
[Federal Register Volume 84, Number 46 (Friday, March 8, 2019)]
[Proposed Rules]
[Pages 8482-8485]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-04144]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0117; Product Identifier 2018-NM-169-AD]
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), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for all 
328 Support Services GmbH Model 328-100 airplanes. This proposed AD was 
prompted by a report indicating that undetected cracks may develop at 
the roll spoiler bearing arms. This proposed AD would require a one-
time non-destructive test (NDT) inspection for cracks in the roll 
spoiler bearing arms and, if necessary, corrective actions. We are 
proposing this AD to address the unsafe condition on these products.

[[Page 8483]]


DATES: We must receive comments on this proposed AD by April 22, 2019.

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 http://www.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.
    For service information identified in this NPRM, 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. You may view this service information at the FAA, 
Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 206-
231-3195.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0117; 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 regulatory evaluation, any comments received, and other 
information. The street address for Docket Operations (phone: 800-647-
5527) is in the ADDRESSES section. Comments will be available in the AD 
docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
International Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3228.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-2019-0117; 
Product Identifier 2018-NM-169-AD'' at the beginning of your comments. 
We specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this NPRM. We will consider all 
comments received by the closing date and may amend this NPRM because 
of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this NPRM.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2018-0254, dated November 23, 2018 (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 328-100 airplanes. The MCAI states:

    Dornier 328 Maintenance Review Board Report provides 
instructions for a detailed inspection for the roll spoilers, 
including the bearing arms, by eddy current [EC] method. It was 
reported that whilst performing Maintenance Planning Document Task 
57-71-03-02-01, referring to Non-Destructive Test (NDT) Manual task 
57-71-03-318-000-AA0, the stacking of 6 parts at the bearing arm No. 
3 prevents detection of cracks with the given EC test settings. The 
NDT results are distorted by geometric features such as part edges 
and fastener installations. Furthermore, the access to certain areas 
is limited for the suggested NDT probe for geometrical reasons. The 
result of the technical investigation identified that undetected 
cracks may develop at the roll spoiler bearing arms, leading to a 
broken (disconnected) bearing arm No. 3, where the actuator is 
connected.
    This condition, if not detected and corrected, could lead to a 
roll spoiler becoming unresponsive to flight crew control inputs, 
possibly resulting in loss of control of the aeroplane.
    To address this potential unsafe condition, 328 SSG published 
the ASB [328 Support Services Alert Service Bulletin ASB-328-57-043, 
dated September 21, 2018] to provide appropriate inspection 
instructions.
    For the reasons described above, this [EASA] AD requires a one-
time NDT inspection of the affected parts and, depending on 
findings, accomplishment of applicable corrective action(s) [repair 
of cracked parts].

    You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0117.

Related Service Information Under 1 CFR Part 51

    328 Support Services has issued Alert Service Bulletin ASB-328-57-
043, dated September 21, 2018. This service information describes 
procedures for a one-time NDT inspection for cracks in the roll spoiler 
bearing arms. 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 the 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 our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all the relevant information and determined the unsafe 
condition described previously is likely to exist or develop on other 
products of the same type design.

Proposed Requirements of This NPRM

    This proposed AD would require accomplishing the actions specified 
in the service information described previously.

Differences Between This Proposed AD and the MCAI or Service 
Information

    Although the MCAI and 328 Support Services Alert Service Bulletin 
ASB-328-57-043, dated September 21, 2018, specify to submit certain 
information to the manufacturer, this AD does not include that 
requirement.

Costs of Compliance

    We estimate that this proposed AD affects 27 airplanes of U.S. 
registry. We estimate the following costs to comply with this proposed 
AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
8 work-hours x $85 per hour = $680...........................              $0             $680          $18,360
----------------------------------------------------------------------------------------------------------------


[[Page 8484]]

    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this proposed 
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.
    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.
    This proposed AD is issued in accordance with authority delegated 
by the Executive Director, Aircraft Certification Service, as 
authorized by FAA Order 8000.51C. In accordance with that order, 
issuance of ADs is normally a function of the Compliance and 
Airworthiness Division, but during this transition period, the 
Executive Director has delegated the authority to issue ADs applicable 
to transport category airplanes to the Director of the System Oversight 
Division.

Regulatory Findings

    We 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. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    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.

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 (AD):

328 Support Services GmbH (Type Certificate Previously Held by 
AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt 
GmbH): Docket No. FAA-2019-0117; Product Identifier 2018-NM-169-AD.

(a) Comments Due Date

    We must receive comments by April 22, 2019.

(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 airplanes, certificated in any 
category, all serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

(e) Reason

    This AD was prompted by a report indicating that undetected 
cracks may develop at the roll spoiler bearing arms. We are issuing 
this AD to address cracks at the roll spoiler bearing arms, which, 
if not detected and corrected, could lead to a roll spoiler becoming 
unresponsive to flight crew control inputs, possibly resulting in 
loss of control of the airplane.

(f) Compliance

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

(g) Definition of Affected Parts

    For the purposes of this AD, an affected part is the bearing arm 
of roll spoilers having part number (P/N) 001B577A1200000, 
001B577A1200001, 001B577A1200002, 001B577A1200003, 001B577A1200004, 
or 001B577A1200005.

(h) Inspection

    Within the compliance time specified in Figure 1 to paragraph 
(h) of this AD, as applicable, do a non-destructive test (NDT) 
inspection of each affected part in accordance with the 
Accomplishment Instructions of 328 Support Services Alert Service 
Bulletin ASB-328-57-043, dated September 21, 2018. The flight cycles 
(FC) specified in Figure 1 to paragraph (h) of this AD are the FC 
accumulated on the airplane since first flight of the airplane, 
unless otherwise specified.
[GRAPHIC] [TIFF OMITTED] TP08MR19.000


[[Page 8485]]



(i) Corrective Action

    If any crack is found during any inspection required by 
paragraph (h) of this AD: Before further flight, obtain corrective 
actions approved by the Manager, International Section, Transport 
Standards Branch, FAA; or the European Aviation Safety Agency 
(EASA); or 328 Support Services GmbH's EASA Design Organization 
Approval (DOA); and accomplish the corrective actions within the 
compliance time specified therein. If approved by the DOA, the 
approval must include the DOA-authorized signature.

(j) No Reporting Requirement

    Although 328 Support Services Alert Service Bulletin ASB-328-57-
043, dated September 21, 2018, specifies to submit certain 
information to the manufacturer, this AD does not include that 
requirement.

(k) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards 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 International Section, send it to the attention of 
the person identified in paragraph (l)(2) 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 principal 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 corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or EASA; or 328 Support 
Services GmbH's EASA DOA. If approved by the DOA, the approval must 
include the DOA-authorized signature.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2018-0254, dated November 23, 
2018, for related information. This MCAI may be found in the AD 
docket on the internet at http://www.regulations.gov by searching 
for and locating Docket No. FAA-2019-0117.
    (2) For more information about this AD, contact Todd Thompson, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3228.
    (3) 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. You may view this service information at 
the FAA, Transport Standards Branch, 2200 South 216th St., Des 
Moines, WA. For information on the availability of this material at 
the FAA, call 206-231-3195.

    Issued in Des Moines, Washington, on February 28, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2019-04144 Filed 3-7-19; 8:45 am]
BILLING CODE 4910-13-P


