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2012-01-08 328 SUPPORT SERVICES GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH): Amendment 39-16920. Docket No. FAA-2011-0995; Directorate Identifier 2010-NM-243-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective February 29, 2012.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to  328  Support  Services  GmbH  (Type Certificate
    Previously Held  by AvCraft  Aerospace GmbH;  Fairchild Dornier  GmbH;
    Dornier  Luftfahrt   GmbH)  Model   328-100  and   328-300  airplanes;
    certificated in any category; all serial numbers.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 27: Flight Controls.

(e) REASON

    This  AD was  prompted by  a  manufacturer  safety analysis  review on
    flight  control   which  resulted   in  recommendations   for  reduced
    repetitive inspection intervals for the flight controls  certification
    maintenance requirements (CMR) of the tab-to-actuator linkage. We  are
    issuing  this  AD to  prevent  failure of  these  components or  their
    constituent parts which could lead to reduced control of the airplane.

(f) COMPLIANCE

    You  are  responsible  for  having the  actions  required  by  this AD
    performed within  the compliance  times specified,  unless the actions
    have already been done.

(g) MAINTENANCE PROGRAM REVISION

    Within 100 flight  hours after the  effective date of  this AD: Revise
    the airplane maintenance program  by incorporating the applicable  CMR
    tasks identified in table 1 of this AD.

                            TABLE 1 - CMR TASKS
__________________________________________________________________________
MODEL        TASK NO.       TASK DESCRIPTION         IDENTIFIED IN
__________________________________________________________________________
328-100      Task           Visual Check of          328 Support Services
airplanes    27-10-00-09    Mechanical Linkages:     Dornier 328
                            Aileron Trim Tab to      Certification
                            Actuator.                Maintenance
                                                     Requirements Document
                                                     TM-CMR-010793-ALL,
                                                     Revision 13, dated
                                                     April 30, 2007.

328-100      Task           Visual Check of          328 Support Services
airplanes    27-20-00-09    Mechanical Linkages:     Dornier 328
                            Rudder Trim Tab/Spring   Certification
                            Tab to Actuator.         Maintenance
                                                     Requirements Document
                                                     TM-CMR-010793-ALL,
                                                     Revision 13, dated
                                                     April 30, 2007.

328-100      Task           Visual Check of          328 Support Services
airplanes    27-30-00-13    Mechanical Linkages:     Dornier 328
                            Elevator Trim Tabs to    Certification
                            Actuator.                Maintenance
                                                     Requirements Document
                                                     TM-CMR-010793-ALL,
                                                     Revision 13, dated
                                                     April 30, 2007.

328-300      Task           Visual Check of          328 Support Services
airplanes    27-10-00-13    Linkage: Aileron Trim    Dornier 328JET
                            Tab to Actuator.         Certification
                                                     Maintenance
                                                     Requirements Document
                                                     TM-CMR-010599-ALL,
                                                     Revision 2, dated May
                                                     1, 2007.

328-300      Task           Visual Check of          328 Support Services
airplanes    27-20-00-11    Linkage: Rudder Trim     Dornier 328JET
                            Tab/Spring Tab.          Certification
                                                     Maintenance
                                                     Requirements Document
                                                     TM-CMR-010599-ALL,
                                                     Revision 2, dated May
                                                     1, 2007.

328-300      Task           Visual Check of          328 Support Services
airplanes    27-30-00-14    Linkage: Elevator Trim   Dornier 328JET
                            Tabs to Actuator.        Certification
                                                     Maintenance
                                                     Requirements Document
                                                     TM-CMR-010599-ALL,
                                                     Revision 2, dated May
                                                     1, 2007.
__________________________________________________________________________

(h) INITIAL COMPLIANCE TIME

    The initial compliance time for the CMR tasks identified in table 1 of
    this AD is within 500  flight hours after the most  recent inspection,
    or  within 100  flight hours  after the  effective date  of  this  AD,
    whichever occurs later.

(i) NO ALTERNATIVE INSPECTIONS OR INSPECTION INTERVALS

    After accomplishing the revision required by paragraph (g) of this AD,
    no alternative inspection  or inspection interval  may be used  unless
    the inspection or  inspection interval is  approved as an  alternative
    method  of  compliance  (AMOC)  in  accordance  with  the   procedures
    specified in paragraph (j)(1) of this AD.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance:  The Manager, International Branch,
    ANM-116, Transport  Airplane Directorate,  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  International
    Branch,  send   it  to   ATTN:  Tom   Rodriguez,  Aerospace  Engineer,
    International  Branch,  ANM-116, Transport  Airplane  Directorate, FAA
    1601 Lind Avenue SW.,  Renton, Washington 98057-3356; telephone  (425)
    227-1137; fax  (425) 227-1149.  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  principal
    inspector,  the  manager  of  the  local  flight  standards   district
    office/certificate holding district  office. The AMOC  approval letter
    must specifically reference this AD.

(2) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product is airworthy before  it
    is returned to service.

(k) RELATED INFORMATION

    Refer to  MCAI European  Aviation Safety  Agency (EASA)  Airworthiness
    Directive 2010-0054, dated March  25, 2010, and the  following service
    information identified in paragraphs (k)(1) and (k)(2) of this AD; for
    related information.

(1) 328   Support   Services   Dornier   328   Certification   Maintenance
    Requirements Document TM-CMR-010793-ALL, Revision 13,  dated April 30,
    2007.

(2) 328  Support  Services  Dornier   328JET   Certification   Maintenance
    Requirements Document TM-CMR-010599-ALL Revision 2, dated May 1, 2007.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) You  must  use  the  following  service  information to do the actions
    required by this AD, unless  the AD specifies otherwise. The  Director
    of the Federal Register approved the incorporation by reference  (IBR)
    of the following service information  under 5 U.S.C. 552(a) and  1 CFR
    part 51.

(i) 328   Support   Services   Dornier   328   Certification   Maintenance
    Requirements Document TM-CMR-010793-ALL, Revision 13, dated  April 30,
    2007. The document number of this document is listed only on the title
    page of the document.

(ii) 328  Support  Services  Dornier  328JET   Certification   Maintenance
     Requirements  Document TM-CMR-010599-ALL,  Revision 2,  dated  May 1,
     2007. The  document number  of this  document is  listed only  on the
     title page of the document.

(2) For  service  information  identified  in this AD, contact 328 Support
    Services GmbH, Global Support Center, P.O. Box 1252, D-82231 Wessling,
    Federal Republic of Germany; telephone: +49 8153 88111 6666; fax:  +49
    8153    88111    6565;    email:    gsc.op@328support.de;    Internet:
    http://www.328support.de.

(3) You may review copies of the service information at the FAA, Transport
    Airplane Directorate,  1601 Lind  Avenue SW.,  Renton, Washington. For
    information on  the availability  of this  material at  the FAA,  call
    (425) 227-1221.

(4) You  may  also  review  copies  of  the  service  information  that is
    incorporated  by  reference  at  the  National  Archives  and  Records
    Administration (NARA).  For information  on the  availability of  this
    material  at  an  NARA  facility,  call  (202)  741-6030,  or  go   to
    http://www.archives.gov/federal_register/code_of_federal_regulations/i
    br_locations.html.

Issued in Renton,  Washington, on January 13, 2012.  John  Piccola, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

FOR  FURTHER  INFORMATION  CONTACT:  Tom  Rodriguez,  Aerospace  Engineer,
International Branch,  ANM-116, Transport  Airplane Directorate,  FAA 1601
Lind Avenue SW., Renton, Washington 98057-3356;  telephone (425) 227-1137;
fax (425) 227-1149.
PREAMBLE 

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

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for all 328
Support Services GmbH (Type Certificate previously held by AvCraft
Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model
328-100 and 328-300 airplanes. This AD was prompted by a manufacturer
safety analyses review on flight control which resulted in
recommendations for reduced repetitive inspection intervals for the
flight controls certification maintenance requirements (CMR) of the
tab-to-actuator linkage. This AD requires revising the airplane
maintenance program by incorporating certain CMR tasks. We are issuing
this AD to prevent failure of these components or their constituent
parts which could lead to reduced control of the airplane.

DATES: This AD becomes effective February 29, 2012.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of February 29,
2012.

ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA 1601
Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-
1137; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on October 5, 2011 (76
FR 61638). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:

Based on in-service experience, the System Safety Analyses for
the Flight Controls have been reviewed and their conclusions have
been accepted during the latest Candidate Maintenance Coordination
Committee meeting.
This review resulted in reduced inspection intervals,
specifically for the flight controls tab-to-actuator linkage CMR
repetitive inspections, which have been identified as mandatory
actions for continued airworthiness.
Failure of these components or their constituent parts could
lead to reduced control of the aeroplane.
Consistent with the [European Aviation Safety Agency] EASA
policy to require compliance with any new and reduced airworthiness
limitations by taking AD action and for the reasons described above,
this EASA AD requires the accomplishment of the reduced-interval
repetitive inspections and, depending on findings, related
corrective action(s). In addition, this [EASA] AD requires the
implementation of the affected reduced inspection intervals and
associated corrective actions into the operator's approved
maintenance programme.

You may obtain further information by examining the MCAI in the AD
docket.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (76 FR 61638, October 5,
2011) or on the determination of the cost to the public.

Conclusion

We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (76 FR 61638, October 5, 2011) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (76 FR 61638, October 5, 2011).

Costs of Compliance

We estimate that this AD will affect 63 products of U.S. registry.
We also estimate that it will take about 1 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Based on these figures, we estimate the cost of
this AD to the U.S. operators to be $5,355, or $85 per product.

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.
We are 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

We determined that 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 this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not affect intrastate aviation in Alaska; and
4. 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. We prepared a regulatory evaluation
of the estimated costs to comply with this AD and placed it in the AD
docket.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov;
or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM (76 FR 61638, October 5,
2011), the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

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 AD: