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2020-09-13 328 SUPPORT SERVICES GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH): Amendment 39-19909; Docket No. FAA-2020-0090; Product Identifier 2019-NM-196-AD.
(a) EFFECTIVE DATE

    This AD is effective June 22, 2020.

(b) AFFECTED ADS

    This AD affects the ADs identified  in  paragraphs (b)(1)  and  (2) of
    this AD:

(1) AD 2009-01-06 R1,  Amendment 39-16082  (74 FR 57411, November 6, 2009)
    ("AD 2009-01-06 R1").

(2) AD 2012-01-08,  Amendment 39-16920 (77 FR 3583, January 25, 2012) ("AD
    2012-01-08").

(c) APPLICABILITY

    This AD  applies to  all 328  Support Services  GmbH (Type Certificate
    previously held  by AvCraft  Aerospace GmbH;  Fairchild Dornier  GmbH;
    Dornier Luftfahrt GmbH) Model  328-300 airplanes, certificated in  any
    category.

(d) SUBJECT

    Air  Transport  Association  (ATA)  of  America Code 05,  Time Limits/
    Maintenance Checks.

(e) REASON

    This AD was prompted by  a determination that new or  more restrictive
    airworthiness limitations are necessary. The FAA is issuing this AD to
    address the potential  failure of parts,  which could lead  to reduced
    control of  the airplane;  and to  address the  potential of  ignition
    sources inside fuel tanks,  which, in combination with  flammable fuel
    vapors, could result  in fuel tank  explosions 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 2019-0271, dated
    October 30, 2019 ("EASA AD 2019-0271").

(h) EXCEPTIONS TO EASA AD 2019-0271

(1) The requirements specified  in paragraphs (1) and (2) of EASA AD 2019-
    0271 do not apply to this AD.

(2) Where paragraph (3)  of EASA AD 2019-0271 specifies  a compliance time
    of "Within 12 months" after its effective date to "revise the approved
    AMP" this AD requires "revising the existing maintenance or inspection
    program, as applicable,"  to incorporate the "limitations,  tasks  and
    associated thresholds and intervals,"  specified  in  paragraph (3) of
    EASA AD 2019-0271 within 90 days after the effective date of this AD.

(3) The initial compliance time for doing the tasks specified in paragraph
    (3) of EASA AD 2019-0271 is at the applicable  "associated thresholds"
    specified in paragraph (3) of EASA AD 2019-0271,  or  within  90  days
    after the effective date of this AD, whichever occurs later.

(4) The provisions specified  in paragraphs (4) and (5)  of  EASA AD 2019-
    0271 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2019-0271 does not apply to this AD.

(i) PROVISIONS FOR ALTERNATIVE ACTIONS, INTERVALS AND CRITICAL DESIGN CON-
    FIGURATION CONTROL LIMITATION (CDCCLS)

    After the existing maintenance or inspection program has been  revised
    as required by paragraph (g) of this AD, no alternative actions (e.g.,
    inspections), intervals, and CDCCLs are allowed except as specified in
    the provisions  of the  "Ref. Publications"  section of  EASA AD  2019
    -0271.

(j) TERMINATING ACTION FOR OTHER ADS

(1) Accomplishing the maintenance  or inspection program revision required
    by paragraph (g) of this AD terminates all requirements of AD 2009-01-
    06 R1.

(2) Accomplishing the maintenance  or inspection program revision required
    by paragraph (g) of this AD terminates all requirements of AD 2012-01-
    08 for Model 328-300 airplanes only.

(k) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft
    Section,  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  Large Aircraft
    Section, International Validation Branch,  send it to the attention of
    the person identified in paragraph (l) of this AD.  Information may be
    emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved
    AMOC, notify your appropriate principal inspector,  or lacking a prin-
    cipal inspector,  the  manager  of the local flight standards district
    office/certificate holding district 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, Large  Aircraft
    Section, International Validation Branch, FAA; or EASA; or 328 Support
    Services GmbH's EASA Design  Organization Approval (DOA). If  approved
    by the DOA, the approval must include the DOA-authorized signature.

(l) RELATED INFORMATION

    For more information about this AD,  contact Todd Thompson,  Aerospace
    Engineer, Large Aircraft Section, International Validation Branch, FAA
    2200 South 216th St, Des Moines, WA 98198; phone and fax: 206-231-3228
    email: todd.thompson@faa.gov.

(m) 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 2019-0271, dated
    October 30, 2019.

(ii) [Reserved]

(3) For information about EASA AD 2019-0271,  contact  the  EASA,  Konrad-
    Adenauer-Ufer 3,  50668 Cologne,  Germany;  phone: +49 221 89990 6017;
    email: ADs@easa.europa.eu; internet: www.easa.europa.eu.  You may find
    this EASA AD on the EASA website at https://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.  This material may be found in the AD docket on the internet
    at https://www.regulations.gov  by searching for  and  locating Docket
    No. FAA-2020-0090.

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

Issued on May 6, 2020. Lance T. Gant, Director, Compliance & Airworthiness
Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,  Large
Aircraft Section,  International Validation Branch,  FAA, 2200 South 216th
St, Des Moines, WA 98198; phone and fax: 206-231-3228; email todd.thompson
@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0090; Product Identifier 2019-NM-196-AD; Amendment
39-19909; AD 2020-09-13]
RIN 2120-AA64

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

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
328 Support Services GmbH Model 328-300 airplanes. This AD was prompted
by a determination that new or more restrictive airworthiness
limitations are necessary. This AD requires revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations, 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 June 22, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 22,
2020.

ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
phone: +49 221 89990 1000; email: ADs@easa.europa.eu; internet:
www.easa.europa.eu. You may find this IBR material on the EASA website
at https://ad.easa.europa.eu. You may view this IBR 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 on the internet at https://www.regulations.gov by
searching for and locating Docket No. FAA-2020-0090.

Examining the AD Docket

You may examine the AD docket on the internet at https://www.regulations.
gov by searching for and locating Docket No. FAA-2020-
0090; 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, 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.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3228;
email: todd.thompson@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2019-0271, dated October 30, 2019
(``EASA AD 2019-0271'') (referred to after this as the Mandatory
Continuing Airworthiness Information, or ``the MCAI''), to correct an
unsafe condition for all 328 Support Services GmbH Model 328-300
airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all 328 Support
Services GmbH Model 328-300 airplanes. The NPRM published in the
Federal Register on February 12, 2020 (85 FR 7897). The NPRM was
prompted by a determination that new or more restrictive airworthiness
limitations are necessary. The NPRM proposed to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations, as
specified in an EASA AD.
The FAA is issuing this AD to address the potential failure of
parts, which could lead to reduced control of the airplane; and to
address the potential of ignition sources inside fuel tanks, which, in
combination with flammable fuel vapors, could result in fuel tank
explosions and consequent loss of the airplane. See the MCAI for
additional background information.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.

Conclusion

The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this
final rule as proposed, except for minor editorial changes. The FAA has
determined that these minor changes:

Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Related IBR Material Under 1 CFR Part 51


EASA AD 2019-0271 describes procedures for airworthiness
limitations for certification maintenance requirements that include,
among other items, safe life limits and fuel tank system limitations.
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.

Costs of Compliance

The FAA estimates that this AD affects 21 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
FAA recognizes that this number may vary from operator to operator. In
the past, the FAA has estimated that this action takes 1 work-hour per
airplane. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), the FAA has determined that a per-
operator estimate is more accurate than a per-airplane estimate.
Therefore, the FAA estimates the total cost per operator to be $7,650
(90 work-hours x $85 per work-hour).

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.

Adoption of 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 (AD):