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2018-03-16 STEMME AG: Amendment 39-19189; Docket No. FAA-2017-0952; Product Identifier 2017-CE-028-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective March 20, 2018.

(b) AFFECTED ADS

    This AD replaces AD 2017-10-11,  Amendment 39-18885  (82 FR 24239, May
    26, 2017) ("AD 2017-10-11").

(c) APPLICABILITY

    This AD applies to Stemme AG Model Stemme S10-VT gliders (type certif-
    icate previously held by Stemme GmbH & Co. KG), all serial numbers and
    Stemme AG Model Stemme S 12 gliders, all serial numbers, that are:

(1) equipped with a front gearbox,  part number (P/N) 11AG,  with a serial
    number listed in table 1 to paragraph (c) of this AD; and

(2) are certificated in any category.
    ______________________________________________________________________
    TABLE 1 TO PARAGRAPH (C) OF THIS AD –AFFECTED P/N 11AG (FRONT GEARBOX)
                                         S/NS                             
    ______________________________________________________________________
    80058/0814     80059/0915     80060/0915     80061/1115     80062/1215
    80063/0116     80064/0416     80065/0616     80066/0716     80067/0916
    80068/1016     80069/0117     80070/0217     80071/0217
    ______________________________________________________________________

Note 1 to paragraph (c) of this AD:  Page 2 of Stemme AG  Service Bulletin
No. P062-980010,  dated April 21, 2017,  provides a pictorial of where the
serial number of the affected gearboxes are located.

(d) SUBJECT

    Air Transport Association of America (ATA) Code 61: Propellers/Propul-
    sors.

(e) REASON

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI) issued by the aviation authority of another country to identify
    and  address an  unsafe condition  on an  aviation product.  The  MCAI
    describes the unsafe condition as certain propeller front transmission
    gear wheels having insufficient material strength because of  improper
    heat treatment during manufacturing. We  are issuing this AD to  add a
    model glider to  the Applicability, paragraph  (c) of this  AD, and to
    prevent failure of the propeller front transmission gear wheels.  This
    failure  could  cause  loss  of  power  between  the  engine  and  the
    propeller, which could result in reduced control.

(f) ACTIONS AND COMPLIANCE

    Unless already done, do the following actions:

(1) For Model Stemme S10-VT gliders:  Before further flight after June 15,
    2017 (the effective date of AD 2017-10-11),  replace the front gearbox
    following  STEMME Procedural Specification Dok. Nr.:  P320-900060,  as
    specified in STEMME Service Bulletin Dok. Nr.: P062-980010, Issue: 01,
    both dated June 14, 2017.

(2) For Model Stemme S 12 gliders:  Before further flight  after March 20,
    2018 (the effective date of this AD) replace the front gearbox follow-
    ing STEMME Procedural Specification Dok. Nr.: P320-900060 as specified
    in STEMME Service Bulletin Dok. Nr.: P062-980010, Issue: 01 both dated
    June 14, 2017.

(3) As of March 20, 2018 (the effective date of this AD), do not install a
    front gear box listed in table 1 of paragraph (c) of this AD.

(4) The service information  for  this  AD allows the owner/operator to do
    certain  maintenance tasks.  Also, the  service information  specifies
    certain maintenance tasks be done by Stemme AG. However, for this  AD,
    we do not  allow the owner/operator  to do any  maintenance tasks; all
    maintenance tasks must be done by an appropriately certified  mechanic
    or maintenance shop.  In addition, we  do not require  any maintenance
    tasks be done specifically  by Stemme AG; any  appropriately certified
    mechanic or maintenance shop may do the tasks required by this AD.

(g) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Small Airplane
    Standards Branch, FAA, has the authority to approve AMOCs for this AD,
    if requested using the procedures found in 14 CFR 39.19. Send informa-
    tion to ATTN: Jim Rutherford, Aerospace Engineer, FAA,  Small Airplane
    Standards Branch,  901 Locust,  Room 301, Kansas City, Missouri 64106;
    telephone: (816) 329-4165; fax: (816) 329-4090; email: jim.rutherford@
    faa.gov.

(i) Before using any approved AMOC  on  any airplane  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.

(ii) AMOCs approved for AD 2017-10-11,  Amendment  39-18885  (82 FR 24239,
     May 26, 2017) are approved as AMOCs  for the corresponding provisions
     of this AD.

(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, Small  Airplane
    Standards Branch, FAA; or the European Aviation Safety Agency (EASA).

(h) RELATED INFORMATION

    Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2017-0072-
    E, dated April 26, 2017 and Stemme AG Service Bulletin No. P062-980010
    dated April 21, 2017,  for  related  information.  You may examine the
    MCAI on the Internet  at  http://www.regulations.gov  by searching for
    and  locating  Docket No.  https://www.regulations.gov/document?D=FAA-
    2017-0952-0002.

(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) STEMME Service Bulletin Dok. Nr.: P062-980010,  Issue: 01,  dated June
    14, 2017.

(ii) STEMME Procedural Specification Dok. Nr.: P320-900060, dated June 14,
     2017.

(3) For  Stemme AG service information  identified  in  this  AD,  contact
    STEMME AG,  Flugplatzstrasse F2, Nr. 6–7, D-15344 Strausberg, Germany;
    telephone: +49 (0) 3341 3612-0,  fax: +49 (0) 3341 3612-30;  Internet:
    https://www.stemme.com.

(4) You may view this service information at FAA,  Policy  and  Innovation
    Division, 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-2017-0639.

(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 February 5, 2018.  Melvin J. Johnson,
Deputy Director, Policy & Innovation Division, Aircraft Certification Ser-
vice.

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0952; Product Identifier 2017-CE-028-AD; Amendment
39-19189; AD 2018-03-16]
RIN 2120-AA64

Airworthiness Directives; Stemme AG Gliders

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

ACTION: Final rule.

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

SUMMARY: We are superseding Airworthiness Directive (AD) 2017-10-11 for
Stemme AG Model Stemme S10-VT gliders (type certificate previously held
by Stemme GmbH & Co. KG). This AD results from mandatory continuing
airworthiness information (MCAI) issued by an aviation authority of
another country to identify and address an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as certain
propeller front transmission gear wheels having insufficient material
strength because of improper heat treatment during manufacturing. We
are issuing this AD to require actions to address the unsafe condition
on these products and to add Stemme AG Model Stemme S 12 gliders to the
Applicability section.

DATES: This AD is effective March 20, 2018.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 20,
2018.

ADDRESSES: You may examine the AD docket on the internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2017-
0952; or in person at Docket Operations, U.S. Department of
Transportation, 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 STEMME AG,
Flugplatzstrasse F2, Nr. 6-7, D-15344 Strausberg, Germany; telephone:
+49 (0) 3341 3612-0, fax: +49 (0) 3341 3612-30; internet: https://www.
stemme.com. You may view this referenced service information at the
FAA, Policy and Innovation Division, 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-2017-0952.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer,
FAA, Small Airplane Standards Branch, 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 Stemme AG Model Stemme
S10-VT gliders (type certificate previously held by Stemme GmbH & Co.
KG) and all Stemme AG Model Stemme S 12 gliders equipped with a certain
front gearbox, part number 11AG. That NPRM was published in the Federal
Register on October 10, 2017 (82 FR 46938), and proposed to supersede
AD 2017-10-11, Amendment 39-18885 (82 FR 24239, May 26, 2017) (``AD
2017-10-11'').
Since we issued AD 2017-10-11, we have type certificated Stemme AG
Model Stemme S 12 gliders in the United States and have determined
those model gliders should also be included in the applicability of AD
2017-10-11. In addition, Stemme AG has issued new service information
with procedures for addressing the unsafe condition.

Comments

We gave the public the opportunity to participate in developing
this AD. The following presents the comment received on the proposal
and the FAA's response to the comment.

Request for Manufacturer To Be Responsible for All Associated Cost

Taylor Ray stated that the manufacturer should be responsible for
replacing the front gearbox on the affected gliders at no cost to the
owners/operators. We infer that the commenter is referring to the cost
for both parts and labor.
Taylor Ray stated that since the unsafe condition resulted from the
manufacturing process, the manufacturer should be responsible for
fixing the unsafe condition.
We neither agree nor disagree since the FAA does not get involved
in who pays for the cost of mitigating an unsafe condition. The primary
concern the FAA has when issuing an AD is addressing unsafe conditions
on various aircraft flying in the United States. While we provide
information related to the estimated labor and parts cost associated
with each AD, we do not control warranty coverage for owner/operators
of the affected aircraft nor can
we mandate the manufacturer to cover all associated costs. We have
contacted Stemme AG about this issue. The following is the response we
received: ``All costs will be paid by Stemme AG (parts + work) for
customers who are affected within the one-year warranty. Customers who
are out of the one-year warranty will receive parts for free, but
unfortunately, they have to pay for the necessary work (approx. 10
working hours).'' Based on this response from Stemme AG, we revised the
Cost of Compliance section in this AD. We changed the number of
estimated work-hours per product to replace the front gearbox from 19
to 10, updated the total cost on U.S. operators and cost per product
based on this change, and added standard warranty information.

Conclusion

We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this AD as proposed except for changes stated above. We have determined
that these 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 Service Information Under 1 CFR Part 51

Stemme AG has issued STEMME Service Bulletin Dok. Nr.: P062-980010,
Issue: 01, dated June 14, 2017, and STEMME Procedural Specification
Dok. Nr.: P320-900060, dated June 14, 2017. In combination, the service
information describes procedures for replacing the front gearbox. 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.

Differences Between This AD and the Service Information

The service information for this AD allows the owner/operator to do
certain maintenance tasks. Also, the service information specifies
certain maintenance tasks be done by Stemme AG. However, for this AD,
we do not allow the owner/operator to do any maintenance tasks; all
maintenance tasks must be done by an appropriately certified mechanic
or maintenance shop. In addition, we do not require any maintenance
tasks be done specifically by Stemme AG; any appropriately certified
mechanic or maintenance shop may do the tasks required by this AD.

Costs of Compliance

According to the U.S. registry, we have a total of 51 of both
glider types registered, but there are still only 14 serial numbers of
the part number 11AG front gearbox. Therefore, the most gliders that
will be affected remains 14. According to Stemme AG, there are a total
of 4 of the affected front gearboxes on both glider types of U.S.
registry (2 for each model).
It will take an estimated 10 work-hours per product to comply with
the basic requirements of this AD. The average labor rate is $85 per
work-hour. Required parts will cost about $2,000 per product.
Based on these figures, if we consider the costs for all 14
affected gearboxes, then we estimate the cost of this AD on U.S.
operators to be $39,990, or $2,850 per product.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

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 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 small airplanes, gliders,
balloons, airships, domestic business jet transport airplanes, and
associated appliances to the Director of the Policy and Innovation
Division.

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-
0952; or in person at Docket Operations 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 Docket Operations (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 removing Amendment 39-18885 (82 FR
24239, May 26, 2017), and adding the following new AD: