Proposed Rule2025-01884
Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.; Empresa Brasileira de Aeronáutica S.A. (EMBRAER)) Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
January 31, 2025
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2006-20-08, which applies to all Embraer S.A. Model EMB-145, -145ER, - 145MR, -145LR, -145XR, -145MP, and -145EP airplanes. AD 2006-20-08 requires repetitive inspections to detect cracking or failure of the rod ends and fittings of the aileron power control actuator (PCA) and corrective actions if necessary, and provides an optional terminating action. Since the FAA issued AD 2006-20-08, it has been determined that there was an error in identifying a maintenance task number. This proposed AD would continue to require the actions in AD 2006-20-08 and corrects an error in a task number, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 90 Issue 20 (Friday, January 31, 2025)</title>
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[Federal Register Volume 90, Number 20 (Friday, January 31, 2025)]
[Proposed Rules]
[Pages 8684-8687]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-01884]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0010; Project Identifier MCAI-2024-00270-T]
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.; Empresa Brasileira de Aeron[aacute]utica S.A.
(EMBRAER)) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2006-20-08, which applies to all Embraer S.A. Model EMB-145, -145ER, -
145MR, -145LR, -145XR, -145MP, and -145EP airplanes. AD 2006-20-08
requires repetitive inspections to detect cracking or failure of the
rod ends and fittings of the aileron power control actuator (PCA) and
corrective actions if necessary, and provides an optional terminating
action. Since the FAA issued AD 2006-20-08, it has been determined that
there was an error in identifying a maintenance task number. This
proposed AD would continue to require the actions in AD 2006-20-08 and
corrects an error in a task number, as specified in an Ag[ecirc]ncia
Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is proposed
for incorporation by reference (IBR). The FAA is proposing this AD to
address the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by March 17,
2025.
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 <a href="http://regulations.gov">regulations.gov</a>. 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 <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2025-0010; 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:
<bullet> For ANAC material identified in this proposed 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 <a href="/cdn-cgi/l/email-protection#43332220037f22632b3126257e" http: anac.gov">anac.gov</a>.br">pac@<a href="http://anac.gov">anac.gov</a>.br</a>;
website <a href="http://anac.gov">anac.gov</a>.br/en/. You may find this material on the ANAC website
at <a href="http://sistemas.anac.gov">sistemas.anac.gov</a>.br/certificacao/DA/DAE.asp. It is also available
at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2025-0010.
<bullet> 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.
FOR FURTHER INFORMATION CONTACT: Hassan Ibrahim, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 206-231-3653; email <a href="/cdn-cgi/l/email-protection#563e3725253738783b783f3424373e3f3b1630373778313920"><span class="__cf_email__" data-cfemail="b0d8d1c3c3d1de9edd9ed9d2c2d1d8d9ddf0d6d1d19ed7dfc6">[email protected]</span></a>.
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-2025-0010;
Project Identifier MCAI-2024-00270-T'' 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 this 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
<a href="http://regulations.gov">regulations.gov</a>, 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
Hassan Ibrahim,
[[Page 8685]]
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 206-231-3653; email
<a href="/cdn-cgi/l/email-protection#f991988a8a9897d794d7909b8b98919094b99f9898d79e968f"><span class="__cf_email__" data-cfemail="85ede4f6f6e4ebabe8abece7f7e4edece8c5e3e4e4abe2eaf3">[email protected]</span></a>. 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 2006-20-08, Amendment 39-14777 (71 FR 58487,
October 4, 2006) (AD 2006-20-08), for all Embraer Model EMB-145, -
145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes. AD 2006-
20-08 was prompted by an MCAI originated by Departmento de Aviacao
Civil (DAC), which was the aviation authority for Brazil (now known as
ANAC). DAC issued AD 1999-02-01R6, dated June 21, 2004, to correct an
unsafe condition.
AD 2006-20-08 requires repetitive inspections to detect cracking or
failure/breaking of the rod ends and fittings of the aileron PCA,
corrective actions if necessary, and provides an optional terminating
action for the requirements. The FAA issued AD 2006-20-08 to detect and
correct cracking or breaking of the rod ends and connecting fittings of
the aileron PCA, which could result in reduced controllability of the
airplane.
Actions Since AD 2006-20-08 Was Issued
Since the FAA issued AD 2006-20-08, ANAC superseded AD 1999-02-
01R6, dated June 21, 2004, and issued ANAC AD 1999-02-01R7, effective
May 6, 2024; corrected October 11, 2024 (ANAC AD 1999-02-01R7) (also
referred to as the MCAI), to correct an unsafe condition for all
Embraer S.A. Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and
-145EP airplanes. The MCAI states that after ANAC AD 1999-02-01R6 was
issued it was identified that the visual inspection task number
referenced on requirement (c) of that AD (AMM TASK 27-12-01-212-002-
A00, ``Aileron PCA Rod Ends/Fitting, Lugs for Integrity and General
Condition'') was incorrect. ANAC AD 1999-02-01R7 was issued to replace
the task reference to MRB-145/1150 TASK 27-12-01-212-002-A05. For
airplanes identified in paragraph (c) of ANAC AD 1999-02-01R7,
accomplishing repetitive inspections as specified in MRB-145/1150 TASK
27-12-01-212-002-A05 are necessary to address the unsafe condition.
The FAA is proposing this AD to detect and correct cracking or
breaking of the rod ends and connecting fittings of the aileron PCA,
which could result in reduced controllability of the airplane. You may
examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under Docket No.
FAA-2025-0010.
Explanation of Retained Requirements
Although this proposed AD does not explicitly restate the
requirements of AD 2006-20-08, this proposed AD would retain certain
requirements of AD 2006-20-08. Those requirements are referenced in
ANAC AD 1999-02-01R7, which, in turn, is referenced in paragraph (g) of
this proposed AD.
Material Incorporated by Reference Under 1 CFR Part 51
ANAC AD 1999-02-01R7 specifies procedures for repetitive
inspections to detect cracking and failure of the rod ends and PCA
fittings of the aileron PCA and corrective actions if necessary, and
provides an optional terminating action. Corrective actions include
replacing cracked and failed rod ends and PCA fittings. 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
referenced above. The FAA is issuing this NPRM after determining that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would retain certain requirements of AD 2006-20-
08. This proposed AD would require accomplishing the actions specified
in ANAC AD 1999-02-01R7 described previously, except for any
differences identified as exceptions in the regulatory text of this
proposed 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, the
FAA proposes to incorporate ANAC AD 1999-02-01R7 by reference in the
FAA final rule. This proposed AD would, therefore, require compliance
with ANAC AD 1999-02-01R7 in its entirety through that incorporation,
except for any differences identified as exceptions in the regulatory
text of this proposed AD. Material required by ANAC AD 1999-02-01R7 for
compliance will be available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-
2025-0010 after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 272 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Retained actions from AD 2006-20- 1 work-hour x $85 None............. $85 $23,120
08. per hour = $85.
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Estimated Costs for Optional Actions
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Labor cost Parts cost Cost per product
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24 work-hours x $85 per hour = $19,817 $21,857
$2,040.........................
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[[Page 8686]]
The FAA estimates the following costs to do any necessary on-
condition action that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need this on-condition actions:
Estimated Costs of On-Condition Actions
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Labor cost Parts cost Cost per product
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24 work-hours x $85 per hour = $19,817 $21,857
$2,040.........................
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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 this 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
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:
0
a. Removing Airworthiness Directive (AD) 2006-20-08, Amendment 39-14777
(71 FR 58487, October 4, 2006); and
0
b. Adding the following new AD:
Embraer S.A. (Type Certificate Previously Held by Yabor[atilde]
Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer S.A.; Empresa
Brasileira de Aeron[aacute]utica S.A. (EMBRAER)): Docket No. FAA-
2025-0010; Project Identifier MCAI-2024-00270-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by March 17, 2025.
(b) Affected ADs
This AD replaces AD 2006-20-08, Amendment 39-14777 (71 FR 58487,
October 4, 2006) (AD 2006-20-08).
(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.; Empresa Brasileira de Aeron[aacute]utica S.A.
(EMBRAER)) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP,
and -145EP airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
(e) Unsafe Condition
This AD was prompted by reports of broken rod ends of the
aileron power control actuator (PCA) at the aileron or at the wing
structure connection points and a determination that an incorrect
task number was published in AD 2006-20-08. The FAA is issuing this
AD to address cracking or breaking of the rod ends and connecting
fittings of the aileron PCA. The unsafe condition, if not addressed,
could result in reduced controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraphs (h) and (i) 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 1999-02-01R7, effective May 6, 2024; corrected
October 11, 2024 (ANAC AD 1999-02-01R7).
(h) Exceptions to ANAC AD 1999-02-01R7
(1) Where ANAC AD 1999-02-01R7 refers to ``21 jul. 2004,'' this
AD requires using November 8, 2006 (the effective date of AD 2006-
20-08).
(2) This AD does not adopt paragraph (f) of ANAC AD 1999-02-
01R7.
(3) Where ANAC AD 1999-02-01R7 specifies ``operating days,''
this AD requires replacing that text with ``days.''
(4) Where paragraphs (a)2. and (a)3. of ANAC AD 1999-02-01R7
specify to replace cracked and failed rod ends and PCA fittings, for
this AD, all applicable replacements must be done before further
flight.
(5) Where paragraph (a) of ANAC AD 1999-02-01R7 does not specify
an initial compliance time for the repetitive inspections, for this
AD the initial compliance time for the inspection is at the
applicable time identified in paragraph (h)(5)(i), (ii), or (iii) of
this AD.
(i) For airplanes that have PCAs with part number (P/N) 394900-
1003 or 394900-1005, do the initial inspection within 3 days after
November 8, 2006.
(ii) For airplanes that have PCAs with P/N 394900-1007, do the
initial inspection within 14 days after November 8, 2006.
(iii) For airplanes that have PCAs with P/Ns 418800-1001,
418800-1003, 418800-9003, 418800-1005, 418800-9005, 418800-1007, or
418800-9007; and that have new reinforced PCA fittings installed in
accordance with paragraph (k) or (l) of AD 2006-20-08 or paragraph
(b) of ANAC AD 1999-02-01R7, do the initial inspection within 500
flight hours after November 8, 2006.
(6) Where paragraph (b) of ANAC AD 1999-02-01R7 specifies to
accomplish an installation within ``6000 operating cycles,'' for
this AD, the compliance time is at the applicable time specified in
paragraph (h)(6)(i) or (ii) of this AD.
(i) For airplanes with PCAs with P/N 394900-1003, 394900-1005,
or 394900-1007: At the later of the times in paragraphs (h)(6)(i)(A)
or (B) of this AD.
(A) Before the airplane accumulates 6,000 total flight hours.
(B) Within 3 days or 25 flight hours after November 8, 2006 (the
effective date of AD 2006-20-08), whichever occurs later.
(ii) For airplanes with PCAs with P/N 418800-1001, 418800-1003,
418800-9003,
[[Page 8687]]
418800-1005, 418800-9005, 418800-1007, or 418800-9007: Before the
airplane accumulates 6,000 total flight cycles or within 600 flight
cycles after November 8, 2006 (the effective date of AD 2006-20-08),
whichever occurs later.
(7) Where paragraph (c) of ANAC AD 1999-02-01R7 specifies to do
an inspection in accordance with a task, for this AD, inspections
done before the effective date of this AD using AMM Task 27-12-01-
212-002-A00 or using a method approved by either the Manager,
International Validation Branch, FAA, or ANAC (or its delegated
agent) are acceptable methods of compliance. Inspections done on or
after the effective date of this AD must be done using the task
identified in paragraph (c) of ANAC AD 1999-02-01R7 or using a
method approved as specified in paragraph (k)(2) of this AD.
(8) Where paragraph (c) of ANAC AD 1999-02-01R7 specifies to
accomplish the initial inspection ``in conjunction with the new PCA
fittings and reinforcement provisions referred on item (b) above,''
this AD requires replacing that text with ``Within 500 flight hours
after accomplishing the installation and reinforcements provisions
referred to item (b) above.''
(9) Where paragraph (c) of ANAC AD 1999-02-01R7 specifies to
accomplish the inspections ``every 500 flight hours'' this AD
requires replacing that text with ``at intervals not to exceed 500
flight hours.''
(10) Where paragraph (d) of ANAC AD 1999-02-01R7 specifies to
accomplish the inspections ``every 1000 flight hours'' this AD
requires replacing that text with ``at intervals not exceeding 1,000
flight hours.''
(i) Credit for Previous Actions
This paragraph provides credit for the replacement specified in
paragraph (a)2. of ANAC AD 1999-02-01R7 and the optional terminating
actions specified in paragraph (d) of ANAC AD 1999-02-01R7, if those
actions were performed before the effective date of this AD using
EMBRAER Service Bulletin 145-27-0061, dated October 19, 1999.
(j) No Return of Parts
Where the service information identified in ANAC AD 1999-02-01R7
specifies to send parts to the parts manufacturer, that action is
not required by this AD.
(k) 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 of the
International Validation Branch, send it to the attention of the
person identified in paragraph (l)(1) of this AD and email to:
<a href="/cdn-cgi/l/email-protection#0544484a46456364642b626a73"><span class="__cf_email__" data-cfemail="62232f2d21220403034c050d14">[email protected]</span></a>.
(i) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(ii) AMOCs approved previously for AD 2006-20-08 are approved as
AMOCs for the corresponding provisions of ANAC AD 1999-02-01R7 that
are required by paragraph (g) of this AD.
(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.
(l) Additional Information
(1) For more information about this AD, contact Hassan Ibrahim,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 206-231-3653; email
<a href="/cdn-cgi/l/email-protection#167e7765657778387b387f7464777e7f7b5670777738717960"><span class="__cf_email__" data-cfemail="b0d8d1c3c3d1de9edd9ed9d2c2d1d8d9ddf0d6d1d19ed7dfc6">[email protected]</span></a>.
(2) For EMBRAER material identified in this AD that is not
incorporated by reference, contact Embraer S.A., Technical
Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170--
Putim--12227-901 S[atilde]o Jose dos Campos--SP--Brasil; telephone
+55 12 3927-5852 or +55 12 3309-0732; fax +55 12 3927-7546; email
<a href="/cdn-cgi/l/email-protection#53373a2027213a3113363e31213236217d303c3e7d3121"><span class="__cf_email__" data-cfemail="7c18150f080e151e3c19111e0e1d190e521f1311521e0e">[email protected]</span></a>; website <a href="http://flyembraer.com">flyembraer.com</a>.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 1999-02-01R7, effective May 6, 2024; corrected October 11, 2024.
(ii) [Reserved]
(3) For ANAC material identified in this AD, contact 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 <a href="/cdn-cgi/l/email-protection#5a2a3b391a663b7a32283f3c67" http: anac.gov">anac.gov</a>.br">pac@<a href="http://anac.gov">anac.gov</a>.br</a>; website <a href="http://anac.gov">anac.gov</a>.br/en/. You may find this
material on the ANAC website at <a href="http://sistemas.anac.gov">sistemas.anac.gov</a>.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 <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#9dfbefb3f4f3eeedf8fee9f4f2f3ddf3fceffcb3faf2eb"><span class="__cf_email__" data-cfemail="c7a1b5e9aea9b4b7a2a4b3aea8a987a9a6b5a6e9a0a8b1">[email protected]</span></a>.
Issued on January 23, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-01884 Filed 1-30-25; 8:45 am]
BILLING CODE 4910-13-P
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