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PROPOSED AD STEMME AG: Docket No. FAA-2021-0716; Project Identifier 2019-CE-023-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    October 12, 2021.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to Stemme AG  Model Stemme S  12 gliders, all  serial
    numbers, certificated in any category.

(d) SUBJECT

    Joint  Aircraft  System  Component  (JASC)  Code  3414,  Airspeed/Mach
    Indicator.

(e) UNSAFE CONDITION

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI) issued by the aviation authority of another country to identify
    and  correct an  unsafe condition  on  an  aviation product.  The MCAI
    describes the  unsafe condition  as an  airspeed indicator  (ASI) with
    speed markings  inconsistent with  the approved  and published  values
    (beginning of the white and green arc). The FAA is issuing this AD  to
    prevent   erroneous   information  being   provided   to  the   pilot,
    particularly  at  the  lower   speed  operation  limits.  The   unsafe
    condition, if not  addressed, could result  in reduced control  of the
    glider.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

(1) Within 30 days after the effective date of this AD,  inspect  ASI part
    number (P/N) IF-W230  or  IF-W190 for incorrect markings in accordance
    with the table in the Appendix, "2.3. Airspeed Indicator Markings," of
    Stemme Service Bulletin No. P062-980027,  Revision 00,  dated December
    17, 2018 (the SB).  If  an  ASI marking is incorrect,  before  further
    flight, perform one of the following:

(i) Replace the ASI by following the Actions, Action 2, of the SB; or

(ii) Amend the existing aircraft flight manual (AFM)  for  your  glider by
     inserting  the  Appendix,  temporary  page  2-3  SB,  "2.3.  Airspeed
     Indicator Markings," of  the SB. Within  3 months after  amending the
     AFM, replace the ASI  by following the Actions,  Action 2, of the  SB
     and remove temporary page 2-3 SB, "2.3. Airspeed Indicator Markings,"
     from the AFM.

(2) As of the effective date of this AD, do not install ASI P/N IF-W230 or
    IF-W190 on any glider unless it has passed  the inspection required by
    this AD.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, 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 manager  of the
    certification  office,  send  it  to  the  attention  of  the   person
    identified   in   Related   Information   or   email:    9-AVS-AIR-730
    -AMOC@faa.gov.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(i) RELATED INFORMATION

(1) For more information about this AD,  contact Jim Rutherford,  Aviation
    Safety Engineer,  General Aviation & Rotorcraft Section, International
    Validation Branch,  FAA,  901 Locust, Room 301, Kansas City, MO 64106;
    phone: (816) 329-4165; fax: (816) 329-4090; email: jim.rutherford@faa.
    gov.

(2) Refer to  European Union Aviation Safety Agency  (EASA)  AD 2019-0082,
    dated April 12, 2019,  for more information.  You may examine the EASA
    AD in the AD docket at https://www.regulations.gov  by  searching  for
    and locating it in Docket No. FAA-2021-0716.

(3) For service information  identified  in  this  AD,  contact STEMME AG,
    Flugplatzstrasse F2, Nr. 6-7, D-15344 Strausberg,  Germany; phone: +49
    (0) 3341 3612-0, fax +49 (0) 3341 3612-30; email airworthiness@stemme.
    de; website: https://www.stemme.com. You may view this referenced ser-
    vice information at the FAA,  Airworthiness  Products  Section, Opera-
    tional Safety Branch, 901 Locust, Kansas City, MO 64106.  For informa-
    tion on the availability of this material at the FAA,  call (816) 329-
    4148.

Issued on August 20, 2021. Lance T. Gant, Director, Compliance & Airworth-
iness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by  October 12,
2021.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0716; Project Identifier 2019-CE-023-AD]
RIN 2120-AA64

Airworthiness Directives; Stemme AG Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Stemme AG Model Stemme S 12 gliders. This proposed AD was
prompted by mandatory continuing airworthiness information (MCAI)
issued by the aviation authority of another country to identify and
correct an unsafe condition on an aviation product. The MCAI describes
the unsafe condition as an airspeed indicator (ASI) with speed markings
inconsistent with the approved and published values. This proposed AD
would require inspecting the ASI markings and, depending on findings,
either replacing the ASI or amending the existing aircraft flight
manual (AFM) until the ASI is replaced. The FAA is proposing this AD to
address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by October 12,
2021.

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 https://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 STEMME AG,
Flugplatzstrasse F2, Nr. 6-7, D-15344 Strausberg, Germany; phone: +49
(0) 3341 3612-0, fax: +49 (0) 3341 3612-30; email:
airworthiness@stemme.de; website: https://www.stemme.com. You may view
this service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For
information on the availability of this material at the FAA, call (816)
329-4148.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0716; 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 MCAI,
any comments received, and other information. The street address for
Docket Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aviation Safety
Engineer, General Aviation & Rotorcraft Section, International
Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO 64106;
phone: (816) 329-4165; fax: (816) 329-4090; email:
jim.rutherford@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include "Docket No. FAA-2021-0716; Project Identifier
2019-CE-023-AD" at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.

Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as "PROPIN." The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Jim
Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft
Section, International Validation Branch, FAA, 901 Locust, Room 301,
Kansas City, MO 64106. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.

Background

The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0082, dated April 12, 2019 (referred to after this as
"the MCAI"), to address an unsafe condition on Stemme AG Model Stemme
S 12 gliders. The MCAI states:

During a production inspection of a new powered sailplane, an
ASI was found with speed markings inconsistent with the approved and
published values (begin[ning] of the white and green arc).
Subsequent investigation of the production records for delivered
Stemme S 12 powered sailplanes does not exclude that a similar, non-
conforming ASI was installed during production.

This condition, if not corrected, could lead to erroneous
information being provided to the pilot, particularly at the lower
speed operation limits, possibly resulting in reduced control of the
powered sailplane.

To address this unsafe condition, Stemme AG issued the SB
[service bulletin] to provide inspections instructions.

For the reason described above, this [EASA] AD requires a one-
time inspection of the markings of the affected part and, depending
on findings, amending the Aircraft Flight Manual (AFM) and replacing
the affected part. This [EASA] AD also prohibits installation of
affected parts.

You may examine the MCAI in the AD docket at https://www.regulations.gov
by searching for and locating Docket No. FAA-2021-0716.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Stemme Service Bulletin No. P062-980027, Revision
00, dated December 17, 2018. The service information specifies checking
the ASI markings and provides illustrations of correct markings. The
service information specifies the procedure to replace an affected ASI
with an ASI with correct markings. The service information also
includes a temporary page to insert into the AFM until the ASI is
replaced. 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 ADDRESSES.

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
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI and
service information referenced above. The FAA is issuing this NPRM
after determining the unsafe condition described previously is likely
to exist or develop on other products of the same type design.

Proposed AD Requirements in This NPRM


This proposed AD would require a one-time inspection of the ASI
markings and, depending on findings, either replacing the ASI before
further flight or amending the existing AFM until the ASI is replaced
within 3 months.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 20 gliders of U.S. registry. The FAA estimates that it would
take about 0.5 work-hour per glider to comply with the inspection
requirements of this AD. The average labor rate is $85 per work-hour.

Based on these figures, the FAA estimates the cost of this AD on
U.S. operators to be $850 or $42.50 per glider.

The FAA estimates that amending the AFM to insert and then remove
the temporary page as a result of the inspection would take about 1
work-hour per glider for a total cost of $85 per glider. The FAA
estimates that replacing the ASI would take about 3.5 work-hours and
require parts costing $603, for a total cost of $900.50 per glider. The
FAA has no way of determining the number of gliders that may need these
actions.

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected operators.

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

The FAA 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) Would not affect intrastate aviation in Alaska, and

(3) Would 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

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: