of October 15,
2024.
The FAA must receive comments on this AD by November 14, 2024.
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-2024-2316; 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, Otto-Lilienthal Weg 2/Am Flugplatz, 76646
Bruchsal, Germany; phone: +49 (0) 7251 36660-32; email: [email protected]; website: 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-2024-2316.
FOR FURTHER INFORMATION CONTACT: Fred Guerin, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (206)
231-2346; 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
ADDRESSES. Include ``Docket No. FAA-2024-2316; Project Identifier MCAI-
2024-00381-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.
[[Page 79426]]
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 Fred
Guerin, 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 2024-0126, dated July 2, 2024 (EASA AD 2024-0126) (also
referred to as the MCAI), to correct an unsafe condition on the
following DG Aviation GmbH sailplanes (gliders):
Model DG-100G, DG-100G ELAN, DG-200, DG-200/17, DG-200/
17C, DG-300, DG-300 ELAN, DG-300 Club ELAN, DG-300 ELAN ACRO, DG-300
Club ELAN ACRO, DG-400, DG-600, DG-600/18, DG-600M, and DG-600/18 M
sailplanes and powered sailplanes, all serial numbers except those
equipped with l'Hotellier connections of the elevator control.
Model DG-500/22 ELAN, DG-500 ELAN Trainer, DG-500/20 ELAN,
DG-500 ELAN ORION, DG-500 M, and DG-500 MB sailplanes and powered
sailplanes, all serial numbers.
Model DG-800 A, DG-800 B, DG-808C, DG-800 LA, DG-800 S,
and DG-808 S sailplanes and powered sailplanes all serial numbers.
Model DG-1000S, DG-1000T, DG-1000M, and DG-1000E
sailplanes and powered sailplanes, all serial numbers.
The MCAI states an occurrence was reported of a broken rod end at
the upper end of the elevator pushrod in the fin of a Model DG-300
sailplane. It was determined that the elevator play adjustment screw
was screwed in too far, which caused jamming of the roller inside the
funnel. Even with higher force, the roller could not be moved up to the
front of the funnel; therefore, each time, when rigging and during
normal operation, a bending force affected the rod end, causing fatigue
failure. Further investigation revealed that a significant number of
certain sailplane models were operated with the elevator play
adjustment screw screwed in too far. It was also determined that
because of its location, the elevator pushrod end damage could not be
detected using visual or non-destructive testing to identify fatigue
cracks. This condition, if not detected and corrected, could lead to
loss of pitch control of the (powered) sailplane. Due to the similarity
of design, all DG sailplanes in the applicability of the MCAI (if
equipped with automatic hook-up) could be affected by the unsafe
condition.
The MCAI requires a one-time operational check of the free play
adjustment of the automatic elevator hook-up and, depending on the
findings, replacement of the affected parts, and for a certain group of
(powered) sailplanes, mandatory replacement of the rod end. The MCAI
also requires following revised applicable Maintenance Manual tasks.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-2316.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed the following material that specifies revising
your existing glider maintenance manual and specifies procedures for
accomplishing an operational check of the free play of the automatic
elevator hook-up and installing new elevator pushrod ends and new
elevator rollers and adjusting the free play, as applicable. These
documents are distinct since they apply to different glider models.
DG Aviation GmbH Technical Note No. DG-SS-09, Doc. No.
TMDG-SS-09 FE-29-01, Issue 01.f, dated March 5, 2024, for Model DG-400
gliders.
DG Aviation GmbH Technical Note No. 500/17, Doc. No.
TM500-17 FE-29-01, Issue 01.c, dated March 5, 2023, for Model DG-500
gliders.
DG Aviation GmbH Technical Note No. 800/50, Doc. No.
TM800-50 FE-29-01, Issue 01.c, dated March 5, 2024, for Model DG-800
gliders.
DG Aviation GmbH Technical Note No. 1000/50, Doc. No.
TM1000-50 FE-29-01, Issue 01.c, dated March 4, 2024, for Model DG-1000
gliders.
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 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, it 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.
AD Requirements
This AD requires accomplishing the actions specified in the
material already described, except as discussed under ``Differences
Between this AD and the MCAI.''
Differences Between This AD and the MCAI
The MCAI applies to Model DG-100G, DG-100G ELAN, DG-200, DG-200/17,
DG-200/17C, DG-300, DG-300 ELAN, DG-300 Club ELAN, DG-300 ELAN ACRO,
DG-300 Club ELAN ACRO, DG-600, DG-600/18, DG-600M, DG-600/18 M, DG-800
LA, DG-800 S, DG-808 S, and DG-1000E gliders, but this AD does not
because these models do not have an FAA type certificate.
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 operating a glider with the elevator play adjustment screw
screwed in too far could lead to a loss of pitch control of the glider
and loss of the ability to control the glider in flight or during
landing. The FAA has determined that certain gliders will need an
operational check within 3 months and immediate action if any
discrepancy is found and certain other
[[Page 79427]]
gliders will need replacement of an affected part within 3 months after
the effective date of this AD. This compliance time 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 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 101 gliders of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Revise glider maintenance manual 1 work-hour x $85 per $0 85 8,585.
(Group 1 and Group 2 gliders). hour = $85.
Perform operational check of the 1 work-hour x $85 per 0 85 8,585.
free play adjustment of the hour = $85.
automatic elevator hook-up (Group
1 and Group 2 gliders).
Replace the elevator pushrod end 2 work-hours x $85 100 270 7,020 (26 gliders).
(Group 1 gliders). per hour = $170.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary elevator
roller replacement (both Group 1 and Group 2 gliders) or elevator rod
replacement (Group 2 gliders) that would be required based on the
results of the operational check. The agency has no way of determining
the number of gliders that might need these replacements:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replace the elevator roller with a new one and 2 work-hours x $85 per hour = 150 320
adjust free play (Group 1 and Group 2 $170.
gliders).
Replace the elevator pushrod end (Group 2 2 work-hours x $85 per hour = 100 270
gliders). $170.
----------------------------------------------------------------------------------------------------------------
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:
2024-19-12 DG Aviation GmbH (Type Certificate Previously Held by DG
Flugzeugbau GmbH): Amendment 39-22854; Docket No. FAA-2024-2316;
Project Identifier MCAI-2024-00381-G.
(a) Effective Date
This airworthiness directive (AD) is effective October 15, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the following:
(1) DG Aviation GmbH (type certificate previously held by DG
Flugzeugbau GmbH) Model DG-400 gliders, all serial numbers,
certificated in any category, except those
[[Page 79428]]
with l'Hotellier connections of the elevator control installed; and
(2) DG Aviation GmbH (type certificate previously held by DG
Flugzeugbau GmbH) Model DG-500 Elan Orion, DG-500 Elan Trainer, DG-
500/20 Elan, DG-500/22 Elan, DG-500M, DG-500MB, DG-800A, DG-800B,
DG-808C, DG-1000M, DG-1000S, and DG-1000T gliders, all serial
numbers; certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 2730, Elevator
Control System.
(e) Unsafe Condition
This AD was prompted by a report of a broken rod end at the
upper end of the elevator pushrod in the fin (vertical tail) of a DG
Aviation GmbH DG-300 glider. The FAA is issuing this AD to detect
and address the unsafe condition. The unsafe condition, if not
addressed, could result in loss of pitch control of the glider.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definitions
For the purposes of this AD the definitions in paragraphs (g)(1)
through (5) of this AD apply.
(1) The ``applicable technical note for your glider'' is:
(i) Model DG-400 gliders: DG Aviation GmbH Technical Note No.
DG-SS-09, Doc. No. TMDG-SS-09 FE-29-01, Issue 01.f, dated March 5,
2024.
(ii) Model DG-500 gliders: DG Aviation GmbH Technical Note No.
500/17, Doc. No. TM500-17 FE-29-01, Issue 01.c, dated March 5, 2023.
(iii) Model DG-800 gliders: DG Aviation GmbH Technical Note No.
800/50, Doc. No. TM800-50 FE-29-01, Issue 01.c, dated March 5, 2024.
(iv) Model DG-1000 gliders: DG Aviation GmbH Technical Note No.
1000/50, Doc. No. TM1000-50 FE-29-01, Issue 01.c, dated March 4,
2024.
(2) A ``new elevator pushrod end'' is an elevator pushrod with
zero hours time-in-service (TIS) having a part number specified in
the applicable technical note for your glider that has never been
installed on any glider.
(3) A ``new elevator roller'' is an elevator roller with zero
hours TIS having a part number specified in the applicable technical
note for your glider that has never been installed on any glider.
(4) Group 1 gliders: Model DG-400 gliders.
(5) Group 2 gliders: Model DG-500 Elan Orion, DG-500 Elan
Trainer, DG-500/20 Elan, DG-500/22 Elan, DG-500M, DG-500MB, DG-800A,
DG-800B, DG-808C, DG-1000M, DG-1000S, and DG-1000T gliders.
(h) Required Actions
(1) Group 1 and Group 2 gliders: Within 3 months after the
effective date of this AD, revise your existing glider maintenance
manual in accordance with paragraph 1 of the Instructions in the
applicable technical note for your glider.
(2) Group 1 and Group 2 gliders: Within 3 months after the
effective date of this AD, accomplish an operational check of the
free play adjustment of the automatic elevator hook-up in accordance
with paragraph 2 of the Instructions in the applicable technical
note for your glider.
(i) Group 1 gliders: If, during the operational check required
by paragraph (h)(2) of this AD, any discrepancy as described in
paragraph 2 of the Instructions in the applicable technical note for
your glider is detected, before further flight, replace the elevator
roller with a new elevator roller and adjust free play in accordance
with paragraph 2 of the Instructions in the applicable technical
note for your glider. Where the technical note for your glider
specifies to ``mark the removed rod end as [an] unserviceable part''
this AD requires ``removing that elevator pushrod end from
service.'' Where the technical note for your glider specifies ``If a
new rod end is needed, order it immediately at DG'' this AD only
requires ``replacing the elevator pushrod end with a new elevator
pushrod end.''
(ii) Group 2 gliders: If, during the operational check required
by paragraph (h)(2) of this AD, any discrepancy, as described in
paragraph 2 of the Instructions of the applicable technical note for
your glider is detected, before further flight, replace either the
elevator pushrod end or elevator roller or both, as applicable, with
a new elevator pushrod end and new elevator roller and adjust the
free play in accordance with paragraph 2 of the Instructions in the
applicable technical note for your glider. Where the technical note
for your glider specifies to ``mark the removed rod end as [an]
unserviceable part'' this AD requires ``removing that elevator
pushrod end from service.'' Where the technical note for your glider
specifies ``If a new rod end is needed, order it immediately at DG''
this AD only requires ``replacing the elevator pushrod end with a
new elevator pushrod end.''
(3) Group 1 gliders: Within 3 months after the effective date of
this AD, replace the elevator pushrod end with a new elevator
pushrod end in accordance with paragraph 2 of the Instructions in
the applicable technical note for your glider.
(i) Reporting Not Required
Although the Remarks section of the material specified in
paragraph (g)(1) of this AD states to report ``any damaged parts,
false adjustment of the elevator control, or false installation of
parts'' and ``If you find that airworthiness may be affected this
has to be reported to the competent authority,'' this AD does not
require those actions.
(j) Special Flight Permit
Special flight permits are prohibited.
(k) 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 (l) 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.
(l) Additional Information
For more information about this AD, contact Fred Guerin,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (206) 231-2346; email:
[email protected].
(m) 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 the AD specifies otherwise.
(i) DG Aviation GmbH Technical Note No. DG-SS-09, Doc. No. TMDG-
SS-09 FE-29-01, Issue 01.f, dated March 5, 2024.
(ii) DG Aviation GmbH Technical Note No. 500/17, Doc. No. TM500-
17 FE-29-01, Issue 01.c, dated March 5, 2023.
(iii) DG Aviation GmbH Technical Note No. 800/50, Doc. No.
TM800-50 FE-29-01, Issue 01.c, dated March 5, 2024.
(iv) DG Aviation GmbH Technical Note No. 1000/50, Doc. No.
TM1000-50 FE-29-01, Issue 01.c, dated March 4, 2024.
(3) For DG Aviation GmbH material identified in this AD, contact
DG Aviation GmbH, Otto-Lilienthal Weg 2/Am Flugplatz, 76646
Bruchsal, Germany; phone: +49 (0) 7251 36660-32; email: [email protected]; website: 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 September 19, 2024.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-22321 Filed 9-25-24; 4:15 pm]
BILLING CODE 4910-13-P