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2023-05-03 ALEXANDER SCHLEICHER GMBH & CO. SEGELFLUGZEUGBAU: Amendment 39-22372; Docket No. FAA-2022-1303; Project Identifier MCAI-2022-01001-G.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective April 18, 2023.

(b) AFFECTED ADS

    This AD replaces AD 2022-14-14,  Amendment 39-22119 (87 FR 43403, July
    21, 2022) (AD 2022-14-14).

(c) APPLICABILITY

    This  AD  applies  to Alexander Schleicher GmbH & Co. Segelflugzeugbau
    Model ASW-15 and ASW-15B gliders, all serial numbers, certificated  in
    any category, equipped with wooden wing root ribs.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 5712, Wing, Rib/Bulkhead.

(e) UNSAFE CONDITION

    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 wing root rib damage.  The FAA
    is issuing this AD to detect and correct damaged root ribs. The unsafe
    condition,  if  not  addressed,  could  result  in  reduced structural
    integrity of the wing assembly, which could lead to loss of control of
    the glider.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIRED ACTIONS

(1) For Model ASW-15 gliders: Within 30 days after August 25, 2022 (effec-
    tive date of AD 2022-14-14), and thereafter at intervals not to exceed
    12 months, inspect all wing root ribs (4 places) for cracks, looseness
    and damage,  in  accordance  with  the  Action  section  in  Alexander
    Schleicher GmbH & Co. Segelflugzeugbau ASW 15  Maintenance Instruction
    G, Issue 1, dated June 28, 2021.  If there is a crack in any root rib,
    a loose rib or lift pin bushing, or any damage, before further flight,
    replace the root rib in accordance  with Action paragraph (B) in Alex-
    ander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Technical Note 29,
    dated  June 28, 2021,  and  steps 1 through 7  in Alexander Schleicher
    GmbH & Co. Segelflugzeugbau ASW 15 Repair instruction exchange of wing
    root ribs according to TN 29, dated June 28, 2021; or Action paragraph
    (C) in Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Techni-
    cal Note 29, Issue II,  dated  May 4, 2022,  and  steps 1 through 7 in
    Alexander Schleicher GmbH & Co. Segelflugzeugbau  ASW  15  Repai r in-
    struction exchange of wing root ribs  according  to  TN 29, dated June
    28, 2021.

(2) For Model ASW-15B gliders:  Within 30 days after the effective date of
    this AD  and thereafter at intervals not to exceed 12 months,  inspect
    all wing root ribs (4 places) for cracks,  looseness,  and  damage, in
    accordance with the Action section  in Alexander Schleicher GmbH & Co.
    Segelflugzeugbau ASW 15 Maintenance Instruction G, Issue 1, dated June
    28, 2021. If there is a crack in any root rib, a loose rib or lift pin
    bushing, or any damage, before further flight, replace the root rib in
    accordance with Action  paragraph (C)  in  Alexander Schleicher GmbH &
    Co. Segelflugzeugbau ASW 15 Technical Note 29, Issue II,  dated May 4,
    2022,  and  steps 1 through 7 in Alexander Schleicher GmbH & Co. Segel
    flugzeugbau ASW 15 Repair  instruction  exchange  of  wing  root  ribs
    according to TN 29, dated June 28, 2021.

(3) For  Model ASW-15 and ASW-15B gliders:  Replacing  all  four wing root
    ribs with new ribs is terminating action  for  the  repetitive inspec-
    tions required by this AD.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

    The Manager, International Validation Branch,  FAA,  has the authority
    to approve AMOCs for this AD,  if requested using the procedures found
    in Sec. 39.19.  In  accordance  with Sec. 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
    International Validation Branch,  mail it to the address identified in
    paragraph (i)(2) of this AD  or  email to: 9-AVS-AIR-730-AMOC@faa.gov.
    If mailing information, also submit information by email. Before using
    any approved AMOC,  notify  your  appropriate principal inspector,  or
    lacking a principal inspector,  the manager of the local flight stand-
    ards district office/certificate holding district office.

(i) ADDITIONAL INFORMATION

(1) Refer  to  European Union Aviation Safety Agency  (EASA) AD 2022-0146,
    dated  July 11, 2022,  for  related  information.  This EASA AD may be
    found in the AD docket  at regulations.gov  under Docket No. FAA-2022-
    1303.

(2) 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; email: jim.rutherford@faa.gov.

(j) 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 the AD specifies otherwise.

(3) The following  service information  was approved  for IBR on April 18,
    2023.

(i) Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Technical Note
    29, Issue II, dated May 4, 2022.

(ii) [Reserved]

(4) The following  service information was approved  for IBR on August 25,
    2022 (87 FR 43403, July 21, 2022).

(i) Alexander Schleicher GmbH & Co. Segelflugzeugbau  ASW  15  Maintenance
    Instruction G, Issue 1, dated June 28, 2021.

(ii) Alexander Schleicher GmbH & Co. Segelflugzeugbau  ASW  15  Repair in-
     struction exchange of wing root ribs according to TN 29,  dated  June
     28, 2021.

(iii) Alexander Schleicher GmbH & Co. Segelflugzeugbau  ASW  15  Technical
      Note 29, dated June 28, 2021.

(5) For service information  identified  in  this  AD,  contact  Alexander
    Schleicher GmbH & Co.  Segelflugzeugbau,  Alexander-Schleicher-Str. 1,
    Poppenhausen, Germany D-36163; phone: +49 (0) 06658 89-0; email: info@
    alexander-schleicher.de; website: alexander-schleicher.de.

(6) You may view this service information at the FAA,  Airworthiness Prod-
    ucts Section, Operational Safety Branch,  901 Locust,  Kansas City, MO
    64106. For information on the availability of this material at the FAA
    call (817) 222-5110.

(7) You may view  this service information  that is incorporated by refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information on the availability of this material  at NARA,  email: fr.
    inspection@nara.gov,  or go to: www.archives.gov/federal-register/cfr/
    ibr-locations.html.

Issued on March 5, 2023.  Christina Underwood, Acting Director, Compliance
& Airworthiness Division, Aircraft Certification Service.

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;
email: jim.rutherford@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39


[Docket No. FAA-2022-1303; Project Identifier MCAI-2022-01001-G;
Amendment 39-22372; AD 2023-05-03]
RIN 2120-AA64

Airworthiness Directives; Alexander Schleicher GmbH & Co.
Segelflugzeugbau Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2022-14-
14, which applied to all Alexander Schleicher GmbH & Co.
Segelflugzeugbau Model ASW-15 gliders. AD 2022-14-14 required
repetitively inspecting the wing root ribs for cracks, looseness, and
damage and replacing any root rib with a crack, a loose rib or lift pin
bushing, or any damage. Since the FAA issued AD 2022-14-14, the
European Union Aviation Safety Agency (EASA) superseded its mandatory
continuing airworthiness information (MCAI) to add all Model ASW-15B
gliders to the applicability. This AD is prompted by MCAI originated by
an aviation authority of another country to identify and correct an
unsafe condition on an aviation product. This AD retains the
requirements from AD 2022-14-14 of repetitively inspecting the wing
root ribs for cracks, looseness, and damage and replacing any root rib
with a crack, a loose rib or lift pin bushing or any damage; and
revises the applicability by adding Model ASW-15B gliders and
specifying that this AD applies to all Model ASW-15 and ASW-15B gliders
equipped with wooden wing root ribs. The FAA is issuing this AD to
address the unsafe condition on these products.

DATES: This AD is effective April 18, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 18,
2023.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of August
25, 2022 (87 FR 43403, July 21, 2022).

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1303; 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 final rule, any comments received, the MCAI, and
other information. The address for Docket Operations is U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For service information identified in this final rule,
contact Alexander Schleicher GmbH & Co. Segelflugzeugbau, Alexander-
Schleicher-Str. 1, Poppenhausen, Germany D-36163; phone: +49 (0) 06658
89-0; email: info@alexander-schleicher.de; website: alexander-
schleicher.de.
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 (817) 222-5110. It is also available at
regulations.gov under Docket No. FAA-2022-1303.

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; email: jim.rutherford@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2022-14-14, Amendment 39-22119 (87 FR
43403, July 21, 2022) (AD 2022-14-14). AD 2022-14-14 applied to all
serial-numbered Alexander Schleicher GmbH & Co. Segelflugzeugbau Model
ASW-15 gliders. AD 2022-14-14 required repetitively inspecting the wing
root ribs for cracks, looseness, and damage and replacing any root rib
with a crack, a loose rib or lift pin bushing, or any damage. The FAA
issued AD 2022-14-14 to detect and correct damaged root ribs.
The NPRM published in the Federal Register on October 26, 2022 (87
FR 64734; corrected November 10, 2022 (87 FR 67837)). The NPRM was
prompted by EASA AD 2022-0146, dated July 11, 2022 (EASA AD 2022-0146)
(referred to after this as ``the MCAI''), issued by EASA, which is the
Technical Agent for the Member States of the European Union. The MCAI
states that wing root rib damage can also affect Model ASW-15B gliders,
and the Model ASW-15B as well as the ASW-15 gliders require
repetitively inspecting the wing root ribs and replacing any damaged
wing root ribs. You may examine the MCAI in the AD docket at
regulations.gov under Docket No. FAA-2022-1303.
In the NPRM, the FAA proposed to retain the requirements from AD
2022-14-14 of repetitively inspecting the wing root ribs for cracks,
looseness, and damage and replacing any root rib with a crack, a loose
rib or lift pin bushing, or any damage; and add the Model ASW-15B
gliders to the applicability.

Discussion of Final Airworthiness Directive

Comments

The FAA received comments from three individual commenters. The
following presents the comments received on the NPRM and the FAA's
response to each comment.

Request Regarding Applicability

Three individual commenters requested that the FAA change the
applicability of the proposed AD to specify that only Model ASW-15 and
ASW-15B gliders equipped with wooden wing root ribs would be affected. The
commenters stated that EASA AD 2022-0146 and Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Technical Note 29, Issue II, dated May 4, 2022 (TN 29,
Issue II), are for all models and serial numbers of ASW 15 gliders built with
wooden wing root ribs and that in the proposed AD the FAA did not
specify that only gliders equipped with wooden wing root ribs would be
affected.
The FAA agrees. The FAA revised paragraph (c), Applicability, of
this AD to specify Alexander Schleicher GmbH & Co. Segelflugzeugbau
Model ASW-15 and ASW-15B gliders, all serial numbers, certificated in
any category, equipped with wooden wing root ribs.

Request Regarding On-Condition Costs

An individual commenter requested that the FAA increase the
proposed work-hour estimates in the NPRM for replacing all wing root
ribs. The individual stated that the estimate of 8 work-hours to
replace all wing root ribs is a significant underestimate.
The FAA agrees. The FAA researched the work-hour estimate for
replacing all four wing root ribs and has since determined that it
should be an estimate of 55 work-hours. Based on this information, the
FAA revised the on-condition cost estimate in this final rule to
include 55 work-hours for the replacement of all four wing root ribs.

Conclusion

These products have been approved by the aviation authority of
another country and are 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 referenced above. The FAA reviewed the relevant data,
considered the comments received, and determined that air safety
requires adopting this AD as proposed. Accordingly, the FAA is issuing
this AD to address the unsafe condition on these products. Except for
any changes described previously, this AD is adopted as proposed in the
NPRM.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Alexander Schleicher GmbH & Co. Segelflugzeugbau
ASW 15 Technical Note 29, Issue II, dated May 4, 2022 (TN 29, Issue
II). This service information specifies replacement of wooden wing root
ribs with new ribs.
This AD also requires Alexander Schleicher GmbH & Co.
Segelflugzeugbau ASW 15 Technical Note 29, dated June 28, 2021;
Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Repair
instruction exchange of wing root ribs according to TN 29, dated June
28, 2021; and Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15
Maintenance Instruction G, Issue 1, dated June 28, 2021, which the
Director of the Federal Register approved for incorporation by
reference as of August 25, 2022 (87 FR 43403, July 21, 2022).
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.

Differences Between This AD and the Service Information

TN 29, Issue II, specifies the exchange of page 22A and page 27A of
the Flight and Operations Manual for the Model ASW-15 and ASW-15B
gliders, respectively, with a new version of those pages and then
specifies documenting this change on page 3, Amendments, of the
respective manual, and the MCAI and this AD do not.

Costs of Compliance

The FAA estimates that this AD affects 29 gliders of U.S. registry.
The FAA estimates the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Inspection of root ribs 1 work-hour x $85 per hour = $85 Not Applicable $85 per inspection cycle $2,465 per inspection cycle

The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
inspection. The agency has no data to determine the number of gliders
that might need these replacements:

On-Condition Costs

Action
Labor cost
Parts cost
Cost per product
Replace all four root ribs 55 work-hours x $85 per hour = $4,675
$1,000
$5,675

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 has 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 that this AD:

(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) 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 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:

a. Removing Airworthiness Directive AD 2022-14-14, Amendment 39-22119
(87 FR 43403, July 21, 2022); and

b. Adding the following new airworthiness directive: