Published 2023-06-05 · Federal Register document 2023-11813
Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. Model ERJ 190-300 and ERJ 190-400 airplanes. This AD was prompted by the excessive operation of certain elevator and rudder surfaces during manufacturing, causing damage and accelerating wear of internal parts of the power control units (PCUs). This AD requires replacement of the left-hand (LH) and right-hand (RH) elevator PCUs and lower and upper rudder PCUs, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference. 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 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[150]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-10-01
- Effective date printed in this edition
- 2023-06-20
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective June 20, 2023.
Exact source excerpt. Text positions 14194–14281, end exclusive, in the original decoded publication. SHA-256: e176f9fa21796ffaa2dd253fe53865785e9439244ebec4dd9fe1ce9a838ced27
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 14281–14310, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Embraer S.A Model ERJ 190-300, and 190-400
airplanes, certificated in any category, as identified in
Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) 2022-
09-01, effective September 7, 2022 (ANAC AD 2022-09-01).
Exact source excerpt. Text positions 14310–14580, end exclusive, in the original decoded publication. SHA-256: d86995e2851f816996dd77f6a1dff0a40ed145666e107ba61ad82426cf62d6aa
Subject
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
Exact source excerpt. Text positions 14580–14668, end exclusive, in the original decoded publication. SHA-256: 186fb9f39cb08117e4277f92b8c074b8e40e49dd904f8efbc03dae9d2afec4cd
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by the excessive operation of certain
elevator and rudder surfaces during manufacturing. The FAA is
issuing this AD to address damage to internal parts of these PCUs,
which can accelerate their wear. The unsafe condition, if not
addressed, could leave the PCUs unprotected from aeroelastic
phenomena, which can adversely affect aircraft structural integrity
under certain operational conditions and compromise safety of
flight.
Exact source excerpt. Text positions 14668–15151, end exclusive, in the original decoded publication. SHA-256: 3935cf469d7ed2a1a93328c07f448c3079f20a9a5d576b071cb6ee439104c33f
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 15151–15253, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, ANAC AD 2022-09-01.
Exact source excerpt. Text positions 15253–15439, end exclusive, in the original decoded publication. SHA-256: ac0e74fc9c6828aaf8ef59bda2ef535490e915f5e651232e2cad701cd71642b6
Exceptions to ANAC AD 2022-09-01
(h) Exceptions to ANAC AD 2022-09-01
(1) Where ANAC AD 2022-09-01 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Alternative methods of compliance (AMOC)'' section of
ANAC AD 2022-09-01 does not apply to this AD.
Exact source excerpt. Text positions 15439–15711, end exclusive, in the original decoded publication. SHA-256: 96d4020039a82e7813fd5d20d6b21888ee07694549e688ab4cde10b6897c9dca
Additional AD Provisions
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) 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 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (j) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or ANAC; or ANAC's authorized Designee. If
approved by the ANAC Designee, the approval must include the
Designee's authorized signature.
Exact source excerpt. Text positions 15711–16883, end exclusive, in the original decoded publication. SHA-256: 1f12b7e2a77a544295e29d673577238eeac369e44cd910b8160b63f495f302e2
Additional Information
(j) Additional Information
For more information about this AD, contact Allison Buss,
Aerospace Engineer, Americas Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone 303
342 1090; email [email protected].
Exact source excerpt. Text positions 16883–17142, end exclusive, in the original decoded publication. SHA-256: 88d9d1c93735834a8b074147d5f5b3b251f288f176be8853c4e85a5bd9610e3e
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 2022-09-01, effective September 7, 2022.
(ii) [Reserved]
(3) For ANAC AD 2022-09-01, contact National Civil Aviation
Agency (ANAC), Aeronautical Products Certification Branch (GGCP),
Rua Dr. Orlando Feirabend Filho, 230--Centro Empresarial Aquarius--
Torre B--Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-
190--S[atilde]o Jos[eacute] dos Campos--SP, Brazil; telephone 55
(12) 3203-6600; email: anac.gov.br">pac@anac.gov.br; internet anac.gov.br/en/.
You may find this ANAC AD on the ANAC website at
sistemas.anac.gov.br/certificacao/DA/DAE.asp.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St.,
Des Moines, WA. For information on the availability of this material
at the FAA, call 206-231-3195.
(5) You may view this material 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: www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 17142–18660, end exclusive, in the original decoded publication. SHA-256: 62b4aa636a55a931a8e2ae58087aa8c16fb47e21ecfbcb32cba44e2eceac1e23
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2023-10-01 · 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: 039fd4a2bcf1818697ff9b0815c02bb3676faf1fa940541b10af2095beb58060. Source manifest: df80420069e88b7e4557f01ac174037a77a50f421e68ce7acb000686ed3e5d98.
Official source · 2023-06-05
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 88, Number 107 (Monday, June 5, 2023)]
[Rules and Regulations]
[Pages 36461-36463]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-11813]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 88, No. 107 / Monday, June 5, 2023 / Rules
and Regulations
[[Page 36461]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1045; Project Identifier MCAI-2022-01209-T;
Amendment 39-22437; AD 2023-10-01]
RIN 2120-AA64
Airworthiness Directives; Embraer S.A. (Type Certificate
Previously Held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica
S.A.; Embraer S.A.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Embraer S.A. Model ERJ 190-300 and ERJ 190-400 airplanes. This
AD was prompted by the excessive operation of certain elevator and
rudder surfaces during manufacturing, causing damage and accelerating
wear of internal parts of the power control units (PCUs). This AD
requires replacement of the left-hand (LH) and right-hand (RH) elevator
PCUs and lower and upper rudder PCUs, as specified in an Ag[ecirc]ncia
Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is
incorporated by reference. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD becomes effective June 20, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 20,
2023.
The FAA must receive comments on this AD by July 20, 2023.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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-2023-1045; 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, 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:
<bullet> For ANAC material incorporated by reference in this AD,
contact National Civil Aviation Agency (ANAC), Aeronautical Products
Certification Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230--
Centro Empresarial Aquarius--Torre B--Andares 14 a 18, Parque
Residencial Aquarius, CEP 12.246-190--S[atilde]o Jos[eacute] dos
Campos--SP, Brazil; telephone 55 (12) 3203-6600; email anac.gov.br">pac@anac.gov.br;
website anac.gov.br/en/. You may find this material on the ANAC website
at sistemas.anac.gov.br/certificacao/DA/DAE.asp.
<bullet> You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available at
regulations.gov under Docket No. FAA-2023-1045.
FOR FURTHER INFORMATION CONTACT: Allison Buss, Aerospace Engineer,
Americas Section, International Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; phone 303-342-1090; email
[email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2023-1045; Project Identifier MCAI-
2022-01209-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, 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 final rule 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 final rule.
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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Allison
Buss, Aerospace Engineer, Americas Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone 303-342-
1090; email [email protected]. Any commentary that the FAA
receives which is not specifically designated as CBI will be placed in
the public docket for this rulemaking.
Background
ANAC, which is the aviation authority for Brazil, has issued ANAC
AD 2022-09-01, effective September 7, 2022 (ANAC AD 2022-09-01) (also
referred to as the MCAI), to correct an unsafe condition for certain
Embraer S.A. Model ERJ 190-300 and ERJ 190-400 airplanes. The MCAI
states that during decontamination procedures on the Embraer
manufacturing line, the
[[Page 36462]]
flight control system (FCS) surfaces were operated to make the
hydraulic fluid circulate and send the contaminants to the filter
manifolds. The elevator and rudder PCUs of the airplane were operated,
when disengaged, during manufacturing line hydraulic decontamination
procedures, which may have caused damage and could accelerate wear of
internal parts of the PCUs. The accelerated wear in both PCUs of these
flight control surfaces may leave them unprotected from aeroelastic
phenomena and compromise the airplane's structural integrity under
certain operational conditions.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1045.
Related Service Information Under 1 CFR Part 51
ANAC AD 2022-09-01 specifies procedures for replacement of the LH
and RH elevator PCUs and lower and upper rudder PCUs with airworthy
parts having the same part number.
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
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
described above. The FAA is issuing this AD after determining that the
unsafe condition described previously is likely to exist or develop on
other products of the same type design.
Requirements of This AD
This AD requires accomplishing the actions specified in ANAC AD
2022-09-01 described previously, except for any differences identified
as exceptions in the regulatory text of this AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result,
ANAC AD 2022-09-01 is incorporated by reference in this AD. This AD
requires compliance with ANAC AD 2022-09-01 in its entirety through
that incorporation, except for any differences identified as exceptions
in the regulatory text of this AD. Service information required by ANAC
AD 2022-09-01 for compliance will be available at regulations.gov under
Docket No. FAA-2023-1045 after this AD is published.
FAA's Justification and Determination of the Effective Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
There are currently no domestic operators of these products.
Accordingly, notice and opportunity for prior public comment are
unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the
forgoing reason(s), the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days.
Regulatory Flexibility Act (RFA)
The requirements of the RFA do not apply when an agency finds good
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and
comment. Because the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.
Costs of Compliance
Currently, there are no affected U.S.-registered airplanes. If an
affected airplane is imported and placed on the U.S. Register in the
future, the FAA provides the following cost estimates to comply with
this AD:
Estimated Costs for Required Actions
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
Up to 6 work-hours x $85 per * $0 Up to $510.
hour = $510.
------------------------------------------------------------------------
* The FAA has received no definitive data on which to base the cost
estimates for the parts specified in this AD.
According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in the cost estimate.
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
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, and
(2) Will not affect intrastate aviation in Alaska.
[[Page 36463]]
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 adding the following new airworthiness
directive:
2023-10-01 S.A. (Type Certificate Previously Held by Yabor[atilde]
Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer S.A.) Airplanes:
Amendment 39-22437; Docket No. FAA-2023-1045; Project Identifier
MCAI-2022-01209-T.
(a) Effective Date
This airworthiness directive (AD) is effective June 20, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Embraer S.A Model ERJ 190-300, and 190-400
airplanes, certificated in any category, as identified in
Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) 2022-
09-01, effective September 7, 2022 (ANAC AD 2022-09-01).
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
(e) Unsafe Condition
This AD was prompted by the excessive operation of certain
elevator and rudder surfaces during manufacturing. The FAA is
issuing this AD to address damage to internal parts of these PCUs,
which can accelerate their wear. The unsafe condition, if not
addressed, could leave the PCUs unprotected from aeroelastic
phenomena, which can adversely affect aircraft structural integrity
under certain operational conditions and compromise safety of
flight.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, ANAC AD 2022-09-01.
(h) Exceptions to ANAC AD 2022-09-01
(1) Where ANAC AD 2022-09-01 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Alternative methods of compliance (AMOC)'' section of
ANAC AD 2022-09-01 does not apply to this AD.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) 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 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (j) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or ANAC; or ANAC's authorized Designee. If
approved by the ANAC Designee, the approval must include the
Designee's authorized signature.
(j) Additional Information
For more information about this AD, contact Allison Buss,
Aerospace Engineer, Americas Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone 303
342 1090; email [email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 2022-09-01, effective September 7, 2022.
(ii) [Reserved]
(3) For ANAC AD 2022-09-01, contact National Civil Aviation
Agency (ANAC), Aeronautical Products Certification Branch (GGCP),
Rua Dr. Orlando Feirabend Filho, 230--Centro Empresarial Aquarius--
Torre B--Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-
190--S[atilde]o Jos[eacute] dos Campos--SP, Brazil; telephone 55
(12) 3203-6600; email: anac.gov.br">pac@anac.gov.br; internet anac.gov.br/en/.
You may find this ANAC AD on the ANAC website at
sistemas.anac.gov.br/certificacao/DA/DAE.asp.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St.,
Des Moines, WA. For information on the availability of this material
at the FAA, call 206-231-3195.
(5) You may view this material 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: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on May 10, 2023.
Gaetano A. Sciortino,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-11813 Filed 6-2-23; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T01:35:14.448801+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- ce9263bcc543558d27eb3842fa69bcf5df83fa46198f2a3d53bbb34a55be1db2
- Text SHA-256
- 039fd4a2bcf1818697ff9b0815c02bb3676faf1fa940541b10af2095beb58060
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
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.