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PROPOSED AD EMBRAER S.A.: Docket No. FAA-2024-0455; Project Identifier MCAI-2023-00997-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    April 22, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies to Embraer S.A. Model EMB-550 and EMB-545 airplanes,
    certificated in any category,  as  identified  in  Agencia Nacional de
    Aviacao Civil  (ANAC)  AD  2023-08-03R01,  effective  November 2, 2023
    (ANAC AD 2023-08-03R01).

(d) SUBJECT

    Air Transport Association (ATA) of America Code 56, Windows.

(e) UNSAFE CONDITION

    This AD was prompted by  occurrences of premature cracks in  the outer
    layer of certain flight deck  side windows caused by interference  due
    to manufacturing  tolerances. The  FAA is  issuing this  AD to address
    cracks, delamination,  and any  other damage  of the  flight deck side
    windows. The unsafe condition, if not addressed, may subject the inner
    layer of the  window to unpredicted  loads for several  flights, which
    could   result   in   window   failure   and   subsequent    in-flight
    depressurization events.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIREMENTS

    Except as specified  in paragraph (h)  of this AD: Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, ANAC AD 2023-08-03R01.

(h) EXCEPTIONS TO ANAC AD 2023-08-03R01

(1) Where ANAC AD 2023-08-03R01 refers to its effective date,  this AD re-
    quires using the effective date of this AD.

(2) Where paragraph (b)(1)(i)  of  ANAC  AD 2023-08-03R01 says "In case of
    any crack in the outer layer is detected,  before the next flight, re-
    place the damaged window," for this AD,  replace that wording with "If
    any crack, delamination, or any other damage is found, before the next
    flight, replace the affected window."

(3) Where paragraph (b)(2)  of  ANAC AD 2023-08-03R01 says  "at each 2,000
    FC,"  for this AD,  replace that wording with "at intervals not to ex-
    ceed 2,000 FC."

(4) This AD does not adopt paragraph (d) of ANAC AD 2023-08-03R01.

(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  of  the International
    Validation Branch, mail it to the address identified in paragraph  (j)
    of this  AD. Information  may be  emailed to: AVS-AIR-730-AMOC@faa.gov
    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.

(2) Contacting the Manufacturer:  For any requirement in this AD to obtain
    instructions from a manufacturer,  the  instructions  must  be  accom-
    plished using a method approved by the Manager,  International Valida-
    tion Branch, FAA; or ANAC; or ANAC's authorized Designee.  If approved
    by the ANAC Designee, the approval must include the Designee's author-
    ized signature.

(j) ADDITIONAL INFORMATION

    For more information about this AD,  contact Hassan Ibrahim,  Aviation
    Safety Engineer,  FAA,  1600 Stewart Avenue,  Suite 410,  Westbury, NY
    11590; phone: 206-231-3653; email: hassan.m.ibrahim@faa.gov.

(k) 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) Agencia Nacional de Aviacao Civil (ANAC)  AD 2023-08-03R01,  effective
    November 2, 2023.

(ii) [Reserved].

(3) For ANAC AD 2023-08-03R01, contact ANAC, Aeronautical Products Certif-
    ication Branch (GGCP),  Rua Dr. Orlando Feirabend Filho,  230 - Centro
    Empresarial Aquarius-Torre B-Andares 14 a 18, Parque Residencial Aqua-
    rius, CEP 12.246-190-Sao Jose 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 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 Admin-
    istration (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 February 27, 2024.  Victor Wicklund, Deputy Director, Compliance
& Airworthiness Division, Aircraft Certification Service.

DATES: The FAA  must receive comments  on this proposed  AD  by  April 22,
2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0455; Project Identifier MCAI-2023-00997-T]
RIN 2120-AA64

Airworthiness Directives; Embraer 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 EMB-545 and EMB-550 airplanes. This
proposed AD was prompted by occurrences of premature cracks in the
outer layer of certain flight deck side windows caused by interference
due to manufacturing tolerances. This proposed AD would require initial
and repetitive inspections of the flight deck side windows and
applicable corrective actions, and would prohibit the installation of
affected flight deck side windows, as specified in an Ag[ecirc]ncia
Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD. 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 April 22,
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-2024-0455; 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 material that is proposed for IBR in this AD, contact
National Civil Aviation Agency (ANAC), Aeronautical Products
Certification Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230--
Centro Empresarial Aquarius--Torre B--Andares 14 a 18, Parque
Residencial Aquarius, CEP 12.246-190--Sao Jose 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-2024-0455.
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;
phone: 206-231-3653; email: hassan.m.ibrahim@faa.gov.

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-2024-0455; Project Identifier
MCAI-2023-00997-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
Hassan Ibrahim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone: 206-231-3653; email:
hassan.m.ibrahim@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 2023-08-03R01, effective November 2, 2023 (ANAC AD 2023-08-03R01)
(also referred to as the MCAI), to correct an unsafe condition for
Embraer S.A. Model EMB-550 and EMB-545 airplanes. The MCAI states
premature cracks have occurred in the outer layer of left-hand and right-hand
flight deck side windows with part number (P/N) NP-200402-7 or P/N NP-
200402-8, caused by interference due to manufacturing tolerances.
The FAA is proposing this AD to address cracks, delamination, and
any other damage with the affected left-hand and right-hand flight deck
side windows. The unsafe condition, if not addressed, may subject the
inner layer of the window to unpredicted loads for several flights,
which could result in window failure and subsequent in-flight
depressurization events.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-0455.

Related Service Information Under 1 CFR Part 51

ANAC AD 2023-08-03R01 specifies procedures for initial and
repetitive general visual inspections of the left-hand and right-hand
flight deck side windows to detect cracks, delamination, and any other
damage (such as scratches, chipping, erosion, and crazing). ANAC AD
2023-08-03R01 specifies replacing any cracked window with a new window
P/N NP-200402-9 or P/N NP-200402-10, as applicable. ANAC AD 2023-08-
03R01 also prohibits the installation of flight deck side windows with
P/N NP-200402-7 or P/N NP-200402-8, on any airplane.
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 2023-08-03R01 described previously, except as specified
under ``Difference Between this Proposed AD and the Service
Information,'' and 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 2023-08-03R01 by reference in the
FAA final rule. This proposed AD would, therefore, require compliance
with ANAC AD 2023-08-03R01 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-
08-03R01 for compliance will be available at regulations.gov under
Docket No. FAA-2024-0455 after the FAA final rule is published.

Costs of Compliance


The FAA estimates that this AD, if adopted as proposed, would
affect 44 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
1 work-hour x $85 per hour = $85
$0
$85
$3,740

The FAA estimates the following costs to do any necessary on-
condition actions 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 these on-condition actions:

Estimated Costs of On-Condition Actions

Labor cost
Parts cost
Cost per window
15 work-hours x $85 per hour = $1,2750
$21,636
$22,911

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed AD may be covered under warranty, thereby reducing the
cost impact on affected operators.

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

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]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: