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2024-03-07 DEUTSCHE AIRCRAFT GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY 328 SUPPORT SERVICES GMBH; AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH): Amendment 39-22677; Docket No. FAA-2023-2230; Project Identifier MCAI-2023-00861-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective April 16, 2024.

(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 and 328-
    300 airplanes, certificated in any category.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) UNSAFE CONDITION

    This AD was prompted by operator reports of worn and ruptured  bonding
    straps inside the feeder wing tanks  and in both outer and inner  wing
    tanks. The FAA is issuing  this AD to address damaged  bonding straps.
    The unsafe condition,  if not addressed,  could result in  the loss of
    bonding function and, in combination with a lightning strike, create a
    source of ignition  in a fuel  tank, possibly resulting  in a fire  or
    explosion and consequent loss of the airplane.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready 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 2023-0137, dated
    July 12, 2023 (EASA AD 2023-0137).

(h) EXCEPTIONS TO EASA AD 2023-0137

(1) Where EASA AD 2023-0137 refers to its effective date, this AD requires
    using the effective date of this AD.

(2) This AD does not adopt the "Remarks" section of EASA AD 2023-0137.

(3) Where paragraph (2)  of EASA AD 2023-0137  specifies if "any damage is
    detected as defined in the ASB,"  this  AD  requires  replacing  those
    words with "any worn or ruptured bonding strap is detected."

(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  manager  of  the International
    Validation Branch, mail it to the address 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  accom-
    plished using a method approved by the Manager,  International Valida-
    tion 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 2023-0137,  dated July
    12, 2023.

(ii) [Reserved]

(3) For EASA AD 2023-0137,  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 website
    at ad.easa.europa.eu.

(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 Admin-
    istration (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 February 8, 2024. Victor Wicklund, Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39


[Docket No. FAA-2023-2230; Project Identifier MCAI-2023-00861-T;
Amendment 39-22677; AD 2024-03-07]
RIN 2120-AA64

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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Deutsche Aircraft GmbH Model 328-100 and 328-300 airplanes. This AD was
prompted by operator reports of worn and ruptured bonding straps inside
the feeder wing tanks and in both outer and inner wing tanks. This AD
requires a one-time detailed inspection of each affected part, and
applicable corrective actions, as specified in a European Union
Aviation Safety Agency (EASA) AD, which is incorporated by reference.
The FAA is issuing this AD to address the unsafe condition on these
products.

DATES: This AD is effective April 16, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 16,
2024.

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-2230; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For EASA material incorporated by reference in this AD,
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 at ad.easa.europa.eu.
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. It is also available in the AD docket at
regulations.gov under Docket No. FAA-2023-2230.

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:

Background

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to 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 and 328-300 airplanes. The NPRM published in the Federal
Register on December 6, 2023 (88 FR 84764). The NPRM was prompted by AD
2023-0137, dated July 12, 2023 (EASA AD 2023-0137) (also referred to as
the MCAI), issued by EASA, which is the Technical Agent for the Member
States of the European Union. The MCAI states that operators reported
findings of damaged affected parts. The extent of the detected damage
of the affected parts did not ensure that appropriately low electrical
impedance is obtained and maintained through the affected bonding path.
The unsafe condition, if not detected and corrected, could lead to the
loss of bonding function and, in combination with a lightning strike,
create a source of ignition in a fuel tank, possibly resulting in a
fire or explosion.
In the NPRM, the FAA proposed to require a one-time detailed
inspection of each affected part, and applicable corrective actions, as
specified in EASA AD 2023-0137. The FAA is issuing this AD to address
the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-2230.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

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 reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.

Related Service Information Under 1 CFR Part 51

EASA AD 2023-0137 specifies procedures for a one-time detailed
inspection of each affected part for worn and ruptured bonding straps,
and applicable corrective actions (replacing the affected parts). 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.

Interim Action

The FAA considers that this AD is 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 affects 35 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per product
Cost on U.S. operators
44 work-hours x $85 per hour = $3,740
$0
$3,740
$130,900

The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need these on-condition actions:
The FAA has received no definitive data on which to base the cost
estimates for the on-condition actions specified in this AD.

Authority for This Rulemaking


Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.

Regulatory Findings


This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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: