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2017-13-06 DG FLUGZEUGBAU GMBH:
Amendment 39-18936; Docket No. FAA-2017-0343; Directorate Identifier 2017-CE-005-AD.

(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective July 31, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to  DG Flugzeugbau GmbH   Models  DG-400,  DG-500M,
    DG-500MB, DG-800A, and DG-800B gliders, all serial numbers, that:

(1) Have textile fabric covered fuel hoses installed in the fuselage; and

(2) are certificated in any category.

Note 1 to paragraph (c) of this AD:  Metal  fabric covered  fuel hoses in-
stalled in the engine area are not affected by this AD.

(d) SUBJECT

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

(e) REASON

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI)  originated  by an  aviation  authority of  another  country to
    identify and correct an unsafe  condition on an aviation product.  The
    MCAI  describes  the unsafe  condition  as a  manufacturing  defect in
    certain textile fabric covered fuel hoses, which could cause the  fuel
    hose to fail. We  are issuing this AD  to prevent failure of  the fuel
    hose, which could cause reduced  fuel supply and result in  partial or
    total loss of power.

(f) ACTIONS AND COMPLIANCE

    Unless already done, do the following actions:

(1) Within  the  next 30 days  after July 31, 2017  (the effective date of
    this AD), inspect all textile fabric covered fuel hoses located in the
    fuselage  following  Instructions 1.  of DG Flugzeugbau GmbH Technical
    note (TN) No. 800-44, 500-10, DG-SS-02, dated November 9, 2016.

Note 2 to paragraph (f)(1) through (6) of this AD:  DG Flugzeugbau GmbH TN
No. 800-44, DG Flugzeugbau GmbH TN No. 500-10,  and DG Flugzeugbau GmbH TN
No. DG-SS-02, are all dated November 9, 2016, and co-published as one doc-
ument.

(2) If any kinking  or  wet fabric covering is found during the inspection
    required in paragraph (f)(1) of this AD, within the next 14 days after
    the inspection,  replace all textile fabric covered fuel hoses located
    in  the  fuselage  following Instructions 2. of DG Flugzeugbau GmbH TN
    No. 800-44, 500-10, DG-SS-02, dated November 9, 2016,  and DG-400 dia-
    gram 8, 6 TN DG-SS-02; DG-500M diagram 14, TN 500/10; DG-500MB diagram
    14,  TN 500/10;  DG-800A/LA diagram 11,  TN 800/44;  DG-800B Solo 2625
    diagram 11, TN 800/44;  DG-800B Solo 2625 diagram 11a, TN 800/44;  DG-
    800B Solo 2625 diagram 11b, TN 800/44; and DG-800B ab W.Nr. 8-155/from
    ser. no. 8-155 on, diagram 11d, TN 800/44, as applicable, all diagrams
    issued October 2016.

(3) If no kinking  or  wet fabric covering is found  during the inspection
    required  in  paragraph (f)(1) of this AD,  within  the next 12 months
    after July 31, 2017 (the effective date of this AD),  replace all tex-
    tile fabric covered fuel hoses located  in the fuselage  following the
    instructions and diagrams specified in paragraph (f)(2) of this AD.

(4) Within 12 months  after doing the replacements required  in  paragraph
    (f)(2) or (f)(3) of this AD,  as applicable,  and  repetitively there-
    after at intervals not to exceed 12 months,  inspect all fuel hoses in
    the fuselage for any signs of wear, fissures, kinks, lack of tight fit
    or leaks.  For this inspection,  the ignition switch must be turned on
    to run the electric fuel pump  to demonstrate  an operating fuel pres-
    sure.  Do this inspection following Instructions 4.  of DG Flugzeugbau
    GmbH TN No. 800-44, 500-10, DG-SS-02, dated November 9, 2016.

(5) If any signs of wear, fissures, kinks, lack of tight fit, or leaks are
    found during any inspection required  in paragraph (f)(4) of this  AD,
    replace  the  defective  fuel  hose  in  the  fuselage  following  the
    instructions and diagrams  specified in paragraph  (f)(2) of this  AD.
    Continue with  the repetitive  inspections as  specified in  paragraph
    (f)(4) of this AD.

(6) If no signs of wear, fissures, kinks, lack of tight fit,  or leaks are
    found during any inspection required  in paragraph (f)(4) of this  AD,
    at intervals not  to exceed 10  years, replace the  fuel hoses in  the
    fuselage with new fuel  hoses following the instructions  and diagrams
    specified in paragraph (f)(2) of this AD.

(g) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative  Methods  of  Compliance  (AMOCs):  The Manager, Standards
    Office,  FAA,  has the authority to approve AMOCs for this AD,  if re-
    quested using the procedures found in 14 CFR 39.19.  Send  information
    to  ATTN: Jim Rutherford,  Aerospace  Engineer,  FAA,  Small  Airplane
    Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106;  tele-
    phone: (816) 329-4165; fax: (816) 329-4090; email: jim.rutherford@faa.
    gov.  Before using  any approved AMOC  on any glider to which the AMOC
    applies,  notify your appropriate principal inspector (PI)  in the FAA
    Flight Standards District Office (FSDO),  or lacking a PI,  your local
    FSDO.

(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.

(h) RELATED INFORMATION

    Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 2016-0259
    dated December 21, 2016, for related information.  You may examine the
    MCAI on the  Internet  at  https://www.regulations.gov/document?D=FAA-
    2017-0343-0002.

(i) 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) DG-400 diagram 8, issued October 2016 TN DG-SS-02.

(ii) DG-500M diagram 14, issued October 2016 TN 500/10.

(iii) DG-500MB diagram 14, issued October 2016 TN 500/10.

(iv) DG-800A/LA diagram 11, issued October 2016 TN 800/44.

(v) DG-800B Solo 2625 diagram 11, issued October 2016 TN 800/44.

(vi) DG-800B Solo 2625 diagram 11a, issued October 2016 TN 800/44.

(vii) DG-800B Solo 2625 diagram 11b, issued October 2016 TN 800/44.

(viii) DG-800B ab W.Nr. 8-155/from ser. no. 8-155 on,  diagram 11d, issued
       October 2016 TN 800/44.

(ix) DG Flugzeugbau GmbH Technical note (TN) No. 800-44, 500-10, DG-SS-02,
     dated November 9, 2016.

Note 3 to paragraph (i)(2)(ix) of this AD: DG Flugzeugbau GmbH TN No. 800-
44, DG Flugzeugbau GmbH TN No. 500-10,  and DG Flugzeugbau GmbH TN No. DG-
SS-02, are all dated November 9, 2016, and co-published as one document.

(3) For  service information identified  in this AD,  DG Flugzeugbau GmbH,
    Otto-Lilienthal Weg 2,  D-76646 Bruchsal, Germany;  telephone: +49 (0)
    7251 3202-0;  email: info@dg-flugzeugbau.de;  Internet: http://www.dg-
    flugzeugbau.de/en/?noredirect=en_US.

(4) You may view  this service information  at  the  FAA,  Small  Airplane
    Directorate, 901 Locust, Kansas City, Missouri 64106.  For information
    on the availability of this material at the FAA,  call (816) 329-4148.
    In  addition,  you can access this service information on the Internet
    at http://www.regulations.gov by searching for and locating Docket No.
    FAA-2017-0343.

(5) You  may  view  this  service  information  that  is  incorporated  by
    reference at the National Archives and Records Administration  (NARA).
    For information on the availability of this material at NARA, call 202
    -741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-
    locations.html.

Issued in  Kansas City,  Missouri,  on  June 19, 2017.  Pat Mullen, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford,  Aerospace Engineer, FAA,
Small Airplane Directorate,  901 Locust,  Room 301,  Kansas City, Missouri
64106; telephone: (816) 329-4165;  fax: (816) 329-4090;  email: jim.ruther
ford@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39


[Docket No. FAA-2017-0343; Directorate Identifier 2017-CE-005-AD;
Amendment 39-18936; AD 2017-13-06]
RIN 2120-AA64

Airworthiness Directives; DG Flugzeugbau GmbH Gliders

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all DG
Flugzeugbau GmbH Models DG-400, DG-500M, DG-500MB, DG-800A, and DG-800B
gliders. This AD results from mandatory continuing airworthiness
information (MCAI) issued by an aviation authority of another country
to identify and correct an unsafe condition on an aviation product. The
MCAI describes the unsafe condition as a manufacturing defect in
certain textile fabric covered fuel hoses, which could cause the fuel
hose to fail. We are issuing this AD to require actions to address the
unsafe condition on these products.

DATES: This AD is effective July 31, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 31,
2017.

ADDRESSES: You may examine the AD docket on the Internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2017-
0343; or in person at Document Management Facility, 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 service information identified in this AD, contact DG
Flugzeugbau GmbH, Otto-Lilienthal Weg 2, D-76646 Bruchsal, Germany;
telephone: +49 (0)7251 3202-0; email: info@dg-flugzeugbau.de; Internet:
http://www.dg-flugzeugbau.de/en/?noredirect=en_US. You may view this
referenced service information at the FAA, Small Airplane Directorate,
901 Locust, Kansas City, Missouri 64106. For information on the
availability of this material at the FAA, call (816) 329-4148. It is
also available on the Internet at http://www.regulations.gov by
searching for Docket No. FAA-2017-0343.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email:
jim.rutherford@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to all DG Flugzeugbau GmbH
Models DG-400, DG-500M, DG-500MB, DG-800A, and DG-800B gliders. The
NPRM was published in the Federal Register on April 21, 2017 (82 FR
18722). The NPRM proposed to correct an unsafe condition for the
specified products and was based on mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country.
The MCAI states:

During service and annual inspection, DG found that some fuel
hoses with textile fabric covering, installed from the beginning of
the year 2015, had become weak or untight with time. The suspected
root cause for this premature degradation is a manufacturing defect
of a certain batch of fuel hoses.
This condition, if not detected and corrected, may lead to
kinking of the fuel hoses, possibly resulting in a reduced fuel
supply and consequent partial or total loss of available power.

To address this unsafe condition, DG-Flugzeugbau published
Technical Note TN 800-44, 500-10, DG-SS-02 providing inspection and
replacement instructions.
For the reason described above, this [EASA] AD requires
inspection and replacement of the affected fuel hoses.

The MCAI can be found in the AD docket on the Internet at https://www.regulations.gov/document?D=FAA-2017-0343-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

We reviewed the relevant data and determined that air safety and
the public interest require adopting this 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 for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

We reviewed DG Flugzeugbau GmbH Technical note No. 800-44, 500-10,
DG-SS-02, dated November 9, 2016, and co-published as one document; DG-
400 diagram 8, 6 TN DG-SS-02; DG-500M diagram 14, TN 500/10; DG-500MB
diagram 14, TN 500/10; DG-800A/LA diagram 11, TN 800/44; DG-800B Solo
2625 diagram 11, TN 800/44; DG-800B Solo 2625 diagram 11a, TN 800/44;
DG-800B Solo 2625 diagram 11b, TN 800/44; and DG-800B ab W.Nr. 8-155/
from ser. no. 8-155 on, diagram 11d, TN 800/44, all diagrams issued
October 2016. In combination, the service information describes
procedures for inspecting and replacing the fuel hoses on different
aircraft model variants covered by the applicability of this AD. 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 of this AD.

Costs of Compliance

We estimate that this AD will affect 59 products of U.S. registry.
We also estimate that it will take about 2 work-hours per product to
comply with each inspection required by this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the inspection cost of this AD
on U.S. operators to be $10,030, or $170 per product.
In addition, we estimate that each replacement action required by
this AD will take about 8 work-hours and require parts costing $500.
Based on these figures, we estimate the replacement cost of this AD on
U.S. operators to be $69,620, or $1,180 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),
(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.

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-2017-0343;
or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains the NPRM, the regulatory evaluation, any comments received,
and other information. The street address for the Docket 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: