Rule2022-27404
Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) 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
December 19, 2022
Effective
January 23, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2019-25- 16, which applied to certain Embraer S.A. Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU airplanes; and Model ERJ 170-200 LR, -200 SU, -200 STD, and -200 LL airplanes. AD 2019-25-16 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by the determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2019-25-16 and requires revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive airworthiness limitations and certain structural modifications, 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.
Full Text
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<title>Federal Register, Volume 87 Issue 242 (Monday, December 19, 2022)</title>
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[Federal Register Volume 87, Number 242 (Monday, December 19, 2022)]
[Rules and Regulations]
[Pages 77493-77497]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-27404]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0979; Project Identifier MCAI-2022-00171-T;
Amendment 39-22263; AD 2022-25-07]
RIN 2120-AA64
Airworthiness Directives; Embraer S.A. (Type Certificate
Previously Held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica
S.A.; Embraer S.A.) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-25-
16, which applied to certain Embraer S.A. Model ERJ 170-100 LR, -100
STD, -100 SE, and -100 SU airplanes; and Model ERJ 170-200 LR, -200 SU,
-200 STD, and -200 LL airplanes. AD 2019-25-16 required revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations. This AD
was prompted by the determination that new or more restrictive
airworthiness limitations are necessary. This AD continues to require
the actions in AD 2019-25-16 and requires revising the existing
maintenance or inspection program, as applicable, to incorporate
additional new or more restrictive airworthiness limitations and
certain structural modifications, 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
[[Page 77494]]
to address the unsafe condition on these products.
DATES: This AD is effective January 23, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 23,
2023.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of
February 10, 2020 (85 FR 453, January 6, 2020).
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0979; 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:
<bullet> For material incorporated by reference 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#02726361423e63226a7067643f" 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.
<bullet> For Embraer service information identified in this final
rule, 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#57333e2423253e3517323a35253632257934383a793525"><span class="__cf_email__" data-cfemail="17737e6463657e7557727a75657672653974787a397565">[email protected]</span></a>; internet
<a href="http://flyembraer.com">flyembraer.com</a>.
<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. It is also available in the AD docket at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-0979.
FOR FURTHER INFORMATION CONTACT: Allison Buss, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 303-342-1090; email
<a href="/cdn-cgi/l/email-protection#20414c4c49534f4e0e4a0e42555353604641410e474f56"><span class="__cf_email__" data-cfemail="b7d6dbdbdec4d8d999dd99d5c2c4c4f7d1d6d699d0d8c1">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-25-16, Amendment 39-21015 (85 FR 453,
January 6, 2020) (AD 2019-25-16). AD 2019-25-16 applied to certain
Embraer S.A. Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU
airplanes; and Model ERJ 170-200 LR, -200 SU, -200 STD, and 200 LL
airplanes. AD 2019-25-16 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations; and added airplanes to the
applicability. The FAA issued AD 2019-25-16 to address fatigue cracking
of various principal structural elements (PSEs); such cracking could
result in reduced structural integrity of the airplane and to prevent
safety significant latent failures; such failures, in combination with
one or more other specified failures or events, could result in a
hazardous or catastrophic failure condition of avionics, hydraulic
systems, fire detection systems, fuel systems, or other critical
systems. Furthermore, the FAA issued AD 2019-25-16 to address potential
ignition sources inside fuel tanks caused by latent failures,
alterations, repairs, or maintenance actions; such failures, in
combination with flammable fuel vapors, could result in fuel tank
explosions and consequent loss of the airplane.
The NPRM published in the Federal Register on July 28, 2022 (87 FR
45284). The NPRM was prompted by AD 2022-02-01, effective February 9,
2022, issued by ANAC (referred to after this as the MCAI) (ANAC AD
2022-02-01). The MCAI states that it was prompted by a determination
that new or more restrictive airworthiness limitations are necessary.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0979.
In the NPRM, the FAA proposed to continue to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations and
certain structural modifications, as specified in ANAC AD 2022-02-01.
The FAA is issuing this AD to address the unsafe condition on these
products.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Horizon Air. The following presents
the comment received on the NPRM and the FAA's response.
Request To Update the Required Service Information
Horizon Air requested that the Embraer 170/175 Maintenance Review
Board Report, MRB 1621, Revision 17, dated July 01, 2021, referenced in
ANAC AD 2022-02-01, be updated to Embraer 170/175 Maintenance Review
Board Report, MRB 1621, Revision 18, dated July 4, 2022.
The FAA confirms that it intends to allow the use of applicable
later MRB revisions to comply with the requirements of this AD. This AD
refers to ANAC AD 2022-02-01 as the appropriate source of service
information for accomplishing the required actions. Paragraph (f) of
ANAC AD 2022-02-01 accepts the use of later approved revisions of the
referenced MRB document for compliance. Therefore, applicable later
approved MRB revisions are acceptable for compliance with this AD. No
change to the AD is required.
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, considered the
comment received, 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 2022-02-01 describes new or more restrictive airworthiness
limitations for airplane structures and the incorporation of certain
structural modifications (i.e., reinforcement of left-hand (LH) and
right-hand (RH) wing spar II lower; and reinforcement of the wing lower
skin chordwise splices of LH and RH wing) before the defined structural
modifications points (SMP).
This AD also requires Appendix A--Airworthiness Limitations of
EMBRAER
[[Page 77495]]
170/175 Maintenance Review Board Report (MRBR), MRB-1621, Revision 14,
dated September 27, 2018; and Embraer Temporary Revision (TR) 14-1,
dated November 13, 2018, to Part 4-Life-Limited Items, of Appendix A of
EMBRAER 170/175 Maintenance Review Board Report (MRBR), MRB-1621,
Revision 14, dated September 27, 2018; which the Director of the
Federal Register approved for incorporation by reference as of February
10, 2020 (85 FR 453).
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 662 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2019-25-16 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. Since operators incorporate maintenance or inspection
program changes for their affected fleet(s), the FAA has determined
that a per-operator estimate is more accurate than a per-airplane
estimate.
The FAA estimates the total cost per operator for the new revision
to the existing maintenance or inspection program to be $7,650 (90
work-hours x $85 per work-hour).
Estimated Costs for Required Actions *
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
New proposed actions................ 196 work-hours x $85 $98,860 $115,520 $76,474,240
per hour = $16,660.
----------------------------------------------------------------------------------------------------------------
* Table does not include estimated costs for revising the existing maintenance or inspection program.
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 operators. The FAA does not control warranty coverage for
affected operators. 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
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 2019-25-16, Amendment 39-21015 (85
FR 453, January 6, 2020); and
0
b. Adding the following new airworthiness directive:
2022-25-07 Embraer S.A. (Type Certificate Previously Held by
Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer
S.A.): Amendment 39-22263; Docket No. FAA-2022-0979; Project
Identifier MCAI-2022-00171-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 23, 2023.
(b) Affected ADs
This AD replaces AD 2019-25-16, Amendment 39-21015 (85 FR 453,
January 6, 2020) (AD 2019-25-16).
(c) Applicability
This AD applies to all Embraer S.A. Model ERJ 170-100 LR, -100
STD, -100 SE, and -100 SU airplanes; and Model ERJ 170-200 LR, -200
SU, -200 STD, and -200 LL airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks; 27, Flight controls; 28, Fuel; 52, Doors; 53,
Fuselage; 54, Nacelles/pylons; 55, Stabilizers; 57, Wings; 71,
Powerplant; and 78, Exhaust.
(e) Unsafe Condition
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address fatigue cracking of various principal
structural elements (PSEs); such cracking could result in reduced
structural integrity of the airplane. The FAA is also issuing this
AD to address safety significant latent failures; such failures, in
combination with one or more other specified failures or events,
could result in a hazardous or catastrophic failure condition of
avionics, hydraulic systems, fire detection systems, fuel systems,
or other critical systems. Furthermore, the FAA is issuing this AD
to address potential ignition sources inside fuel tanks caused by
latent failures, alterations, repairs, or maintenance actions; such
failures, in combination with flammable fuel vapors, could result in
fuel tank explosions and consequent loss of the airplane.
[[Page 77496]]
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Revision of the Existing Maintenance or Inspection
Program, With No Changes
This paragraph restates the requirements of paragraph (i) of AD
2019-25-16, with no changes. For Model ERJ 170-100 LR, -100 STD, -
100 SE, and -100 SU airplanes; and Model ERJ 170-200 LR, -200 SU, -
200 STD, and -200LL airplanes; manufacturer serial numbers 17000002,
17000004 through 17000013 inclusive, and 17000015 through 17000761
inclusive: Within 90 days after February 10, 2020 (the effective
date of AD 2019-25-16), revise the existing maintenance or
inspection program, as applicable, to incorporate the information
specified in Part 1-Certification Maintenance Requirements, Part 2-
Airworthiness Limitation Inspections (ALI)-Structures, Part 3-Fuel
System Limitation Items, and Part 4-Life Limited Items; and EMBRAER
Temporary Revision (TR) 14-1, dated November 13, 2018, to part 4-
Life Limited Items; of Appendix A of the EMBRAER 170/175 MRBR, MRB-
1621, Revision 14, dated September 27, 2018 (EMBRAER 170/175 MRB-
1621, Revision 14). The initial compliance time for doing the tasks
is at the later of the times specified in paragraphs (g)(1) and (2)
of this AD.
(1) Within the applicable times specified in EMBRAER 170/175
MRB-1621, Revision 14. For the purposes of this AD, the initial
compliance times (identified as ``Threshold'' or ``T'' in EMBRAER
170/175 MRB-1621, Revision 14) are expressed in ``total flight
cycles'' or ``total flight hours,'' as applicable.
(2) Within 90 days or 600 flight cycles after February 10, 2020
(the effective date of AD 2019-25-16), whichever occurs later.
(h) Retained Restrictions on Alternative Actions, Intervals, and
CDCCLs, With No Changes
This paragraph restates the requirements of paragraph (j) of AD
2019-25-16, with no changes. Except as required by paragraph (i) of
this AD: After the existing maintenance or inspection program has
been revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections), intervals, or CDCCLs may be used unless
the actions, intervals, and CDCCLs are approved as an AMOC in
accordance with the procedures specified in paragraph (l)(1) of this
AD.
(i) New Revision of the Existing Maintenance or Inspection Program
Except as specified in paragraph (j) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, ANAC AD 2022-02-01, effective February 9, 2022
(ANAC AD 2022-02-01). Accomplishing the revision of the existing
maintenance or inspection program required by this paragraph
terminates the requirements for Part 2--Airworthiness Limitation
Inspections (ALI)-Structures specified in paragraph (g) of this AD
only.
(j) Exceptions to ANAC AD 2022-02-01
(1) Where ANAC AD 2022-02-01 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Alternative method of compliance (AMOC)'' section of
ANAC AD 2022-02-01 does not apply to this AD.
(3) Where paragraph (b)(1) of ANAC AD 2022-02-01 specifies
incorporating all airworthiness limitations in Part 2 of the service
information specified in paragraph (b)(1) of ANAC AD 2022-02-01, for
this AD, do not incorporate the threshold and interval for
maintenance review board report (MRBR) task number 57-30-002-0002,
``Enhanced Wingtip to Wing Spar Attachments--Internal.''
Note 1 to paragraph (j)(3): AD 2022-11-51, Amendment 39-22074
(87 FR 33623, June 3, 2022) (AD 2022-11-51), requires, among other
actions, incorporating alternate thresholds and intervals for MRBR
task number 57-30-002-0002. The airplanes affected by MRBR task
number 57-30-002-0002 are identified in paragraph (c) of AD 2022-11-
51.
(k) New Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (i) of this AD, no alternative
actions (e.g., inspections), intervals, and CDCCLs are allowed
unless they are approved as specified in paragraph (f) of ANAC AD
2022-02-01.
(l) Additional FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, 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 Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (m) of this
AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#241d0965727709656d76091317140965696b67644245450a434b52"><span class="__cf_email__" data-cfemail="caf3e78b9c99e78b8398e7fdf9fae78b8785898aacababe4ada5bc">[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 2019-25-16 are approved as
AMOCs for the corresponding provisions of 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, Large Aircraft
Section, 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
paragraph (l)(2) of this AD, if any service information referenced
in ANAC AD 2022-02-01 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.
(m) Additional Information
For more information about this AD, contact Allison Buss,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 303-342-1090; email <a href="/cdn-cgi/l/email-protection#f6979a9a9f859998d89cd894838585b6909797d8919980"><span class="__cf_email__" data-cfemail="b0d1dcdcd9c3dfde9eda9ed2c5c3c3f0d6d1d19ed7dfc6">[email protected]</span></a>.
(n) 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 2022-02-01, effective February 9, 2022.
(ii) [Reserved]
(3) The following service information was approved for IBR on
February 10, 2020 (85 FR 453, January 6, 2020).
(i) Appendix A--Airworthiness Limitations of EMBRAER 170/175
Maintenance Review Board Report (MRBR), MRB-1621, Revision 14, dated
September 27, 2018.
(ii) Embraer Temporary Revision (TR) 14-1, dated November 13,
2018, to Part 4-Life-Limited Items, of Appendix A of EMBRAER 170/175
Maintenance Review Board Report (MRBR), MRB-1621, Revision 14, dated
September 27, 2018.
(4) For ANAC AD 2022-02-01, 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#5e2e3f3d1e623f7e362c3b3863" 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 ANAC AD
on the ANAC website at <a href="http://sistemas.anac.gov">sistemas.anac.gov</a>.br/certificacao/DA/DAE.asp.
(5) For Embraer material, 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;
[[Page 77497]]
email <a href="/cdn-cgi/l/email-protection#a2c6cbd1d6d0cbc0e2c7cfc0d0c3c7d08cc1cdcf8cc0d0"><span class="__cf_email__" data-cfemail="e5818c9691978c87a580888797848097cb868a88cb8797">[email protected]</span></a>; internet <a href="http://flyembraer.com">flyembraer.com</a>.
(6) 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.
(7) 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
<a href="/cdn-cgi/l/email-protection#3553471b5c5b46455056415c5a5b755b5447541b525a43"><span class="__cf_email__" data-cfemail="8aecf8a4e3e4f9faefe9fee3e5e4cae4ebf8eba4ede5fc">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on November 29, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-27404 Filed 12-16-22; 8:45 am]
BILLING CODE 4910-13-P
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