Proposed Rule2021-13988
Airworthiness Directives; DG Flugzeugbau GmbH Gliders
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
July 1, 2021
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Models DG-808C and DG-1000T gliders. This proposed AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as damaged fuel hoses due to environmental and fatigue deterioration. This proposed AD would require inspecting the polyurethane (PU) fuel hoses, replacing the PU fuel hoses if there is damage, and establishing a life limit for the PU fuel hoses. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 86 Issue 124 (Thursday, July 1, 2021)</title>
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[Federal Register Volume 86, Number 124 (Thursday, July 1, 2021)]
[Proposed Rules]
[Pages 35027-35030]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-13988]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0212; Project Identifier 2018-CE-032-AD]
RIN 2120-AA64
Airworthiness Directives; DG Flugzeugbau GmbH Gliders
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all
[[Page 35028]]
DG Flugzeugbau GmbH Models DG-808C and DG-1000T gliders. This proposed
AD was prompted by mandatory continuing airworthiness information
(MCAI) originated by an aviation authority of another country to
identify and correct an unsafe condition on an aviation product. The
MCAI describes the unsafe condition as damaged fuel hoses due to
environmental and fatigue deterioration. This proposed AD would require
inspecting the polyurethane (PU) fuel hoses, replacing the PU fuel
hoses if there is damage, and establishing a life limit for the PU fuel
hoses. The FAA is proposing this AD to address the unsafe condition on
these products.
DATES: The FAA must receive comments on this proposed AD by August 16,
2021.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="https://www.regulations.gov">https://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: (202) 493-2251.
<bullet> 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.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact DG
Flugzeugbau GmbH, Otto-Lilienthal Weg 2, D-76646 Bruchsal, Germany;
phone: +49 (0)7251 3202-0; email: <a href="/cdn-cgi/l/email-protection#771e1911183713105a111b02100d120210151602591312"><span class="__cf_email__" data-cfemail="573e3931381733307a313b22302d322230353622793332">[email protected]</span></a>; website:
<a href="https://www.dg-flugzeugbau.de/">https://www.dg-flugzeugbau.de/</a>. You may view this service information
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 (816) 329-4148.
Examining the AD Docket
You may examine the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2021-0212; 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 NPRM, any comments
received, and other information. The street address for Docket
Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aviation Safety
Engineer, General Aviation & Rotorcraft Section, International
Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106;
phone: (816) 329-4165; fax: (816) 329-4090; email:
<a href="/cdn-cgi/l/email-protection#b1dbd8dc9fc3c4c5d9d4c3d7dec3d5f1d7d0d09fd6dec7"><span class="__cf_email__" data-cfemail="503a393d7e222524383522363f2234103631317e373f26">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2021-0212; Project Identifier
2018-CE-032-AD'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, 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 proposal 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
<a href="https://www.regulations.gov">https://www.regulations.gov</a>, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.
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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to Jim
Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft
Section, International Validation Branch, FAA, 901 Locust, Room 301,
Kansas City, MO 64106. 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 Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2018-0127, dated June 11, 2018 (referred to after this as ``the
MCAI''), to address an unsafe condition on DG Flugzeugbau GmbH Models
DG-808C and DG-1000T gliders. The MCAI states:
An occurrence was reported where, during accomplishment of a 10
years inspection on a DG-808C powered sailplane, a damaged (broken)
PU [polyurethane] fuel hose was found. The result of subsequent
investigation indicated that the damage mode has features of
environmental and fatigue deterioration. Additionally, it was
determined that similar PU fuel hoses are also installed on other
powered sailplane types of the same manufacturer.
This condition, if not detected and corrected, could lead to
reduced or interrupted fuel supply to the engine, consequent loss of
the available power or fire, possibly resulting in reduced control
of the powered sailplane.
To address this potential unsafe condition, DG-Flugzeugbau GmbH
issued the applicable TN [Technical Note], providing instructions to
inspect the affected parts and replace these with serviceable parts.
Additionally, service life limits were established for those
serviceable parts.
For the reasons described above, this [EASA] AD requires
repetitive inspections of the affected parts. This [EASA] AD also
requires replacement of the affected parts with serviceable parts
and introduces life limits for serviceable parts.
You may examine the MCAI in the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2021-
0212.
Related Service Information Under 1 CFR Part 51
The FAA reviewed DG Flugzeugbau GmbH Technical Note No. 800/46,
Issue 01.a, dated March 7, 2018, for Model DG-808C gliders; and
Technical Note No. 1000/38, Issue 01.a, dated February 15, 2018, for
Model DG-1000T gliders. The service information, as applicable to the
appropriate model glider, specifies inspections of the PU fuel hoses,
replacement of the PU fuel hoses if damage is found during an
inspection, and actions to take when the hoses have reached their life
limit. This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in ADDRESSES.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
our bilateral agreement with this State of Design Authority, it has
notified the FAA of the unsafe condition described in the MCAI and
service information
[[Page 35029]]
referenced above. The FAA is issuing this NPRM after determining the
unsafe condition described previously is likely to exist or develop on
other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the service information already described, except as discussed under
``Differences Between this Proposed AD and the MCAI.''
Differences Between This Proposed AD and the MCAI
The MCAI requires replacing any damaged fuel hoses before next
engine operation, while this proposed AD would require replacing
damaged fuel hoses before further flight. Even though use of the engine
is optional and the glider can operate without the engine, the glider
has other electronic equipment installed that could cause arcing and
result in an in-flight fire if there is a fuel leak.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 10 gliders of U.S. registry. The FAA also estimates that it
would take about 2 work-hours per glider to comply with each inspection
required by this proposed AD. The average labor rate is $85 per work-
hour.
Based on these figures, the FAA estimates the inspection cost of
this proposed AD on U.S. operators to be $1,700, or $170 per glider,
each inspection cycle.
In addition, the FAA estimates that each replacement action
required by this proposed AD would take about 8 work-hours and require
parts costing $500. Based on these figures, the FAA estimates the
replacement cost of this proposed AD on U.S. operators to be $1,180 per
glider.
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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
DG Flugzeugbau GmbH: Docket No. FAA-2021-0212; Project Identifier
2018-CE-032-AD.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 16, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to DG Flugzeugbau GmbH Models DG-808C and DG-
1000T gliders, all serial numbers, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 2800, Aircraft Fuel
System.
(e) Unsafe Condition
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as damaged
polyurethane (PU) fuel hoses due to environmental and fatigue
deterioration. The FAA is issuing this AD to prevent reduced or
interrupted fuel supply to the engine or fuel leakage. The unsafe
condition, if not addressed, could result in loss of engine power or
in-flight fire.
(f) Definitions
(1) For purposes of this AD, an ``affected part'' is a PU fuel
hose installed in an airframe fuel system or engine compartment
that:
(i) Does not meet industrial standard DIN 73379-2A, or
(ii) Does not meet ISO 7840-A1 without metal shielding.
(2) For purposes of this AD, a ``serviceable part'' is a PU fuel
hose installed in an airframe fuel system or engine compartment
that:
(i) Meets industrial standard DIN 73379-2A, or
(ii) Meets industrial standard ISO 7840-A1 without metal
shielding.
(g) Inspections for Gliders With An Affected Part Installed
Within the next 30 days after the effective date of this AD and
thereafter at intervals not to exceed 12 months, visually inspect
each affected part for fissures, kinks, and leaks. For this
inspection, the ignition switch must be turned on to run the
electric fuel pump to demonstrate an operating fuel pressure.
(1) If a fissure, kink, or leak is found on an affected part
during any inspection required by the introductory language to
paragraph (g) of this AD, before further flight: Replace all
affected parts with unused (zero hours time-in-service (TIS))
serviceable parts by following paragraphs 3 and 4 of the
Instructions in DG Flugzeugbau GmbH Technical Note No. 800/46, Issue
01.a, dated March 7, 2018 (TN No. 800/46), or paragraphs 3 through 5
of the Instructions in DG Technical Note No. 1000/38, Issue 01.a,
dated February 15, 2018 (TN No. 1000/38), as applicable to your
model glider.
(2) If no fissures, kinks, and leaks are found on all affected
parts during any inspection required by the introductory language to
paragraph (g) of this AD, before each affected part accumulates 6
years since first installation on a glider or within 6 months after
the effective date of this AD, whichever occurs later: Replace all
affected parts with unused (zero hours TIS) serviceable parts by
following paragraphs 3 and 4 of the Instructions in TN No. 800/46 or
paragraphs 3 through 5 of the Instructions in TN No. 1000/38, as
applicable to your model glider. If the date of first installation
on a glider is unknown for any affected hose, replace all affected
hoses within 6 months after the effective date of this AD.
[[Page 35030]]
(h) Inspections for Gliders With Only Serviceable Parts Installed
(1) Before or upon accumulating 6 years since first installation
on a glider and thereafter at intervals not to exceed 12 months,
visually inspect each serviceable part for fissures, kinks, and
leaks. For this inspection, the ignition switch must be turned on to
run the electric fuel pump to demonstrate an operating fuel
pressure.
(2) If a fissure, a kink, or a leak is found during any
inspection required by paragraph (h)(1) of this AD, before further
flight, replace the part with an unused (zero hours TIS) serviceable
part by following paragraphs 3 and 4 of the Instructions in TN No.
800/46 or paragraphs 3 through 5 of the Instructions in TN No. 1000/
38, as applicable to your model glider.
(i) Life Limit
Before accumulating 10 years since first installation on a
glider and thereafter at intervals not to exceed 10 years, remove
each serviceable part from service and replace with an unused (zero
hours TIS) serviceable part by following paragraphs 3 and 4 of the
Instructions in TN No. 800/46 or paragraphs 3 through 5 of the
Instructions in TN No. 1000/38, as applicable to your model glider.
(j) Parts Installation Prohibition
As of the effective date of this AD, do not install an affected
part on any glider.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation Branch, 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 certification office, send it to the
attention of the person identified in Related Information or email:
<a href="/cdn-cgi/l/email-protection#cdf4e08c9b9ee08c849fe0fafefde08c80828e8dabacace3aaa2bb"><span class="__cf_email__" data-cfemail="f5ccd8b4a3a6d8b4bca7d8c2c6c5d8b4b8bab6b5939494db929a83">[email protected]</span></a>.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(l) Related Information
(1) For more information about this AD contact Jim Rutherford,
Aviation Safety Engineer, General Aviation & Rotorcraft Section,
International Validation Branch, FAA, 901 Locust, Room 301, Kansas
City, MO 64106; phone: (816) 329-4165; fax: (816) 329-4090; email:
<a href="/cdn-cgi/l/email-protection#8ee4e7e3a0fcfbfae6ebfce8e1fceacee8efefa0e9e1f8"><span class="__cf_email__" data-cfemail="23494a4e0d5156574b4651454c5147634542420d444c55">[email protected]</span></a>.
(2) Refer to European Aviation Safety Agency (EASA) AD 2018-
0127, dated June 11, 2018, for more information. You may examine the
EASA AD in the AD docket on the website at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-
2021-0212.
(3) For service information identified in this AD, contact DG
Flugzeugbau GmbH, Otto-Lilienthal Weg 2, D-76646 Bruchsal, Germany;
phone: +49 (0)7251 3202-0; email: <a href="/cdn-cgi/l/email-protection#0b62656d644b6f6c266d677e6c716e7e6c696a7e256f6e"><span class="__cf_email__" data-cfemail="a2cbccc4cde2c6c58fc4ced7c5d8c7d7c5c0c3d78cc6c7">[email protected]</span></a>; website:
<a href="https://www.dg-flugzeugbau.de/">https://www.dg-flugzeugbau.de/</a>. You may review this referenced
service information 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
(816) 329-4148.
Issued on June 25, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-13988 Filed 6-30-21; 8:45 am]
BILLING CODE 4910-13-P
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