Published 2021-11-19 · Federal Register document 2021-25259
Airworthiness Directives; Austro Engine GmbH Engines
Publication summary
The FAA is superseding Airworthiness Directive (AD) 2021-09-04 for all Austro Engine GmbH E4 and E4P model diesel piston engines. AD 2021-09-04 required replacing a certain oil pump as well as the oil filter and engine oil. This AD was prompted by reports of an oil pump blockage on E4 model diesel piston engines. This AD requires replacing a certain oil pump as well as the oil filter and engine oil. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2021-9c919420683447c6
- Source row
- results[410]
- Raw source SHA-256
- 9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2021-24-10
- Effective date printed in this edition
- 2021-12-27
Read 14 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective December 27,
2021.
Exact source excerpt. Text positions 8759–8852, end exclusive, in the original decoded publication. SHA-256: 33425befb9258c36b34fde73c72c083daa73fc014b81be6481fabb9818d68535
Affected ADs
(b) Affected ADs
This AD replaces AD 2021-09-04, Amendment 39-21517 (86 FR 21637,
April 23, 2021).
Exact source excerpt. Text positions 8852–8958, end exclusive, in the original decoded publication. SHA-256: 056059a1ef594aef8f15fef56d659cb6cd1c375336501b5d09738d90eebd4e29
Applicability wording · Applicability
(c) Applicability
This AD applies to all Austro Engine GmbH E4 and E4P model
diesel piston engines.
Exact source excerpt. Text positions 8958–9065, end exclusive, in the original decoded publication. SHA-256: 4e6b574edb081777928a0baf88fbe4e23fb84f74a220be77f8ba26a785473730
Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 8550, Reciprocating
Engine Oil System.
Exact source excerpt. Text positions 9065–9167, end exclusive, in the original decoded publication. SHA-256: e021385a7de56459392b1911092e4d1a1b66119d927984194df321fd63552b80
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by reports of an oil pump blockage on the
E4 model diesel piston engines. The FAA is issuing this AD to
prevent failure of the engine lubrication system. The unsafe
condition, if not addressed, could result in failure of the engine,
in-flight shutdown, and loss of the airplane.
Exact source excerpt. Text positions 9167–9498, end exclusive, in the original decoded publication. SHA-256: a8bd0bd12b290ddcd4ba970e6ee9ec2b6c75f7b2dcdeb382e48f3664d825074f
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 9498–9600, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(g) Required Actions
For Austro Engine GmbH E4 and E4P model diesel piston engines
having an oil pump, part number (P/N) E4A-50-000-BHY, with a serial
number (S/N) listed in paragraph 1.2., Engines Affected, of Austro
Engine GmbH Mandatory Service Bulletin No. MSB-E4-030/4, Revision
No. 4, dated March 30, 2021 (the MSB), within the compliance time
specified in Table 1 to paragraph (g) of this AD or before further
flight, whichever occurs later:
(1) Remove the oil pump, P/N E4A-50-000-BHY, from service and
replace with a part eligible for installation using the
Accomplishment/Instructions, paragraph 2.2.1 or paragraph 2.2.2, of
the MSB, as applicable.
(2) Replace the oil filter and engine oil using the
Accomplishment/Instructions, paragraph 2.2.1 or paragraph 2.2.2, of
the MSB, as applicable.
BILLING CODE 4910-13-P
[GRAPHIC] [TIFF OMITTED] TR19NO21.576
BILLING CODE 4910-13-C
Exact source excerpt. Text positions 9600–10513, end exclusive, in the original decoded publication. SHA-256: ecd10655be33e0c4aa38bd83f9604f8988b29a880d51776cf601b1834524101d
No Reporting Requirements
(h) No Reporting Requirements
The reporting requirements in the Accomplishment/Instructions,
paragraph 2.2., of the MSB, are not required by this AD.
Exact source excerpt. Text positions 10513–10670, end exclusive, in the original decoded publication. SHA-256: fee6f5ff154819d9f2c913388193ac951f7045db763670dd28fbe15b18a07098
Installation Prohibition
(i) Installation Prohibition
After the effective date of this AD, do not install onto any
engine an oil pump, P/N
[[Page 64813]]
E4A-50-000-BHY, with an S/N listed in paragraph 1.2., Engines
Affected, of the MSB.
Exact source excerpt. Text positions 10670–10893, end exclusive, in the original decoded publication. SHA-256: 027d1340947f817ae9fdeb61d48f0c6ee350c818cce526285da2ff4cd9e02b00
Definitions
(j) Definitions
For the purpose of this AD:
(1) Group 1 engines are E4 model diesel piston engines in
configuration ``-A'' that are installed on single-engine airplanes.
(2) Group 2 engines are E4 model diesel piston engines in
configuration ``-B'' or ``-C'' and E4P model diesel piston engines
that are installed on twin-engine airplanes.
(3) A ``part eligible for installation'' is an oil pump with a
P/N and S/N that is not listed in paragraph 1.2., Engines Affected,
of the MSB.
Exact source excerpt. Text positions 10893–11399, end exclusive, in the original decoded publication. SHA-256: a514f46bf89bcfdca5ef6a20c72b71e58dcb54e1210b346efcf9a9d568f45163
Credit for Previous Actions
(k) Credit for Previous Actions
You may take credit for replacing the oil pump, oil filter, and
engine oil required by paragraph (g) of this AD if you performed
these replacements before the effective date of this AD using the
Accomplishment/Instructions, paragraph 2.2., of Austro Engine GmbH
MSB No. MSB-E4-030, Original Issue, dated February 18, 2021;
Revision No. 1, dated February 23, 2021; Revision No. 2, dated March
3, 2021; or Revision No. 3, dated March 18, 2021.
Exact source excerpt. Text positions 11399–11885, end exclusive, in the original decoded publication. SHA-256: 0b1b90642cb9f53ba0d75b8137a8dfdf9044cca8501042d49b8ccf4d7648da4a
Alternative Methods of Compliance (AMOCs)
(l) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO 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 paragraph (m) of this AD. Information may be emailed
to: [email protected].
(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.
Exact source excerpt. Text positions 11885–12643, end exclusive, in the original decoded publication. SHA-256: 67117668a9eefdbd9c4a238bd6567f9608de9003afc6b5555b1fafd2cfb44272
Related Information
(m) Related Information
For more information about this AD, contact Wego Wang, Aviation
Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington,
MA 01803; phone: (781) 238-7134; fax: (781) 238-7199; email:
[email protected].
Exact source excerpt. Text positions 12643–12888, end exclusive, in the original decoded publication. SHA-256: 9b0ac1b6cf671f32b1509956323632e7e2fcd818edef0a3732d50d7694bc86cc
Material Incorporated by Reference
(n) 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
May 10, 2021 (86 FR 21637, April 23, 2021).
(i) Austro Engine GmbH Mandatory Service Bulletin No. MSB-E4-
030/4, Revision No. 4, dated March 30, 2021.
(ii) [Reserved]
(4) For service information identified in this AD, contact
Austro Engine GmbH, Rudolf-Diesel-Strasse 11, 2700 Weiner Neustadt,
Austria; phone: +43 2622 23000; website: www.austroengine.at.
(5) You may view this service information 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.
(6) 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, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 12888–14240, end exclusive, in the original decoded publication. SHA-256: fbec2e2a71397182fcf1a3b0c5714b27e1e777275a9e1c0fb03c01ffee4a99a6
Explicit historical replacement wording
Find all recorded historical references to AD 2021-24-10 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: e81425f53f39366a5af96281178bfc094b1202e9aa2543911e97573b7bb598a2. Source manifest: 2353be28d7f85acefd052405a157d1a9703a90af15b2cf40207a91f955d77140.
Official source · 2021-11-19
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 86, Number 221 (Friday, November 19, 2021)]
[Rules and Regulations]
[Pages 64810-64813]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-25259]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0781; Project Identifier AD-2021-00775-E;
Amendment 39-21831; AD 2021-24-10]
RIN 2120-AA64
Airworthiness Directives; Austro Engine GmbH Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2021-09-04
for all Austro Engine GmbH E4 and E4P model diesel piston engines. AD
2021-09-04 required replacing a certain oil pump as well as the oil
filter and engine oil. This AD was prompted by reports of an oil pump
blockage on E4 model diesel piston engines. This AD requires replacing
a certain oil pump as well as the oil filter and engine oil. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective December 27, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of May
10, 2021 (86 FR 21637, April 23, 2021).
ADDRESSES: For service information identified in this final rule,
contact Austro Engine GmbH, Rudolf-Diesel-Strasse 11, 2700 Weiner
Neustadt, Austria; phone: +43 2622 23000; website: www.austroengine.at.
You may view this service information at the Airworthiness Products
Section, Operational Safety Branch, FAA, 1200 District Avenue,
Burlington, MA 01803. For information on the availability of this
material at the FAA, call (817) 222-5110. It is also available at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2021-0781.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0781; or in person at
Docket Operations between 9 a.m. and 5 p.m.,
[[Page 64811]]
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, any comments received, 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.
FOR FURTHER INFORMATION CONTACT: Wego Wang, Aviation Safety Engineer,
ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone:
(781) 238-7134; fax: (781) 238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2021-09-04, Amendment 39-21517 (86 FR
21637, April 23, 2021), (AD 2021-09-04). AD 2021-09-04 applied to all
Austro Engine GmbH E4 and E4P model diesel piston engines. The NPRM
published in the Federal Register on September 14, 2021 (86 FR 51026).
The NPRM was prompted by reports of an oil pump blockage on E4 model
diesel piston engines caused by oil contamination with casting sand
from the production process of oil pump part number (P/N) E4A-50-000-
BHY. The root cause was found to be an improperly performed sand casted
oil pump housing cleaning process. In the NPRM, the FAA proposed to
continue to require replacement of an affected oil pump, identified by
P/N and serial number (S/N) in Austro Engine GmbH Mandatory Service
Bulletin No. MSB-E4-030/4, Revision No. 4, dated March 30, 2021. In the
NPRM, the FAA also proposed to require replacement of the oil filter
and engine oil.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adoption of the AD as proposed. Accordingly, the FAA is
issuing this AD to address the unsafe condition on these products. This
AD is adopted as proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Austro Engine GmbH Mandatory Service Bulletin No.
MSB-E4-030/4, Revision No. 4, dated March 30, 2021 (the MSB). This
service information specifies procedures for replacing the affected oil
pumps installed on E4 and E4P model diesel piston engines. This service
information also specifies procedures for replacing the oil filter and
engine oil installed on these engines. In addition, this service
information identifies the applicable S/Ns of affected E4 and E4P model
diesel piston engines, the affected oil pumps requiring replacement,
and an additional oil pump replacement option. The Director of the
Federal Register previously approved the MSB for incorporation by
reference on May 10, 2021 (86 FR 21637, April 23, 2021). 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.
Costs of Compliance
The FAA estimates that this AD affects 55 engines installed on
airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Remove and replace the oil pump, oil 16 work-hours x $85 per $1,488 $2,848 $156,640
filter, and engine oil. hour = $1,360.
----------------------------------------------------------------------------------------------------------------
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 individuals.
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
0
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]
0
2. The FAA amends Sec. 39.13 by:
[[Page 64812]]
0
a. Removing Airworthiness Directive 2021-09-04, Amendment 39-21517 (86
FR 21637, April 23, 2021); and
0
b. Adding the following new airworthiness directive:
2021-24-10 Austro Engine GmbH: Amendment 39-21831; Docket No. FAA-
2021-0781; Project Identifier AD-2021-00775-E.
(a) Effective Date
This airworthiness directive (AD) is effective December 27,
2021.
(b) Affected ADs
This AD replaces AD 2021-09-04, Amendment 39-21517 (86 FR 21637,
April 23, 2021).
(c) Applicability
This AD applies to all Austro Engine GmbH E4 and E4P model
diesel piston engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 8550, Reciprocating
Engine Oil System.
(e) Unsafe Condition
This AD was prompted by reports of an oil pump blockage on the
E4 model diesel piston engines. The FAA is issuing this AD to
prevent failure of the engine lubrication system. The unsafe
condition, if not addressed, could result in failure of the engine,
in-flight shutdown, and loss of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
For Austro Engine GmbH E4 and E4P model diesel piston engines
having an oil pump, part number (P/N) E4A-50-000-BHY, with a serial
number (S/N) listed in paragraph 1.2., Engines Affected, of Austro
Engine GmbH Mandatory Service Bulletin No. MSB-E4-030/4, Revision
No. 4, dated March 30, 2021 (the MSB), within the compliance time
specified in Table 1 to paragraph (g) of this AD or before further
flight, whichever occurs later:
(1) Remove the oil pump, P/N E4A-50-000-BHY, from service and
replace with a part eligible for installation using the
Accomplishment/Instructions, paragraph 2.2.1 or paragraph 2.2.2, of
the MSB, as applicable.
(2) Replace the oil filter and engine oil using the
Accomplishment/Instructions, paragraph 2.2.1 or paragraph 2.2.2, of
the MSB, as applicable.
BILLING CODE 4910-13-P
[GRAPHIC] [TIFF OMITTED] TR19NO21.576
BILLING CODE 4910-13-C
(h) No Reporting Requirements
The reporting requirements in the Accomplishment/Instructions,
paragraph 2.2., of the MSB, are not required by this AD.
(i) Installation Prohibition
After the effective date of this AD, do not install onto any
engine an oil pump, P/N
[[Page 64813]]
E4A-50-000-BHY, with an S/N listed in paragraph 1.2., Engines
Affected, of the MSB.
(j) Definitions
For the purpose of this AD:
(1) Group 1 engines are E4 model diesel piston engines in
configuration ``-A'' that are installed on single-engine airplanes.
(2) Group 2 engines are E4 model diesel piston engines in
configuration ``-B'' or ``-C'' and E4P model diesel piston engines
that are installed on twin-engine airplanes.
(3) A ``part eligible for installation'' is an oil pump with a
P/N and S/N that is not listed in paragraph 1.2., Engines Affected,
of the MSB.
(k) Credit for Previous Actions
You may take credit for replacing the oil pump, oil filter, and
engine oil required by paragraph (g) of this AD if you performed
these replacements before the effective date of this AD using the
Accomplishment/Instructions, paragraph 2.2., of Austro Engine GmbH
MSB No. MSB-E4-030, Original Issue, dated February 18, 2021;
Revision No. 1, dated February 23, 2021; Revision No. 2, dated March
3, 2021; or Revision No. 3, dated March 18, 2021.
(l) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO 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 paragraph (m) of this AD. Information may be emailed
to: [email protected].
(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) Related Information
For more information about this AD, contact Wego Wang, Aviation
Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington,
MA 01803; phone: (781) 238-7134; fax: (781) 238-7199; email:
[email protected].
(n) 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
May 10, 2021 (86 FR 21637, April 23, 2021).
(i) Austro Engine GmbH Mandatory Service Bulletin No. MSB-E4-
030/4, Revision No. 4, dated March 30, 2021.
(ii) [Reserved]
(4) For service information identified in this AD, contact
Austro Engine GmbH, Rudolf-Diesel-Strasse 11, 2700 Weiner Neustadt,
Austria; phone: +43 2622 23000; website: www.austroengine.at.
(5) You may view this service information 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.
(6) 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, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on November 15, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-25259 Filed 11-18-21; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.