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PROPOSED AD ALEXANDER SCHLEICHER GMBH & CO. SEGELFLUGZEUGBAU: ( c o r r e c t i o n ) Docket No. FAA-2022-1303; Project Identifier MCAI-2022-01001-G.
TDATA NOTE: Under  the  "(j) Material Incorporated by Reference"  heading,
            paragraph "(3)","November 30, 2022" should read "[DATE 35 DAYS
            AFTER PUBLICATION OF THE FINAL RULE]"
  
(a) COMMENTS DUE DATE

    The FAA must receive comments  on this airworthiness directive (AD) by
    December 12, 2022.

(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.

(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) ACTION

(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 No.
    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 No. 29, Issue II, dated May 4, 2022, and steps 1 through 7 in
    Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Repair instruc
    -tion 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 No. 29, Issue II, dated May
    4, 2022,  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.

(3) For Model ASW-15 and ASW-15B gliders:  Replacing  all  four  wing root
    ribs is terminating action  for the repetitive inspections 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 Director of the Federal Register  approved  the  following service
    information for incorporation by reference on [DATE 35 DAYS AFTER PUB-
    LICATION OF THE FINAL RULE].

(i) Alexander Schleicher GmbH & Co. Segelflugzeugbau ASW 15 Technical Note
    No. 29, Issue II dated May 4, 2022.

(ii) [Reserved]

(4) The Director of the Federal Register  approved  the  following service
    information for incorporation  by reference  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 No. 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 October 13, 2022.  Christina Underwood, Acting Director, Compli-
ance & Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this NPRM by December 12, 2022.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1303; Project Identifier MCAI-2022-01001-G]
RIN 2120-AA64

Airworthiness Directives; Alexander Schleicher GmbH & Co.
Segelflugzeugbau Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2022-14-14, which applies to all Alexander Schleicher GmbH & Co.
Segelflugzeugbau Model ASW-15 gliders. AD 2022-14-14 requires
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 proposed 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 proposed AD
would 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 would add the Model ASW-15B gliders to the
applicability. The FAA is proposing this AD to address the unsafe
condition on these products.

DATES: The FAA must receive comments on this NPRM by December 12, 2022.

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 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.
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 NPRM, the MCAI, any comments received, and other
information. The street address for Docket Operations is listed above.
Material Incorporated by Reference:
For service information identified in this NPRM, 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.

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:

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-2022-1303; Project Identifier
MCAI-2022-01001-G'' 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
the 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
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 FAA issued AD 2022-14-14, Amendment 39-22119 (87 FR 43403, July
21, 2022), (AD 2022-14-14), for all serial-numbered Alexander
Schleicher GmbH & Co. Segelflugzeugbau Model ASW-15 gliders. AD 2022-
14-14 was prompted by MCAI originated by EASA, which is the Technical
Agent for the Member States of the European Union. EASA issued EASA AD
2021-0187, dated August 9, 2021 (EASA AD 2021-0187), for all Alexander
Schleicher GmbH & Co. Segelflugzeugbau Model ASW 15 gliders to correct
an unsafe condition identified as wing root rib damage.
AD 2022-14-14 requires 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.

Actions Since AD 2022-14-14 Was Issued

Since the FAA issued AD 2022-14-14, Alexander Schleicher GmbH & Co.
Segelflugzeugbau determined that Model ASW-15B gliders can also be
affected by wing root rib damage. As a result, EASA superseded EASA AD
2021-0187, and issued EASA AD 2022-0146, dated July 11, 2022 (referred
to after this as ``the MCAI''). 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. The MCAI retains
the requirements of EASA AD 2021-0187 and expands the applicability to
include all Model ASW-15B gliders.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1303.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Alexander Schleicher GmbH & Co. Segelflugzeugbau
ASW 15 Technical Note No. 29, Issue II (TN No. 29, Issue II), dated May
4, 2022. This service information specifies replacement of root ribs.
This proposed AD would also require Alexander Schleicher GmbH & Co.
Segelflugzeugbau ASW 15 Technical Note No. 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.

FAA's Determination

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 and service information described above. The FAA is issuing
this NPRM after determining that the unsafe condition described
previously is likely to exist or develop on other products of these
same type designs.

Proposed AD Requirements in This NPRM


This proposed AD would retain all of the requirements of AD 2022-
14-14, would add Model ASW-15B gliders to the applicability, and would
provide the option of using the service material from AD 2022-14-14 or
the updated service material.

Differences Between This Proposed AD and the Service Information

TN No. 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 proposed AD do not.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 29 gliders of U.S. registry.
The FAA estimates the following costs to comply with this proposed
AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Inspect root ribs 1 work-hour x $85 per hour = $85 Not Applicable $85 per product 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
proposed inspection. The agency has no way of determining 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 8 work-hours x $85 per hour = $680
$1,000
$1,680

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 that the 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:

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: