Published 2024-01-03 · Federal Register document 2023-28850
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 all Embraer S.A. Model ERJ 190-300 and -400 airplanes. This AD was prompted by a report that the method for calculating level-off altitude by the computerized airplane flight manual (CAFM), may result in a non- conservative level-off height. This AD requires revising the existing airplane flight manual (AFM) to incorporate new CAFM versions 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 2026-09-03T22:24:17.530091+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2024-766a4e72ab891edd
- Source row
- results[8]
- Raw source SHA-256
- 766a4e72ab891edde7194caaae181bc9ea3fd0d54e65313e290f97067e3b7c5a
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-26-01
- Effective date printed in this edition
- 2024-01-18
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective January 18, 2024.
Exact source excerpt. Text positions 13232–13322, end exclusive, in the original decoded publication. SHA-256: 3ca7988f2187040bfe705f46da85ca09108a3b1f588189e94d447f85497670cc
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 13322–13351, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all Embraer S.A. (Type Certificate previously
held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.;
Embraer S.A.) Model ERJ 190-300 and -400 airplanes, certificated in
any category.
Exact source excerpt. Text positions 13351–13589, end exclusive, in the original decoded publication. SHA-256: 734cf3808e8bc203545bdb4904a94fee4e0ae818894ec06bf38a42fdca68dc77
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 13589–13671, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff
Reason
(e) Reason
This AD was prompted by a report that the method for calculating
level-off altitude by the computerized airplane flight manual
(CAFM), for Model ERJ 190-300 and ERJ 190-400 airplanes, may result
in a non-conservative level-off height. The FAA is issuing this AD
to address the possibility that, in the event of an engine failure
during takeoff, an airplane may not be able to overcome obstacles
when the airport is limited to obstacle clearance in the
acceleration segment.
Exact source excerpt. Text positions 13671–14169, end exclusive, in the original decoded publication. SHA-256: dc4cca6d9f16bf6cd785b0bca7419c9c4e1a5cf8c67b4b50afe31aa4d91e867a
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 14169–14271, 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, Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o
Civil (ANAC) AD 2023-04-02, effective April 11, 2023 (ANAC AD 2023-
04-02).
Exact source excerpt. Text positions 14271–14562, end exclusive, in the original decoded publication. SHA-256: 7a39cbefdf0a5c20f9d1090d5845f627b474c670d3f64340833f6a9be00a3e76
Exceptions to ANAC AD 2023-04-02
(h) Exceptions to ANAC AD 2023-04-02
(1) Where ANAC AD 2023-04-02 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Paragraph (c) of ANAC AD 2023-04-02 is not adopted by this
AD.
Exact source excerpt. Text positions 14562–14791, end exclusive, in the original decoded publication. SHA-256: 0467449b868a80fff04e1ca1c26d2f654ac0660ca503b1797c4d69da7b61c20b
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 manager
International Validation Branch, send it to the attention of the
person identified in paragraph (j)(2) 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 14791–15976, end exclusive, in the original decoded publication. SHA-256: a7b827924033a885598616f8804683e59a875ce8b4d47e4b9c13199b8c939105
Additional Information
(j) Additional Information
(1) Refer to ANAC AD 2023-04-02, effective April 11, 2023, for
related information. This ANAC AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2023-2399.
(2) For more information about this AD, contact Joshua Bragg,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: 216-316-6418; email:
[email protected].
Exact source excerpt. Text positions 15976–16388, end exclusive, in the original decoded publication. SHA-256: ba6ec9e230a671127aefc794e437bde8371e414b8b7ffdc2347775c590226b8c
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference
[[Page 256]]
(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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 2023-04-02, effective April 11, 2023.
(ii) [Reserved]
(3) For ANAC AD 2023-04-02, 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 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 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 [email protected].
Exact source excerpt. Text positions 16388–17881, end exclusive, in the original decoded publication. SHA-256: 09fc73130624dad30a413d05496ac9dc17708b443f68ce0921b757de939778a1
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 2023-26-01 · 1 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: 6b1d3c900c20ac60ccf03cd1648ef30c35057ae7983297b1d8be5c8a1b9bc6b0. Source manifest: ce2429fcd495eaac50c34562f77ae09b7d3a6a8b05f7267c7c2f36e2aa3d69d8.
Official source · 2024-01-03
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 89, Number 2 (Wednesday, January 3, 2024)]
[Rules and Regulations]
[Pages 253-256]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-28850]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-2399; Project Identifier MCAI-2023-00592-T;
Amendment 39-22644; AD 2023-26-01]
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 all
Embraer S.A. Model ERJ 190-300 and -400 airplanes. This AD was prompted
by a report that the method for calculating level-off altitude by the
computerized airplane flight manual (CAFM), may result in a non-
conservative level-off height. This AD requires revising the existing
airplane flight manual (AFM) to incorporate new CAFM versions 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 is effective January 18, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 18,
2024
The FAA must receive comments on this AD by February 20, 2024.
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
[[Page 254]]
p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-2399; 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 service information identified in this final rule,
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 referenced 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-2023-2399.
FOR FURTHER INFORMATION CONTACT: Joshua Bragg, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: 216-316-6418; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this final rule. Send your comments to an address
listed under ADDRESSES. Include ``Docket No. FAA-2023-2399; Project
Identifier MCAI-2023-00592-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 Joshua
Bragg, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: 216-316-6418; 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 2023-04-02, effective April 11, 2023 (ANAC AD 2023-04-02) (also
referred to as the MCAI), to correct an unsafe condition for all
Embraer S.A. Model ERJ 190-300 and -400 airplanes. The MCAI states that
the method to calculate level-off altitude by the CAFM may result in a
non-conservative level-off height. In case of an engine failure during
a takeoff, the airplane may not be able to overcome obstacles when the
airport is limited to obstacle clearance in the acceleration segment.
Since this condition may occur in other airplanes and affects flight
safety, corrective action is required.
The FAA is issuing this AD to address the unsafe condition on these
products. You may examine the MCAI in the AD docket at regulations.gov
under Docket No. FAA-2023-2399.
Related Service Information Under 1 CFR Part 51
ANAC AD 2023-04-02 specifies procedures for updating Supplement 1
of the AFM to incorporate CAFM version 1.9 or further versions for
Model ERJ 190-300 airplanes or CAFM version 1.5 or further versions for
Model ERJ 190-400 airplanes, as approved versions in the Limitations
block. 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
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
referenced 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
2023-04-02 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 2023-04-02 is incorporated by reference in this AD. This AD
requires compliance with ANAC AD 2023-04-02 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 2023-04-02 for compliance will be available at regulations.gov under
Docket No. FAA-2023-2399 after this AD is published.
Justification for Immediate Adoption 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
[[Page 255]]
effective in less than thirty days, upon a finding of good cause.
In addition, 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,
for the same reasons the FAA found good cause to forgo notice and
comment.
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
foregoing 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
The requirements of the Regulatory Flexibility Act (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 prior 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
------------------------------------------------------------------------
Parts Cost per
Labor cost cost product
------------------------------------------------------------------------
1 work-hour x $85 per hour = $85.................. $0 $85
------------------------------------------------------------------------
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.
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:
2023-26-01 Embraer S.A. (Type Certificate Previously Held by
Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer
S.A.): Amendment 39-22644; Docket No. FAA-2023-2399; Project
Identifier MCAI-2023-00592-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 18, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Embraer S.A. (Type Certificate previously
held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.;
Embraer S.A.) Model ERJ 190-300 and -400 airplanes, certificated in
any category.
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
(e) Reason
This AD was prompted by a report that the method for calculating
level-off altitude by the computerized airplane flight manual
(CAFM), for Model ERJ 190-300 and ERJ 190-400 airplanes, may result
in a non-conservative level-off height. The FAA is issuing this AD
to address the possibility that, in the event of an engine failure
during takeoff, an airplane may not be able to overcome obstacles
when the airport is limited to obstacle clearance in the
acceleration segment.
(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, Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o
Civil (ANAC) AD 2023-04-02, effective April 11, 2023 (ANAC AD 2023-
04-02).
(h) Exceptions to ANAC AD 2023-04-02
(1) Where ANAC AD 2023-04-02 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Paragraph (c) of ANAC AD 2023-04-02 is not adopted by 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 manager
International Validation Branch, send it to the attention of the
person identified in paragraph (j)(2) 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
(1) Refer to ANAC AD 2023-04-02, effective April 11, 2023, for
related information. This ANAC AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2023-2399.
(2) For more information about this AD, contact Joshua Bragg,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: 216-316-6418; email:
[email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference
[[Page 256]]
(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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 2023-04-02, effective April 11, 2023.
(ii) [Reserved]
(3) For ANAC AD 2023-04-02, 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 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 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 [email protected].
Issued on December 18, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-28850 Filed 1-2-24; 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 2026-10-09T01:31:26.905021+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 8cd221bfafc8306279d8bb45771e0369897064cc1b0652ab8d4315692cf6857f
- Text SHA-256
- 6b1d3c900c20ac60ccf03cd1648ef30c35057ae7983297b1d8be5c8a1b9bc6b0
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.