preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD AUSTRO ENGINE GMBH: Docket No. FAA-2024-2318; Project Identifier MCAI-2023-00981-E.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    November 14, 2024.

(b) AFFECTED ADS

    This  AD  replaces AD  2023-20-03,  Amendment 39-22562  (88  FR 76104,
    November 6, 2023) (AD 2023-20-03).

(c) APPLICABILITY

    This AD applies to Austro Engine GmbH Model E4 and E4P engines with an
    engine serial number (ESN) listed in  Tables 1, 2, 3, and 4  of Austro
    Engine GmbH Mandatory Service  Bulletin No. MSB-E4-039/3, Revision  3,
    dated November 22, 2023 (Austro MSB-E4-039/3).

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 8530, Reciprocating Engine
    Cylinder Section; 8550, Reciprocating Engine Oil System.

(e) UNSAFE CONDITION

    This  AD  was  prompted  by   reports  of  piston  failures  and   the
    determination that certain batches of pistons were manufactured with a
    dimensional deviation in the piston pin bore and piston diameter.  The
    FAA  is  issuing  this  AD  to  prevent  piston  failure.  The  unsafe
    condition, if  not addressed,  could result  in loss  of oil,  loss of
    engine power, and reduced control of the airplane.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

(1) For  all affected  engines,  within the  applicable  compliance  times
    specified in Table 1  to paragraph (g)(1) of  this AD, perform an  oil
    analysis in  accordance with  paragraph 2.,  Technical Details, Engine
    Oil Analysis of Austro MSB-E4-039/3,  and do not return the  engine to
    service until the results of the oil analysis have been determined.

     TABLE 1 TO PARAGRAPH (G)(1)--OIL ANALYSIS FOR ALL AFFECTED ENGINES
    ----------------------------------------------------------------------
          ENGINE GROUP              COMPLIANCE TIME        INTERVAL       
    ----------------------------------------------------------------------
    Group 1 and Group 3 engines     Within 15 flight    Before exceeding
    that do not have an ESN         hours (FHs) from    50 FHs since last
    identified in Table 2 to        December 11, 2023   oil analysis.
    (g)(1) paragraph of this AD.    (the effective
                                    date of AD 2023-
                                    20-03).
    Group 1 and Group 3 engines     Within 15 FHs from  Before exceeding
    that have an ESN identified     the effective       50 FHs since last
    in Table 2 to paragraph (g)(1)  date of this AD.    toil analysis.
    of this AD.
    Group 2 and Group 4 engines     Within 25 FHs from  Before exceeding
    that do not have an ESN iden-   December 11, 2023   100 FHs since
    tified in Table 2 to paragraph  (the effective      last oil
    (g)(1) of this AD.              date of AD 2023-    analysis.
                                    20-03).
    Group 2 and Group 4 engines     Within 25 FHs from  Before exceeding
    that have an ESN identified     the effective       100 FHs since
    in Table 2 to paragraph         date of this AD.    last oil analysis.
    (g)(1) of this AD.
    ----------------------------------------------------------------------
        TABLE 2 TO PARAGRAPH (G)(1) -- AFFECTED ESNS NOT INCLUDED IN
                               AD 2023-20-03
    ----------------------------------------------------------------------
    ENGINE GROUP    ESN           ESN           ESN           ESN         
    ----------------------------------------------------------------------
    Group 1     E4-A-06367     E4-A-06248    ...........   ............
    Group 2     E4-C-06249     E4P-C-06185   ...........   ............
    Group 3     E4-A-05072     E4-A-05074    E4-A-05075    E4-A-05078
    Group 3     E4-A-05079     E4-A-05080    E4-A-05081    E4-A-05082
    Group 3     E4-A-05083     E4-A-05084    E4-A-05085    E4-A-05086
    Group 3     E4-A-05087
    Group 4     E4-C-00559     E4-C-05089    E4-C-05090    E4-C-05091
    Group 4     E4-C-05092     E4-C-05093    E4-C-05094    E4-C-05096
    Group 4     E4-C-05098     E4-C-05099    E4-C-05100    E4-C-05101
    Group 4     E4-C-05102     E4-C-05103    E4-C-05104    E4-C-05105
    Group 4     E4-C-05106     E4-C-05107    E4-C-05108    E4-C-05109
    Group 4     E4-C-05110     E4-C-05111    E4P-C-06073   ............
    ----------------------------------------------------------------------

(2) Thereafter, repeat  the oil analysis  required by paragraph  (g)(1) of
    this AD before exceeding the applicable interval specified in Table  1
    to paragraph (g)(1) of this AD.

(3) Following each repetitive oil analysis, the engine may be returned  to
    service for no more than the applicable interval specified in Table  1
    to paragraph  (g)(1) of  this AD,  until receipt  of the  oil analysis
    result.

(4) If the result of any oil analysis required by paragraph (g)(1) of this
    AD indicates the aluminum content of the oil is greater than the limit
    specified in  paragraph 2.,  Technical Details,  Engine Oil  Analysis,
    Table 5--Oil check analysis--Aluminum PPM allowable; of Austro  MSB-E4
    -039/3, before further flight, replace the pistons, piston rings,  con
    -rods  assembly,  and  crankcase,  or  replace  the  engine  core   in
    accordance  with   paragraph  2.,   Technical  Details,   Engine  core
    replacement;  or Pistons,  piston rings,  crankcase and  con-rod  assy
    replacement; as applicable, of Austro MSB-E4-039/3.

(5) For  Group 3  and Group  4 engines,  within the  applicable compliance
    times specified in Table 3 to paragraph (g)(5) of this AD, replace the
    pistons, piston rings,  and con-rods assembly,  or replace the  engine
    core in accordance with  paragraph 2., Technical Details,  Engine core
    replacement; or Pistons, piston  rings and con- rod  assy replacement,
    as applicable, of Austro MSB-E4-039/3.

      TABLE 3 TO PARAGRAPH (G)(5)--REPLACEMENT FOR GROUP 3 AND 4 ENGINES
    ----------------------------------------------------------------------
              ENGINE GROUP                       COMPLIANCE TIME          
    ----------------------------------------------------------------------
    Group 3 engines that do not have an   Before exceeding 900 FHs since
    ESN identified in Table 2 to para-    new, or within 15 FHs after
    graph (g)(1) of this AD.              December 11, 2023 (the
                                          effective date of AD 2023-20-
                                          03), whichever occurs later.
    Group 3 engines that have an ESN      Before exceeding 900 FHs since
    identified in Table 2 to paragraph    new, or within 15 FHs after
    (g)(1) of this AD.                    the effective date of this AD,
                                          whichever occurs later
    Group 4 engines that do not have an   Before exceeding 1,000 FHs
    ESN identified in Table 2 to para-    since new, or within 25 FHs
    graph (g)(1) of this AD.              after December 11, 2023 (the
                                          effective date of AD 2023-20-
                                          03), whichever occurs later.
    Group 4 engines that have an ESN      Before exceeding 1,000 FHs
    identified in Table 2 to paragraph    since new, or within 25 FHs
    (g)(1) of this AD.                    after the effective date of
                                          this AD, whichever occurs
                                          later.
    ----------------------------------------------------------------------

NOTE  1  TO  PARAGRAPH (g)(5):  FHs  since  new indicated  in  Table  3 to
paragraph (g)(5) of this AD are FHs accumulated by the engine since  first
installation on an airplane or since last overhaul as of December 11, 2023
(the effective date of  AD 2023-20-03) for Group  3 and 4 engines  that do
not have an ESN identified in Table  2 to paragraph (g)(1) of this AD,  or
as of the effective date of this AD for Group 3 and 4 engines that have an
ESN identified in Table 2 to paragraph (g)(1) of this AD.

(h) TERMINATING ACTION

(1) Replacement  of  the  pistons,  piston rings,  con-rods  assembly, and
    crankcase,  or  replacement  of  the  engine  core,  as  specified  in
    paragraph (g)(4) of  this AD, constitutes  terminating action for  the
    repetitive oil analysis required by paragraph (g)(2) of this AD.

(2) Replacement of  the pistons, piston  rings, and con-rods  assembly, or
    replacement of the  engine core, as  specified in paragraph  (g)(5) of
    this  AD,  constitutes  terminating  action  for  the  repetitive  oil
    analysis required by paragraph (g)(2) of this AD.

(i) DEFINITIONS

    For the purpose of this AD:

(1) Group 1  engines are engines  having an ESN  listed in Table  1 of No.
    MSB-E4-039/3.

(2) Group 2  engines are engines  having an ESN  listed in Table  2 of No.
    MSB-E4-039/3.

(3) Group 3  engines are engines  having an ESN  listed in Table  3 of No.
    MSB-E4-039/3.

(4) Group 4  engines are engines  having an ESN  listed in Table  4 of No.
    MSB-E4-039/3.

(j) CREDIT FOR PREVIOUS ACTIONS

(1) You may take credit for the actions required by paragraph (g)(1), (4),
    or (5) of this AD, if you performed those actions before December  11,
    2023 (the effective  date of AD  2023-20-03) using Austro  Engine GmbH
    Mandatory Service Bulletin No. MSB-E4-039/0, dated October 24, 2022.

(2) You may take credit for the actions required by paragraph (g)(1), (4),
    or (5) of this AD if you performed those actions before the  effective
    date of this  AD using Austro  Engine GmbH Mandatory  Service Bulletin
    No. MSB-E4-039/2, Revision 2, dated July 26, 2023.

(k) NO RETURN OF PARTS/REPORTING REQUIREMENT

    Although the service information specifies returning certain parts and
    submitting certain information to  the manufacturer, this AD  does not
    include those requirements.

(l) 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
    International  Validation  Branch, send  it  to the  attention  of the
    person  identified  in  paragraph  (m)(1)  of  this  AD  and  email to
    AMOC@faa.gov.

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

(m) ADDITIONAL INFORMATION

(1) For  more  information about  this AD,  contact  Morton  Lee, Aviation
    Safety Engineer,  FAA, 1600  Stewart Avenue,  Suite 410,  Westbury, NY
    11590; phone: (860) 386-1791; email: morton.y.lee@faa.gov.

(2) Material identified in this  AD that is not incorporated  by reference
    is available at the address specified in  paragraph (n)(3) of this AD.

(n) MATERIAL INCORPORATED BY REFERENCE

(1) The  Director of  the Federal  Register approved  the incorporation by
    reference  (IBR) of  the material  listed in  this  paragraph  under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material as applicable to do the actions required by
    this AD, unless the AD specifies otherwise.

(i) Austro Engine  GmbH Mandatory  Service Bulletin No. MSB-E4-039/3, Rev-
    ision 3, dated November 22, 2023.

(ii) [Reserved]

(3) For Austro Engine GmbH material identified in this AD, contact  Austro
    Engine  GmbH,  Rudolf-Diesel-Strasse   11,  A-2700  Weiner   Neustadt,
    Austria; phone: +43 2622 23000; website: austroengine.at.

(4) You  may view  this material  at FAA,  Airworthiness Products Section,
    Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803.
    For information on the availability of this material at the FAA,  call
    (817) 222-5110.

(5) You  may  view this  material at  the National  Archives  and  Records
Administration  (NARA).  For  information  on  the  availability  of  this
material   at   NARA,   visit    www.archives.gov/federal-register/cfr/ibr
-locations or email fr.inspection@nara.gov.

Issued on September 23, 2024. Steven W. Thompson, Acting Deputy  Director,
Compliance & Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this NPRM by November 14, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-2318; Project Identifier MCAI-2023-00981-E]
RIN 2120-AA64

Airworthiness Directives; Austro Engine GmbH Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2023-20-03, which applies to certain Austro Engine GmbH Model E4 and
E4P engines. AD 2023-20-03 requires repetitive engine oil analysis for
aluminum content outside the acceptable limits and, if necessary,
replacement of the pistons, piston rings, con-rods assembly, and
crankcase or, as an alternative, replacement of the engine core. Since
the FAA issued AD 2023-20-03, the manufacturer identified errors in the
lists of affected engines and provided updated information, which
prompted this proposed AD. This proposed AD would retain the
requirements of AD 2023-20-03, add compliance times for additional
affected engine serial numbers, and remove certain engine serial
numbers from the applicability of the existing AD. The FAA is proposing
this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this NPRM by November 14, 2024.

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-2024-2318; 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 mandatory continuing airworthiness
information (MCAI) any comments received, and other information. The
street address for Docket Operations is listed above.

Material Incorporated by Reference:

For Austro Engine GmbH material identified in this
proposed AD, contact Austro Engine GmbH, Rudolf-Diesel-Strasse 11, A-
2700 Weiner Neustadt, Austria; phone: +43 2622 23000; website:
austroengine.at.

You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 1200 District Avenue,
Burlington, MA 01803. For information on the availability of this
material at the FAA, call (817) 222-5110.

FOR FURTHER INFORMATION CONTACT: Morton Lee, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (860)
386-1791; email: morton.y.lee@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 the ADDRESSES section. Include "Docket No. FAA-2024-2318;
Project Identifier MCAI-2023-00981-E" 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
Morton Lee, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590. 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 2023-20-03, Amendment 39-22562 (88 FR 76104,
November 6, 2023) (AD 2023-20-03), for certain Austro Engine GmbH Model
E4 and E4P engines. AD 2023-20-03 was prompted by an MCAI originated by
the European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union. EASA
issued EASA AD 2022-0240R1, dated December 15, 2022 (EASA AD 2022-
0240R1), to address reports of piston failures.

AD 2023-20-03 requires repetitive engine oil analysis for aluminum
content outside the acceptable limits and, if necessary, replacement of
the pistons, piston rings, con-rods assembly, and crankcase or as an
alternative, replacement of the engine core. The FAA issued AD 2023-20-
03 to prevent piston failure, which could result in loss of oil, loss
of engine power, and reduced control of the airplane.

Actions Since AD 2023-20-03 Was Issued


Since the FAA issued AD 2023-20-03, EASA superseded EASA AD 2022-
0240R1 and issued EASA AD 2023-0163, dated August 18, 2023 (EASA AD
2023-0163) (also referred to as the MCAI). The MCAI states that a
manufacturer investigation into reports of piston failures determined
that certain batches of pistons were manufactured with a dimensional
deviation in the piston pin bore and in the piston diameter, which
could cause piston failure, with consequent loss of oil, loss of engine
power, and reduced control of the airplane. To address the unsafe
condition, EASA issued EASA AD 2022-0240, dated December 6, 2022, to
specify repetitive oil analyses and
replacement of the pistons, piston rings, con-rods assembly, and
crankcase, or as an alternative, replacement of the engine core. EASA
AD 2022-0240 also prohibited release to service of an airplane until
receipt of the results for each oil analysis.

Since EASA AD 2022-0240 was issued, the manufacturer determined
that aluminum levels outside of the acceptable limits would be found
during the first oil analysis and would be unlikely to be found during
subsequent oil analyses. As a result, EASA revised EASA AD 2022-0240
and issued EASA AD 2022-0240R1 to allow release to service of airplanes
for a limited number of flight hours immediately after the second and
subsequent oil samples are taken for analyses.

Since EASA AD 2022-0240R1 was issued, the manufacturer identified
errors in the lists of affected engine serial numbers in the service
information and issued Mandatory Service Bulletin No. MSB-E4-039/2,
Revision 2, dated July 31, 2023, to revise the list of affected engine
serial numbers, which prompted EASA to supersede EASA AD 2022-0240R1
with EASA AD 2023-0163, dated August 18, 2023. Since EASA issued EASA
AD 2023-0163, the manufacturer revised the service information again
and issued Mandatory Service Bulletin No. MSB-E4-039/3, Revision 3,
dated November 22, 2023, to amend the labor efforts section.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-2318.

Material Incorporated by Reference Under 1 CFR Part 51


The FAA reviewed Austro Engine GmbH Mandatory Service Bulletin No.
MSB-E4-039/3, Revision 3, dated November 22, 2023, which identifies
affected engine serial numbers and specifies procedures for oil
analysis and replacement of the pistons, piston rings, con-rods
assembly, crankcase, and engine core.

This material 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.

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 material referenced 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 the same type design.

Proposed AD Requirements in This NPRM


This proposed AD would retain all of the requirements of AD 2023-
20-03. This proposed AD would also add compliance times for additional
affected engine serial numbers and remove certain engine serial numbers
from the applicability of the existing AD, as specified in the material
already described.

Costs of Compliance


The FAA estimates that this AD, if adopted as proposed, would
affect 357 engines installed on aircraft 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
Oil analysis
1 work-hour x $85 per hour = $85
$0
$85
$30,345

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
engines that might need these replacements:

On-Condition Costs

ACTION
LABOR COST
PARTS COST
COST PER PRODUCT
Replace engine core
35 work-hours x $85 per hour = $2,975
$15,524
$18,499
Replace pistons, piston rings, and con-rod assembly
65 work-hours x $85 per hour = $5,525
2,216
7,741
Replace pistons, piston rings, con-rod assembly, and crankcase
75 work-hours x $85 per hour = $6,375
4,141
10,516

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this
proposed 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 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 2023-20-03, Amendment 39-22562
(88 FR 76104, November 6, 2023); and

b. Adding the following new airworthiness directive: