Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.) Airplanes, 57795-57798 [2024-15309]
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57795
Proposed Rules
Federal Register
Vol. 89, No. 136
Tuesday, July 16, 2024
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1704; Project
Identifier MCAI–2023–01204–T]
RIN 2120–AA64
Airworthiness Directives; Embraer S.A.
(Type Certificate Previously Held by
Yaborã Indústria Aeronáutica S.A.)
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Embraer S.A. Model ERJ 190
airplanes. This proposed AD was
prompted by a manufacturing quality
escape concerning certain overheat
detection system (ODS) sensing
elements. This proposed AD would
require inspecting the ODS sensing
elements and performing applicable
corrective actions and would prohibit
the installation of affected parts, as
specified in an Agência Nacional de
Aviação 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.
SUMMARY:
DATES:
Comments Invited
You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
regulations.gov. Follow the instructions
for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2024–1704; Project Identifier
MCAI–2023–01204–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.
The FAA must receive comments
on this proposed AD by August 30,
2024.
ADDRESSES:
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• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2024–1704; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this NPRM, the mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For ANAC material, 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—São José
dos Campos—SP, Brazil; telephone 55
(12) 3203–6600; email 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. It is also available at
regulations.gov under Docket No. FAA–
2024–1704.
• You may view this material at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
FOR FURTHER INFORMATION CONTACT:
Joshua Bragg, Aviation Safety Engineer,
FAA, 2200 South 216th Street, Des
Moines, WA 98198; phone: 817–222–
5366; email: joshua.k.bragg@faa.gov.
SUPPLEMENTARY INFORMATION:
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Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Joshua Bragg, Aviation
Safety Engineer, FAA, 2200 South 216th
Street, Des Moines, WA 98198; phone:
817–222–5366; email: joshua.k.bragg@
faa.gov. 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 2023–11–02, effective November 21,
2023 (ANAC AD 2023–11–02) (also
referred to as the MCAI), to correct an
unsafe condition for certain Embraer
S.A. Model ERJ 190–100 IGW, –100 LR,
–100 SR, –100 STD, –200 IGW, –200 LR,
and –200 STD airplanes. Model ERJ
190–100 SR airplanes are not
certificated by the FAA and are not
included on the U.S. type certificate
data sheet; this proposed AD therefore
does not include those airplanes in the
applicability. The MCAI states that a
quality escape occurred during
manufacturing concerning some ODS
sensing elements produced before
January 31, 2021. A defective sensing
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Federal Register / Vol. 89, No. 136 / Tuesday, July 16, 2024 / Proposed Rules
element may not be able to detect a
thermal bleed leak, which is a latent
failure, and depending on the affected
area, may start an ignition source in the
fuel tank, which could damage some
electronic boxes and expose the wing
structure to high temperature gradients
and unexpected thermal loads, which
could result in reduced structural
integrity of the airplane.
ANAC has informed the FAA of an
undated Errata published to correct a
printing error in the English version of
ANAC AD 2023–11–02. The FAA has
included these corrections in
paragraphs (h)(2) and (3) of this AD.
The FAA is proposing 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–2024–1704.
Related Service Information Under 1
CFR Part 51
ANAC AD 2023–11–02 specifies
procedures for a detailed inspection of
the ODS sensing elements of the
airplane bleed lines and replacement, if
applicable, and procedures for reactivation of ODS sensing elements that
were deactivated during the detailed
inspection. ANAC AD 2023–11–02 also
defines and prohibits the installation of
an affected ODS sensing element unless
the affected part passed an inspection,
indicated by a marking on one face of
the connector hex nut.
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 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 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 require
accomplishing the actions specified in
ANAC AD 2023–11–02 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 2023–11–02 by
reference in the FAA final rule. This
proposed AD would, therefore, require
compliance with ANAC AD 2023–11–02
in its entirety through that
incorporation, except for any differences
identified as exceptions in the
regulatory text of this proposed AD.
Service information required by ANAC
AD 2023–11–02 for compliance will be
available at regulations.gov under
Docket No. FAA–2024–1704 after the
FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 90
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Up to 26 work-hours × $85 per hour = Up to $2,210 ..................
The FAA estimates the following
costs to do any necessary on-condition
action that would be required based on
Cost per product
$0
Cost on U.S. operators
Up to $2,210 .............................
the results of any required actions. The
FAA has no way of determining the
Up to $198,900.
number of aircraft that might need this
on-condition action:
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
Parts cost
Cost per
product
2 work-hours × $85 per hour = $170 ......................................................................................................................
$500
$670
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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
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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
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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
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Federal Register / Vol. 89, No. 136 / Tuesday, July 16, 2024 / Proposed Rules
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Embraer S.A. (Type Certificate Previously
Held by Yaborã Indústria Aeronáutica
S.A.): Docket No. FAA–2024–1704;
Project Identifier MCAI–2023–01204–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by August 30,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Embraer S.A. (Type
Certificate previously held by Yaborã
Indústria Aeronáutica S.A.) Model ERJ 190–
100 IGW, –100 LR, –100 STD, –200 IGW,
–200 LR, and –200 STD airplanes,
certificated in any category, as identified in
Agência Nacional de Aviação Civil (ANAC)
AD 2023–11–02, effective November 21, 2023
(ANAC AD 2023–11–02).
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(d) Subject
Air Transport Association (ATA) of
America Code 28, Fuel.
(e) Unsafe Condition
This AD was prompted by a manufacturing
quality escape concerning certain overheat
detection system (ODS) sensing elements.
The FAA is issuing this AD to address
defective sensing elements. The unsafe
condition, if not addressed, could result in a
sensing element not being able to detect a
thermal bleed leak, which is a latent failure,
and, depending on the affected area, may
start an ignition source in the fuel tank,
which could damage some electronic boxes
and expose the wing structure to high
temperature gradients and unexpected
thermal loads, which could result in reduced
structural integrity of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
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(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, ANAC AD 2023–11–
02.
(h) Exceptions to ANAC AD 2023–11–02
(1) Where ANAC AD 2023–11–02 refers to
its effective date, this AD requires using the
effective date of this AD.
(2) Where paragraph (b)(1) of ANAC AD
2023–11–02 specifies ‘‘Within 5,000 Flight
Hours (FH) or 24 months,’’ for this AD,
replace that text with ‘‘Within 7,500 Flight
Hours (FH) or 36 months.’’
(3) Where paragraphs (c)(1), (d)(1), (e)(1),
(f)(1), and (g)(1) of ANAC AD 2023–11–02
specify ‘‘Within 5,000 FH or 24 months,’’ for
this AD, replace that text with ‘‘Within 7,500
FH or 36 months.’’
(4) Where paragraphs (b)(1), (c)(1), (d)(1),
(e)(1), (f)(1), and (g)(1) of ANAC AD 2023–
11–02 specify to inspect ODS sensing
elements at various locations, this AD
requires adding ‘‘in accordance with Embraer
Service Bulletin 190–36–0027, Revision 02,
dated September 5, 2023; or later revisions
approved by ANAC.’’
(5) Where paragraphs (b) through (h) of
ANAC AD 2023–11–02 specify on-condition
actions based on the results of the ODS
sensing element inspections required by
paragraphs (b)(1), (c)(1), (d)(1), (e)(1), (f)(1),
and(g)(1) of ANAC AD 2023–11–02, this AD
requires performing all applicable oncondition actions before further flight after
each inspection.
(6) This AD does not adopt paragraph (k)
of ANAC AD 2023–11–02.
(7) Where paragraph (l) of ANAC AD 2023–
11–02 specifies ‘‘Record compliance with
this [ANAC] AD in the applicable
maintenance log book,’’ for this AD, record
compliance with this FAA AD.
(i) No Return of Parts Requirement
Although the service information
referenced in ANAC AD 2023–11–02
specifies to send removed parts to the
manufacturer, this AD does not include that
requirement.
(j) Special Flight Permit
Special flight permits, as described in 14
CFR 21.197 and 21.199, are not allowed.
(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, mail it to the address identified in
paragraph (l)(1) of this AD. Information may
be emailed to: 9-AVS-AIR-730-AMOC@
faa.gov. Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
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57797
(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.
(3) Required for Compliance (RC): Except
as required by paragraphs (i) and (k)(2) of this
AD, if any service information referenced in
ANAC AD 2023–11–02 contains steps in the
Accomplishment Instructions or figures that
are labeled as RC, the instructions in RC
steps, including subparagraphs under an RC
step and any figures identified in an RC step,
must be done to comply with this AD; any
steps including substeps under those steps,
that are not identified as RC are
recommended. The instructions in steps,
including substeps under those steps, not
identified as RC may be deviated from using
accepted methods in accordance with the
operator’s maintenance or inspection
program without obtaining approval of an
AMOC, provided the instructions identified
as RC can be done and the airplane can be
put back in an airworthy condition. Any
substitutions or changes to instructions
identified as RC require approval of an
AMOC. If a step or substep is labeled ‘‘RC
Exempt,’’ then the RC requirement is
removed from that step or substep.
(l) Additional Information
(1) For more information about this AD,
contact Joshua Bragg, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des
Moines, WA 98198; phone: 817–222–5366;
email: joshua.k.bragg@faa.gov.
(2) For Kidde Aerospace & Defense
material identified in ANAC AD 2023–11–02
that is not incorporated by reference, contact
Kidde Aerospace & Defense, 4200 Airport
Drive NW, Building B, Wilson, NC 27896;
telephone: 319–295–5000; website:
kiddetechnologies.com/aviation.com.
(m) 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 this AD specifies otherwise.
(i) Agência Nacional de Aviação Civil
(ANAC) AD 2023–11–02, effective November
21, 2023.
(ii) [Reserved]
(3) For ANAC AD 2023–11–02, 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—São
José dos Campos—SP, Brazil; telephone 55
(12) 3203–6600; email 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
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Federal Register / Vol. 89, No. 136 / Tuesday, July 16, 2024 / Proposed Rules
Safety Branch, 2200 South 216th Street, 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 fr.inspection@
nara.gov.
Issued on June 25, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate
Management Division, Aircraft Certification
Service.
[FR Doc. 2024–15309 Filed 7–15–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF HOUSING AND
URBAN DEVELOPMENT
24 CFR Parts 203, 206, and 291
[Docket No. FR–6051–P–02]
Federal Housing Administration (FHA):
Single Family Sale Program
Office of the Assistant
Secretary for Housing—Federal Housing
Commissioner, Department of Housing
and Urban Development (HUD).
ACTION: Proposed rule.
AGENCY:
In a Single Family Sale (the
‘‘Program’’), eligible single family
mortgage loans insured by the Federal
Housing Administration (FHA) are
assigned to the Secretary of the
Department of Housing and Urban
Development (HUD) in exchange for
claim payments, and mortgage notes are
then sold, without FHA insurance, to
qualified purchasers in a manner that
seeks to maximize recoveries and
strengthen HUD’s Mutual Mortgage
Insurance Fund (MMIF), and to achieve
HUD’s operational goals for the MMIF.
The Program has operated as a
demonstration since 2002. This
proposed rule would transition the
Program from a demonstration to a
permanent Program by revising HUD’s
Single Family Mortgage Insurance,
Home Equity Conversion Mortgages,
and Disposition of HUD-Acquired and
-Owned Single Family Property
regulations to provide for the sale of
HUD-held single family forward
mortgages and Home Equity Conversion
Mortgages (HECMs), through
Competitive Sale of Single Family Loans
and Direct Sale of Single Family Loans.
This proposed rule would also remove
existing regulations on Disposition of
HUD-Acquired and -Owned Single
Family Property regulations which
provided for a retired program that
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SUMMARY:
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handled the sale of HUD-held single
family mortgage loans.
DATES: Comment due date: September
16, 2024.
ADDRESSES: Interested persons are
invited to submit comments regarding
this document. Comments should refer
to the above docket number and title.
There are two methods for submitting
comment.
1. Submission of comments by mail:
Comments may be submitted by mail to
the HUD Regulations Division, Office of
Housing, Department of Housing and
Urban Development, 451 7th Street SW,
Washington, DC 20410–8000; telephone:
(202) 708–2625 (this is not a toll-free
number) or toll free (800) 481–9895.
HUD welcomes and is prepared to
receive calls from individuals who are
deaf or hard of hearing, as well as
individuals with speech or
communication disabilities. To learn
more about how to make an accessible
telephone call, please visit https://
www.fcc.gov/consumers/guides/
telecommunications-relay-service-trs.
2. Electronic submission of comments:
Comments may be submitted
electronically through the Federal eRulemaking Portal at
www.regulations.gov. HUD strongly
encourages commenters to submit
comments electronically. Electronic
submission of comments allows the
commenter maximum time to prepare
and submit a comment, ensures timely
receipt by HUD, and enables HUD to
make the comments immediately
available to the public. Comments
submitted electronically through the
www.regulations.gov website can be
viewed by other commenters and
interested members of the public.
Commenters should follow instructions
provided on this site to submit
comments electronically.
Note: To receive consideration as public
comments, comments must be submitted
through one of the two methods specified
above. Again, all submissions must refer to
the docket number and title of this
document.
No Facsimile Comments. Facsimile
(FAX) comments are not acceptable.
3. Public inspection of public
comments: All properly submitted
comments and communications
submitted to HUD will be available for
public inspection and copying between
8 a.m. and 5 p.m. weekdays at the above
address. Due to security measures at the
HUD Headquarters building, an
appointment to review the public
comments must be scheduled in
advance by calling the Regulations
Division at (202) 402–5731 (this is not
a toll-free number). HUD welcomes and
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is prepared to receive calls from
individuals who are deaf or hard of
hearing, as well as individuals with
speech or communication disabilities.
To learn more about how to make an
accessible telephone call, please visit
https://www.fcc.gov/consumers/guides/
telecommunications-relay-service-trs.
Copies of all comments submitted are
available for inspection and
downloading at www.regulations.gov.
FOR FURTHER INFORMATION CONTACT: John
Lucey, Director, FHA Office of Asset
Sales, Office of Housing, Department of
Housing and Urban Development, 451
7th Street SW, Washington, DC 20410–
8000; telephone: (202) 708–2625 (this is
not a toll-free number), or toll-free: (800)
481–9895. HUD welcomes and is
prepared to receive calls from
individuals who are deaf or hard of
hearing, as well as from individuals
with speech or communication
disabilities. To learn more about how to
make an accessible telephone call,
please visit https://www.fcc.gov/
consumers/guides/telecommunicationsrelay-service-trs.
SUPPLEMENTARY INFORMATION:
I. Background
Under section 204 of the National
Housing Act,1 HUD has general
authority to pay insurance claims and
dispose of mortgages and properties
acquired under the FHA single family
mortgage insurance programs. Section
204(g) specifically grants HUD broad
discretion to implement a range of
disposition alternatives. The National
Housing Act also requires HUD ensure
the mutual mortgage insurance fund
(MMIF) remains financially sound. HUD
must effectively manage HUD’s
defaulted assets and minimize losses to
the MMIF to carry out its fiduciary
responsibility to ensure the financial
soundness of the MMIF.
Since 2002, HUD has operated a
demonstration program 2 to implement
its broad disposition authority with
respect to mortgages and properties
acquired under the FHA single family
mortgage insurance programs. By notice
published in the Federal Register on
February 5, 2002, HUD announced the
establishment of the Accelerated Claim
and Asset Disposition (ACD)
1 See 12 U.S.C. 1710 (2010), as amended by
section 601 of the Fiscal Year 1999 Departments of
Veterans Affairs and Housing and Urban
Development and Independent Agencies
Appropriations Act (Pub. L. 105–276, approved
October 21, 1998) (‘‘FY 1999 Appropriations Act’’).
2 HUD has used various names to refer to the
demonstration program, including the Accelerated
Claim and Asset Disposition (ACD) Demonstration,
the Single Family Loan Sales (‘‘SFLS’’) Program,
and the Distressed Asset Stabilization Program
(‘‘DASP’’).
E:\FR\FM\16JYP1.SGM
16JYP1
Agencies
[Federal Register Volume 89, Number 136 (Tuesday, July 16, 2024)]
[Proposed Rules]
[Pages 57795-57798]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-15309]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 89 , No. 136 / Tuesday, July 16, 2024 /
Proposed Rules
[[Page 57795]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1704; Project Identifier MCAI-2023-01204-T]
RIN 2120-AA64
Airworthiness Directives; Embraer S.A. (Type Certificate
Previously Held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica
S.A.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Embraer S.A. Model ERJ 190 airplanes. This proposed AD was
prompted by a manufacturing quality escape concerning certain overheat
detection system (ODS) sensing elements. This proposed AD would require
inspecting the ODS sensing elements and performing applicable
corrective actions and would prohibit the installation of affected
parts, 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 August 30,
2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-1704; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For ANAC material, 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. It is also available at regulations.gov under Docket No. FAA-
2024-1704.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
Des Moines, WA. For information on the availability of this material at
the FAA, call 206-231-3195.
FOR FURTHER INFORMATION CONTACT: Joshua Bragg, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone:
817-222-5366; email: [email protected].
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 ADDRESSES. Include ``Docket No. FAA-2024-1704; Project Identifier
MCAI-2023-01204-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
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Joshua Bragg, Aviation Safety Engineer, FAA, 2200 South 216th Street,
Des Moines, WA 98198; phone: 817-222-5366; 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 2023-11-02, effective November 21, 2023 (ANAC AD 2023-11-02) (also
referred to as the MCAI), to correct an unsafe condition for certain
Embraer S.A. Model ERJ 190-100 IGW, -100 LR, -100 SR, -100 STD, -200
IGW, -200 LR, and -200 STD airplanes. Model ERJ 190-100 SR airplanes
are not certificated by the FAA and are not included on the U.S. type
certificate data sheet; this proposed AD therefore does not include
those airplanes in the applicability. The MCAI states that a quality
escape occurred during manufacturing concerning some ODS sensing
elements produced before January 31, 2021. A defective sensing
[[Page 57796]]
element may not be able to detect a thermal bleed leak, which is a
latent failure, and depending on the affected area, may start an
ignition source in the fuel tank, which could damage some electronic
boxes and expose the wing structure to high temperature gradients and
unexpected thermal loads, which could result in reduced structural
integrity of the airplane.
ANAC has informed the FAA of an undated Errata published to correct
a printing error in the English version of ANAC AD 2023-11-02. The FAA
has included these corrections in paragraphs (h)(2) and (3) of this AD.
The FAA is proposing 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-2024-1704.
Related Service Information Under 1 CFR Part 51
ANAC AD 2023-11-02 specifies procedures for a detailed inspection
of the ODS sensing elements of the airplane bleed lines and
replacement, if applicable, and procedures for re-activation of ODS
sensing elements that were deactivated during the detailed inspection.
ANAC AD 2023-11-02 also defines and prohibits the installation of an
affected ODS sensing element unless the affected part passed an
inspection, indicated by a marking on one face of the connector hex
nut.
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 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 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 require accomplishing the actions specified
in ANAC AD 2023-11-02 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 2023-11-02 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
ANAC AD 2023-11-02 in its entirety through that incorporation, except
for any differences identified as exceptions in the regulatory text of
this proposed AD. Service information required by ANAC AD 2023-11-02
for compliance will be available at regulations.gov under Docket No.
FAA-2024-1704 after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 90 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Labor cost Parts cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 26 work-hours x $85 per hour $0 Up to $2,210......... Up to $198,900.
= Up to $2,210.
----------------------------------------------------------------------------------------------------------------
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 action:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Cost per
Labor cost Parts cost product
------------------------------------------------------------------------
2 work-hours x $85 per hour = $170.... $500 $670
------------------------------------------------------------------------
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
[[Page 57797]]
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 adding the following new airworthiness
directive:
Embraer S.A. (Type Certificate Previously Held by Yabor[atilde]
Ind[uacute]stria Aeron[aacute]utica S.A.): Docket No. FAA-2024-1704;
Project Identifier MCAI-2023-01204-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 30, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Embraer S.A. (Type Certificate previously
held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.)
Model ERJ 190-100 IGW, -100 LR, -100 STD, -200 IGW, -200 LR, and -
200 STD airplanes, certificated in any category, as identified in
Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD
2023-11-02, effective November 21, 2023 (ANAC AD 2023-11-02).
(d) Subject
Air Transport Association (ATA) of America Code 28, Fuel.
(e) Unsafe Condition
This AD was prompted by a manufacturing quality escape
concerning certain overheat detection system (ODS) sensing elements.
The FAA is issuing this AD to address defective sensing elements.
The unsafe condition, if not addressed, could result in a sensing
element not being able to detect a thermal bleed leak, which is a
latent failure, and, depending on the affected area, may start an
ignition source in the fuel tank, which could damage some electronic
boxes and expose the wing structure to high temperature gradients
and unexpected thermal loads, which could result in reduced
structural integrity 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, ANAC AD 2023-11-02.
(h) Exceptions to ANAC AD 2023-11-02
(1) Where ANAC AD 2023-11-02 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where paragraph (b)(1) of ANAC AD 2023-11-02 specifies
``Within 5,000 Flight Hours (FH) or 24 months,'' for this AD,
replace that text with ``Within 7,500 Flight Hours (FH) or 36
months.''
(3) Where paragraphs (c)(1), (d)(1), (e)(1), (f)(1), and (g)(1)
of ANAC AD 2023-11-02 specify ``Within 5,000 FH or 24 months,'' for
this AD, replace that text with ``Within 7,500 FH or 36 months.''
(4) Where paragraphs (b)(1), (c)(1), (d)(1), (e)(1), (f)(1), and
(g)(1) of ANAC AD 2023-11-02 specify to inspect ODS sensing elements
at various locations, this AD requires adding ``in accordance with
Embraer Service Bulletin 190-36-0027, Revision 02, dated September
5, 2023; or later revisions approved by ANAC.''
(5) Where paragraphs (b) through (h) of ANAC AD 2023-11-02
specify on-condition actions based on the results of the ODS sensing
element inspections required by paragraphs (b)(1), (c)(1), (d)(1),
(e)(1), (f)(1), and(g)(1) of ANAC AD 2023-11-02, this AD requires
performing all applicable on-condition actions before further flight
after each inspection.
(6) This AD does not adopt paragraph (k) of ANAC AD 2023-11-02.
(7) Where paragraph (l) of ANAC AD 2023-11-02 specifies ``Record
compliance with this [ANAC] AD in the applicable maintenance log
book,'' for this AD, record compliance with this FAA AD.
(i) No Return of Parts Requirement
Although the service information referenced in ANAC AD 2023-11-
02 specifies to send removed parts to the manufacturer, this AD does
not include that requirement.
(j) Special Flight Permit
Special flight permits, as described in 14 CFR 21.197 and
21.199, are not allowed.
(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, mail it to the address identified
in paragraph (l)(1) 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.
(3) Required for Compliance (RC): Except as required by
paragraphs (i) and (k)(2) of this AD, if any service information
referenced in ANAC AD 2023-11-02 contains steps in the
Accomplishment Instructions or figures that are labeled as RC, the
instructions in RC steps, including subparagraphs under an RC step
and any figures identified in an RC step, must be done to comply
with this AD; any steps including substeps under those steps, that
are not identified as RC are recommended. The instructions in steps,
including substeps under those steps, not identified as RC may be
deviated from using accepted methods in accordance with the
operator's maintenance or inspection program without obtaining
approval of an AMOC, provided the instructions identified as RC can
be done and the airplane can be put back in an airworthy condition.
Any substitutions or changes to instructions identified as RC
require approval of an AMOC. If a step or substep is labeled ``RC
Exempt,'' then the RC requirement is removed from that step or
substep.
(l) Additional Information
(1) For more information about this AD, contact Joshua Bragg,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
WA 98198; phone: 817-222-5366; email: [email protected].
(2) For Kidde Aerospace & Defense material identified in ANAC AD
2023-11-02 that is not incorporated by reference, contact Kidde
Aerospace & Defense, 4200 Airport Drive NW, Building B, Wilson, NC
27896; telephone: 319-295-5000; website: kiddetechnologies.com/aviation.com.
(m) 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 this AD specifies otherwise.
(i) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
AD 2023-11-02, effective November 21, 2023.
(ii) [Reserved]
(3) For ANAC AD 2023-11-02, 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
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
[[Page 57798]]
Safety Branch, 2200 South 216th Street, 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 June 25, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-15309 Filed 7-15-24; 8:45 am]
BILLING CODE 4910-13-P