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PROPOSED AD DEUTSCHE AIRCRAFT GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY 328 SUPPORT SERVICES GMBH; AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH): Docket No. FAA-2023-1707; Project Identifier MCAI-2023-00605-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    September 28, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to all Deutsche Aircraft GmbH  (Type Certificate Pre-
    viously Held by 328  Support  Services  GmbH;  AvCraft Aerospace GmbH;
    Fairchild Dornier GmbH;  Dornier  Luftfahrt  GmbH)  Model 328-100 air-
    planes, certificated in any category.

(d) SUBJECT

    Air Transport Association (ATA) of America Code: 53, Fuselage.

(e) UNSAFE CONDITION

    This AD was prompted by a report of finding cracks in fuselage  frames
    (FR) 24 and FR26. The FAA is issuing this AD to address cracks in FR24
    and FR26.  The unsafe  condition, if  not addressed,  could result  in
    failure of  load carrying  structural elements,  possibly resulting in
    reduced integrity of the fuselage.

(f) COMPLIANCE

    Comply  with this  AD within  the compliance  times specified,  unless
    already done.

(g) REQUIREMENTS

    Except as specified in paragraph (h)  of this AD:  Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, European Union Aviation Safety Agency (EASA) AD 2023-0081, dated
    April 18, 2023 (EASA AD 2023-0081).

(h) EXCEPTIONS TO EASA AD 2023-0081

(1) Where EASA AD 2023-0081 refers to its effective date, this AD requires
    using the effective date of this AD.

(2) Where paragraph (1) of EASA AD 2023-0081  refers  to  compliance  time
    within 1,500 FC  or accomplishment of  Deutsche Aircraft GmbH  Dornier
    328 Maintenance Review Board Report (MRBR) task 53-41-37-02,  for this
    AD compliance time  is within 1,500 flight cycles  after the effective
    date of this AD.

(3) Where paragraph (2) of EASA AD 2023-0081 refers to "damages," for this
    AD damages are any possible cracks and surface cracks.

(4) This AD does not adopt the "Remarks" section of EASA AD 2023-0081.

(i) ADDITIONAL AD PROVISIONS

    The following provisions also apply to this AD:

(1) 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 responsible Flight  Standards Office, as appropriate.  If
    sending information directly  to the International  Validation Branch,
    send it to the attention of the person identified in paragraph (j)  of
    this AD.  Information may  be emailed  to: 9-AVS-AIR-730-AMOC@faa.gov.
    Before  using any  approved AMOC,  notify  your  appropriate 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 EASA;  or Deutsche  Aircraft GmbH's  EASA
    Design  Organization  Approval  (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 service information  listed in this  paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable  to do the actions
    required by this AD, unless this AD specifies otherwise.

(i) European Union Aviation Safety Agency (EASA) AD 2023-0081, dated April
    18, 2023.

(ii) [Reserved]

(3) For EASA AD 2023-0081,  contact  EASA,  Konrad-Adenauer-Ufer 3,  50668
    Cologne, Germany; telephone +49 221 8999 000;  email: ADs@easa.europa.
    eu; website: easa.europa.eu. You may find this EASA AD on the EASA web
    site: ad.easa.europa.eu.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts Section, Operational Safety Branch,  2200 South 216th Street, Des
    Moines, WA.  For information  on the availability  of this material at
    the FAA, call 206-231-3195.

(5) You may view  this service information  that is incorporated by refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information on the availability  of this material  at NARA,  email fr.
    inspection@nara.gov,  or go to: www.archives.gov/federal-register/cfr/
    ibr-locations.html.

Issued on August 3, 2023.  Victor Wicklund,  Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD  by September 28,
2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1707; Project Identifier MCAI-2023-00605-T]
RIN 2120-AA64

Airworthiness Directives; Deutsche Aircraft GmbH (Type
Certificate Previously Held by 328 Support Services GmbH; AvCraft
Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH)
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Deutsche Aircraft GmbH (Type Certificate Previously Held by 328
Support Services GmbH; AvCraft Aerospace GmbH; Fairchild Dornier GmbH;
Dornier Luftfahrt GmbH) Model 328-100 airplanes. This proposed AD was
prompted by a report of finding cracks in fuselage frames (FR) 24 and
FR26. This proposed AD would require a one-time detailed and eddy
current inspection of fuselage FR24 and FR26 (left and right sides),
performing corrective actions if necessary, and reporting the
inspection results, as specified in a European Union Aviation Safety
Agency (EASA) AD, which is proposed for incorporation by reference
(IBR). 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 September
28, 2023.

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-2023-1707; 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, 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 material that is proposed for IBR in this NPRM,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email: ADs@easa.europa.eu; website: easa.europa.eu.
You may find this material on the EASA website: ad.easa.europa.eu. It
is also available at regulations.gov under Docket No. FAA-2023-1707.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For information on the availability of
this material at the FAA, call 206-231-3195.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 206-231-3228; email todd.thompson@faa.gov.

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-2023-1707; Project Identifier
MCAI-2023-00605-T'' 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
regulations.gov, 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 Todd
Thompson, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 206-231-3228; email
todd.thompson@faa.gov. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.

Background

EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2023-0081, dated April 18, 2023
(EASA AD 2023-0081) (also referred to as the MCAI), to correct an
unsafe condition for all Deutsche Aircraft GmbH (Type Certificate
Previously Held by 328 Support Services GmbH; AvCraft Aerospace GmbH;
Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328-100
airplanes. The MCAI states a report of finding cracks in fuselage
frames FR24 and FR26. Investigation of the root cause for cracking is
ongoing. This condition, if not detected and corrected, could lead to
failure of load carrying structural elements, possibly resulting in
reduced integrity of the fuselage. The FAA is proposing 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-2023-1707.

Related Service Information Under 1 CFR Part 51

EASA AD 2023-0081 specifies procedures for a one-time detailed and
eddy current inspection of fuselage FR24 and FR26 (left and right
sides) for damage (cracks). Depending on the inspection results, EASA
AD 2023-0081 also specifies corrective action, including obtaining and
following instructions for crack repair. EASA AD 2023-0081 also
requires reporting the inspection results to Deutsche Aircraft GmbH.
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 ADDRESSES section.

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
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA is issuing this NPRM after determining that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified
in EASA AD 2023-0081 described previously, except for any differences
identified as exceptions in the regulatory text of this proposed AD.

Explanation of Required Compliance Information

In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate EASA AD 2023-0081 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2023-0081 in its entirety through that incorporation, except
for any differences identified as exceptions in the regulatory text of
this proposed AD. Using common terms that are the same as the heading
of a particular section in EASA AD 2023-0081 does not mean that
operators need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2023-
0081. Service information required by EASA AD 2023-0081 for compliance
will be available at regulations.gov under Docket No. FAA-2023-1707
after the FAA final rule is published.

Interim Action

The FAA considers that this proposed AD would be an interim action.
If final action is later identified, the FAA might consider further
rulemaking then.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 21 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per product
Cost on U.S. operators
22 work-hours x $85 per hour = $1,870
$0
$1,870
$39,270

The FAA has received no definitive data on which to base the cost
estimates for the on-condition repairs specified in this proposed AD.

Paperwork Reduction Act

A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to a penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of
information displays a current valid OMB Control Number. The OMB
Control Number for this information collection is 2120-0056. Public
reporting for this collection of information is estimated to take
approximately 1 hour per response, including the time for reviewing
instructions, searching existing data sources, gathering and
maintaining the data needed, and completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Send comments regarding this burden estimate
or any other aspect of this collection of information, including
suggestions for reducing this burden, to: Information Collection
Clearance Officer, Federal Aviation Administration, 10101 Hillwood
Parkway, Fort Worth, TX 76177-1524.

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

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]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: