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2022-21-08 EMBRAER S.A.: Amendment 39-22207; Docket No. FAA-2022-0984; Project Identifier MCAI-2022-00236-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective December 22, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Embraer S.A.  Model EMB-545 airplanes, certificated
    in any category,  as  identified  in Agencia Nacional de Aviacao Civil
    (ANAC) AD 2022-02-02, effective February 23, 2022 (ANAC AD 2022-02-02)

(d) SUBJECT

    Air Transport Association (ATA) of America Code 27, Flight Controls.

(e) UNSAFE CONDITION

    This AD was  prompted by an  error that was  detected in the  airplane
    takeoff configuration  warning logic.  The error  prevents the  system
    from sounding an aural alert "No Takeoff Trim" for the flightcrew,  if
    the pitch trim is  in a position that  would not allow a  safe takeoff
    (positioned out of the green band indication). The FAA is issuing this
    AD to address the lack of  sound aural alert "No Takeoff Trim"  to the
    flightcrew on a possibly misconfigured airplane, which could result in
    loss of airplane controllability.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready 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 accord-
    ance with, ANAC AD 2022-02-02.

(h) EXCEPTIONS TO ANAC AD 2022-02-02

(1) Where ANAC AD 2022-02-02  refers  to  its  effective date, this AD re-
    quires using the effective date of this AD.

(2) The "Alternative methods of compliance (AMOC)" section of ANAC AD 2022
    -02-02 does not apply to this AD.

(3) Where paragraph (b) of ANAC AD 2022-02-02  specifies acceptable higher
    software versions,  replace "For higher software versions, use the ap-
    plicable Service Bulletin  recommended by  the Manufacturer" with "For
    higher software versions, use the applicable Service Bulletin approved
    by ANAC and recommended by the Manufacturer."

(i) NO REPORTING REQUIRED

    Although  the service  information  referenced  in ANAC  AD 2022-02-02
    specifies to submit certain  information to the manufacturer,  this AD
    does not include that requirement.

(j) ADDITIONAL AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Validation Branch, FAA,  has the authority  to approve AMOCs  for this
    AD,  if requested  using  the  procedures found  in 14  CFR 39.19.  In
    accordance with  14 CFR  39.19, send  your request  to your  principal
    inspector or responsible Flight  Standards Office, as appropriate.  If
    sending information directly  to the International  Validation Branch,
    send it to the attention of the person identified in paragraph (k)  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.

(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.

(k) ADDITIONAL INFORMATION

    For more information about this AD,  contact Hassan Ibrahim, Aerospace
    Engineer, Large Aircraft Section, FAA, International Validation Branch
    2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3653; e-
    mail Hassan.M.Ibrahim@faa.gov.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference of the service information  listed in this paragraph under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable  to do the actions
    required by this AD, unless this AD specifies otherwise.

(i) Agencia Nacional de Aviacao Civil (ANAC) AD 2022-02-02, effective Feb-
    ruary 23, 2022.

(ii) [Reserved]

(3) For ANAC AD 2022-02-02, contact ANAC, Aeronautical Products Certifica-
    tion Branch (GGCP),  Rua Dr. Orlando Feirabend Filho, 230 – Centro Em-
    presarial 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 ANAC AD  on  the  ANAC website  at sistemas.anac.gov.br/
    certificacao/DA/DAE.asp.

(4) You may view this material at the FAA, Airworthiness Products Section,
    Operational Safety Branch, 2200 South 216th St.,  Des Moines, WA.  For
    information on the availability of this material at the FAA, call 206-
    231-3195.

(5) You may view  this material  that is incorporated  by reference at the
    National Archives and Records Administration (NARA).  For  information
    on the availability of this material at NARA, email fr.inspection@nara
    .gov or go to: www.archives.gov/federalregister/cfr/ibr-locations.html

Issued on October 3, 2022.Christina Underwood, Acting Director, Compliance
& Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Hassan Ibrahim, Aerospace Engineer, Large
Aircraft Section, FAA,  International Validation Branch,  2200 South 216th
St., Des Moines, WA 98198; telephone 206-231-3653; email Hassan.M.Ibrahim@
faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2022-0984; Project Identifier MCAI-2022-00236-T;
Amendment 39-22207; AD 2022-21-08]
RIN 2120-AA64

Airworthiness Directives; Embraer S.A. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Embraer S.A. Model EMB-545 airplanes. This AD was prompted by
an error that was detected in the airplane takeoff configuration
warning logic. The error prevents the system from sounding an aural
alert ``No Takeoff Trim'' for the flightcrew. This AD requires the
installation of a new software version of engine indication and crew
alert system (EICAS), as specified in an Ag[ecirc]ncia Nacional de
Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by
reference. The FAA is issuing this AD to address the unsafe condition
on these products.

DATES: This AD is effective December 22, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 22,
2022.

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-0984; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For material incorporated by reference (IBR) 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 pac@anac.gov.br; website anac.gov.br/en/. You may find this
IBR material on the ANAC website at sistemas.anac.gov.br/certificacao/
DA/DAE.asp.
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. It is also available in the AD docket at
regulations.gov under Docket No. FAA-2022-0984.

FOR FURTHER INFORMATION CONTACT: Hassan Ibrahim, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3653; email
Hassan.M.Ibrahim@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Embraer S.A.
Model EMB-545 airplanes. The NPRM published in the Federal Register on
July 29, 2022 (87 FR 45707). The NPRM was prompted by AD 2022-02-02,
effective February 23, 2022, issued by ANAC, which is the aviation
authority for Brazil (referred to after this as the MCAI). The MCAI
states that an error was detected in the airplane takeoff configuration
warning logic. The error prevents the system from sounding an aural
alert ``No Takeoff Trim'' for the flightcrew, if the pitch trim is in a
position that would not allow a safe takeoff (positioned out of the
green band indication).
In the NPRM, the FAA proposed to require installation of a new
software version of EICAS, as specified in ANAC
AD 2022-02-02. The FAA is issuing this AD to address the lack of sound
aural alert ``No Takeoff Trim'' to the flightcrew on a possibly
misconfigured airplane, which could result in loss of airplane
controllability.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-0984.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

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 reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.

Related Service Information Under 1 CFR Part 51

ANAC AD 2022-02-02 specifies procedures for installation of a new
software version of EICAS.
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.

Costs of Compliance

The FAA estimates that this AD affects 41 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions

Labor cost
Parts cost Cost per product Cost on U.S. operators
3.5 work-hours x $85 per hour * = $297.50
.........
$297.50
$12,197.50

* The FAA has received no definitive data on which to base the cost estimates
for the parts specified in this AD.

According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in the cost estimate.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.

Regulatory Findings

This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will 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 Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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: