Rule2022-11962
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
June 3, 2022
Effective
June 21, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. (Type Certificate previously held by Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer S.A.) Model ERJ 170- 200 STD, ERJ 170-200 LR, ERJ 170-200 SU, and ERJ 170-200 LL airplanes. This AD was prompted by a report of an in-flight detachment of a right- hand wing tip and the subsequent determination that cracks could develop on the wing tip connection area that can affect its structural integrity to the point of an in-flight detachment. This AD requires a detailed inspection for cracks of the affected wing tip connections, corrective action if necessary, and revision of the existing maintenance or inspection program, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is incorporated by reference. The FAA previously sent an emergency AD to all known U.S. owners and operators of these airplanes. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
<html>
<head>
<title>Federal Register, Volume 87 Issue 107 (Friday, June 3, 2022)</title>
</head>
<body><pre>
[Federal Register Volume 87, Number 107 (Friday, June 3, 2022)]
[Rules and Regulations]
[Pages 33623-33627]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-11962]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0597; Project Identifier MCAI-2022-00638-T;
Amendment 39-22074; AD 2022-11-51]
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), DOT.
[[Page 33624]]
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Embraer S.A. (Type Certificate previously held by Yabor[atilde]
Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer S.A.) Model ERJ 170-
200 STD, ERJ 170-200 LR, ERJ 170-200 SU, and ERJ 170-200 LL airplanes.
This AD was prompted by a report of an in-flight detachment of a right-
hand wing tip and the subsequent determination that cracks could
develop on the wing tip connection area that can affect its structural
integrity to the point of an in-flight detachment. This AD requires a
detailed inspection for cracks of the affected wing tip connections,
corrective action if necessary, and revision of the existing
maintenance or inspection program, as specified in an Ag[ecirc]ncia
Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is
incorporated by reference. The FAA previously sent an emergency AD to
all known U.S. owners and operators of these airplanes. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective on June 21, 2022. Emergency AD 2022-11-51,
issued on May 13, 2022, which contained the requirements of this
amendment, was effective with actual notice.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 21,
2022.
The FAA must receive comments on this AD by July 18, 2022.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="https://www.regulations.gov">https://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
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 <a href="/cdn-cgi/l/email-protection#1f6f7e7c5f7e717e7c31787069317d6d"><span class="__cf_email__" data-cfemail="0d7d6c6e4d6c636c6e236a627b236f7f">[email protected]</span></a>; internet <a href="http://www.anac.gov">www.anac.gov</a>.br/en/. You may find
this IBR material on the ANAC website at <a href="https://sistemas.anac.gov.br/certificacao/DA/DAE.asp">https://sistemas.anac.gov.br/certificacao/DA/DAE.asp</a>. You may view this service information at the
FAA, Transport Standards 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 on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0597.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0597; 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 street
address for Docket Operations is listed above. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Krista Greer, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3221; email
<a href="/cdn-cgi/l/email-protection#bef5ccd7cdcadf90f9ccdbdbccfed8dfdf90d9d1c8"><span class="__cf_email__" data-cfemail="b8f3cad1cbccd996ffcaddddcaf8ded9d996dfd7ce">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2022-0597; Project Identifier MCAI-
2022-00638-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, 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 final rule because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="https://www.regulations.gov">https://www.regulations.gov</a>, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this final rule.
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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Krista
Greer, Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3221; email <a href="/cdn-cgi/l/email-protection#743f061d0700155a3306111106341215155a131b02"><span class="__cf_email__" data-cfemail="c388b1aab0b7a2ed84b1a6a6b183a5a2a2eda4acb5">[email protected]</span></a>. Any commentary that
the FAA receives that is not specifically designated as CBI will be
placed in the public docket for this rulemaking.
Background
The FAA issued Emergency AD 2022-11-51, dated May 13, 2022 (the
emergency AD), to address an unsafe condition on Embraer S.A. Model ERJ
170-200 STD, ERJ 170-200 LR, ERJ 170-200 SU, and ERJ 170-200 LL
airplanes. The FAA sent the emergency AD to all known U.S. owners and
operators of these airplanes. The emergency AD requires a detailed
inspection for cracks of the affected wing tip connections, corrective
action if cracks are found, and revision of the existing maintenance or
inspection program to include a revised threshold and interval for a
certain airworthiness limitations task.
The emergency AD was prompted by Emergency AD 2022-05-02, effective
May 13, 2022 (ANAC Emergency AD 2022-05-02) (also referred to after
this as the Mandatory Continuing Airworthiness Information, or the
MCAI), issued by ANAC, which is the aviation authority for Brazil, to
correct the unsafe condition for certain Embraer S.A. Model ERJ 170-200
STD, ERJ 170-200 LR, ERJ 170-200 SU, and ERJ 170-200 LL airplanes. ANAC
Emergency AD 2022-05-02 was prompted by a report of an in-flight
detachment of a right-hand wing tip. Subsequently it was determined
that cracks could develop on the wing tip connection area that can
affect its structural integrity to the point of an in-flight
detachment. This condition, if not addressed, even if sufficient
controllability of the airplane is maintained for the safe continuation
of the flight, could result in the
[[Page 33625]]
detached part damaging other airplane parts and affecting
controllability, as well as damaging property and injuring persons on
the ground.
See the MCAI for additional background information.
Related Service Information Under 1 CFR Part 51
ANAC Emergency AD 2022-05-02 specifies procedures for a detailed
inspection for cracks of the affected wing tip connections, corrective
action including rework of the wing spar 1 or repair/modification of
the wingtip spar 1, and revision of the existing maintenance or
inspection program to include a revised threshold and interval for a
certain airworthiness limitations task. This service information is
reasonably available because the interested parties have access to it
through their normal course of business or by the means identified in
the ADDRESSES section.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
described above. The FAA is issuing this AD after determining that the
unsafe condition described previously is likely to exist or develop on
other products of the same type design.
AD Requirements
This AD requires accomplishing the actions specified in ANAC
Emergency AD 2022-05-02 described previously, except for any
differences identified as exceptions in the regulatory text of this AD
and except as discussed under ``Difference Between this AD and the
MCAI.''
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,
ANAC Emergency AD 2022-05-02 is incorporated by reference in this AD.
This AD requires compliance with ANAC Emergency AD 2022-05-02 in its
entirety through that incorporation, except for any differences
identified as exceptions in the regulatory text of this AD. Using
common terms that are the same as the heading of a particular section
in ANAC Emergency AD 2022-05-02 does not mean that operators need
comply only with that section. For example, where the AD refers to
required actions and compliance, compliance with these AD requirements
is not limited to the section titled ``Required Action'' or
``Compliance'' in ANAC Emergency AD 2022-05-02. Service information
required by ANAC Emergency AD 2022-05-02 for compliance will be
available at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating
Docket No. FAA-2022-0597 after this AD is published.
Difference Between This AD and the MCAI
This AD requires all operators to revise the existing maintenance
or inspection program, as applicable, to include a reduced threshold
and interval for a certain airworthiness limitations task. The MCAI
does not require this action for airplanes with less than 7,500 flight
hours after installation of an affected part number.
Interim Action
The FAA considers this AD interim action. The inspection reports
that are required by this AD will enable the manufacturer to obtain
better insight into the nature, cause, and extent of the cracking, and
eventually to develop final action to address the unsafe condition.
Once final action has been identified, the FAA might consider further
rulemaking.
FAA's Justification and Determination of the Effective Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
An unsafe condition exists that required the immediate adoption of
Emergency AD 2022-11-51 issued on May 13, 2022, to all known U.S.
owners and operators of these airplanes. The FAA found that the risk to
the flying public justified waiving notice and comment prior to
adoption of this rule because cracks on the wing tip connection area
can affect its structural integrity to the point of an in-flight
detachment. Even if sufficient controllability of the airplane is
maintained for the safe continuation of the flight, this condition
could result in the detached part damaging other airplane parts and
affecting controllability, as well as damaging property and injuring
persons on the ground. These conditions still exist, and the AD is
hereby published in the Federal Register as an amendment to 14 CFR
39.13 to make it effective to all persons. Given the significance of
the risk presented by this unsafe condition, it must be immediately
addressed. Accordingly, notice and opportunity for prior public comment
are impracticable and contrary to the public interest pursuant to 5
U.S.C. 553(b)(3)(B). In addition, the FAA finds that good cause exists
pursuant to 5 U.S.C. 553(d) for making this amendment effective in less
than 30 days, for the same reasons the FAA found good cause to forgo
notice and comment.
Regulatory Flexibility Act (RFA)
The requirements of the RFA do not apply when an agency finds good
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and
comment. Because the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 115 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspections....................... 6 work-hours x $85 per $0 $510 $58,650
hour = $510.
----------------------------------------------------------------------------------------------------------------
[[Page 33626]]
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
FAA 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. Therefore, the
FAA estimates the total cost per operator to be $7,650 (90 work-hours x
$85 per work-hour).
The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of the
inspections. The FAA has no way of determining the number of aircraft
that might need these actions:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Reporting.................................. 1 work-hour x $85 per hour = $85... $0 $85
Wing spar 1 rework (per side).............. 49 work-hours x $85 per hour = 2,212 6,377
$4,165.
Wingtip spar 1 repair/modification (per 111 work-hours x $85 per hour = 16,949 26,384
side). $9,435.
----------------------------------------------------------------------------------------------------------------
Paperwork Reduction Act
A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of
information displays a current valid OMB control number. The control
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in
the Costs of Compliance section of this document and includes time for
reviewing instructions, as well as completing and reviewing the
collection of information. Therefore, all reporting associated with
this AD is mandatory. Comments concerning the accuracy of this burden
and suggestions for reducing the burden should be directed to
Information Collection Clearance Officer, Federal Aviation
Administration, 10101 Hillwood Parkway, Fort Worth, TX 76177-1524.
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, and
(2) Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of 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 adding the following new airworthiness
directive:
2022-11-51 Embraer S.A. (Type Certificate Previously Held by
Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.; Embraer
S.A.): Amendment 39-22074; Docket No. FAA-2022-0597; Project
Identifier MCAI-2022-00638-T.
(a) Effective Date
The FAA issued Emergency Airworthiness Directive (AD) 2022-11-51
on May 13, 2022, directly to affected owners and operators. As a
result of such actual notice, the emergency AD was effective for
those owners and operators on the date it was provided. This AD
contains the same requirements as that emergency AD and, for those
who did not receive actual notice, is effective on June 21, 2022.
(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.;
Embraer S.A.) Model ERJ 170-200 STD, ERJ 170-200 LR, ERJ 170-200 SU,
and ERJ 170-200 LL airplanes, certificated in any category, as
identified in Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil
(ANAC) Emergency AD 2022-05-02, effective May 13, 2022 (ANAC
Emergency AD 2022-05-02).
(d) Subject
Air Transport Association (ATA) of America Code 57, Wing
structure.
(e) Unsafe Condition
This AD was prompted by a report of an in-flight detachment of a
right-hand wing tip. Subsequently it was determined that cracks
could develop on the wing tip connection area that can affect its
structural integrity to the point of an in-flight detachment. The
FAA is issuing this AD to address this condition, which, even if
sufficient controllability of the airplane is maintained for the
safe continuation of the flight, could result in the detached part
damaging other airplane parts and affecting controllability, as well
as damaging property and injuring persons on the ground.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, ANAC Emergency AD 2022-05-02.
[[Page 33627]]
(h) Exceptions to ANAC Emergency AD 2022-05-02
(1) Where ANAC Emergency AD 2022-05-02 refers to its effective
date, this AD requires using the effective date of this AD.
(2) For the first column heading of table 1--``Compliance
Times'' of ANAC Emergency AD 2022-05-02, replace ``Flight Hours (FH)
accumulated from installation of affected PN'' with ``Flight Hours
(FH) accumulated from installation of affected PN as of the
effective date of this (FAA) AD.''
(3) Where table 1--``Compliance Times'' of ANAC Emergency AD
2022-05-02 specifies flight hours of ``19.800 or greater,'' for this
AD use flight hours of ``19.800 or greater.''
(4) Where paragraphs (a)(i) and (a)(ii) of ANAC Emergency AD
2022-05-02 specify correcting ``discrepancies,'' this AD defines a
discrepancy as a crack.
(5) The inspections and corrective actions specified in
paragraphs (a)(i) and (a)(ii) of ANAC Emergency AD 2022-05-02 must
be done using the service information specified in paragraphs (a)(i)
and (a)(ii) of ANAC Emergency AD 2022-05-02.
(6) Where paragraph (a)(iii) of ANAC Emergency AD 2022-05-02
specifies to ``Modify task 57-30-002-0002 of the Airworthiness
Limitations Section, on MRB 1621, APPENDIX A--PART 2--AIRWORTHINESS
LIMITATION INSPECTIONS (ALI)--STRUCTURES, to revise its compliance
interval'' at the times in table 1--``Compliance Times'' of ANAC
Emergency AD 2022-05-02, this AD requires revising the existing
maintenance or inspection program, as applicable, within 30 days
after the effective date of this AD to incorporate the information
specified in table 2--``Airworthiness Limitations Section Updates''
of ANAC Emergency AD 2022-05-02; except do not include the
information in the ``Current Threshold/Interval'' column. The
initial compliance time for the airworthiness limitations task is
within 1,000 flight hours after accomplishment of the tasks
specified in paragraphs (a)(i) and (a)(ii) of ANAC Emergency AD
2022-05-02; except, for airplanes that have accumulated 7,499 flight
hours or less from installation of an affected part number, as
defined in ANAC Emergency AD 2022-05-02, the initial compliance time
is before the accumulation of 10,000 flight hours from installation
of the affected part number.
(7) Paragraph (b) of ANAC Emergency AD 2022-05-02 specifies to
report crack findings to Embraer and ANAC within a certain
compliance time. For this AD, report crack findings at the
applicable time specified in paragraph (h)(7)(i) or (ii) of this AD.
(i) If the inspection was done on or after the effective date of
this AD: Submit the report within 36 hours after accomplishment of
the inspection.
(ii) If the inspection was done before the effective date of
this AD: Submit the report within 36 hours after the effective date
of this AD.
(8) The ``Alternative method of compliance (AMOC)'' section of
ANAC Emergency AD 2022-05-02 does not apply to this AD.
(i) Other 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 (j) of this
AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#d7eefa968184fa969e85fae0e4e7fa969a989497b1b6b6f9b0b8a1"><span class="__cf_email__" data-cfemail="192034584f4a3458504b342e2a29345854565a597f7878377e766f">[email protected]</span></a>.
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, 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.
(j) Related Information
For more information about this AD, contact Krista Greer,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3221; email <a href="/cdn-cgi/l/email-protection#206b52495354410e6752454552604641410e474f56"><span class="__cf_email__" data-cfemail="8ac1f8e3f9feeba4cdf8efeff8caecebeba4ede5fc">[email protected]</span></a>.
(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) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC)
Emergency AD 2022-05-02, effective May 13, 2022.
(ii) [Reserved]
(3) For ANAC Emergency AD 2022-05-02, 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:
<a href="/cdn-cgi/l/email-protection#f6869795b697989795d8919980d89484"><span class="__cf_email__" data-cfemail="7c0c1d1f3c1d121d1f521b130a521e0e">[email protected]</span></a>; internet <a href="http://www.anac.gov">www.anac.gov</a>.br/en/. You may find this IBR
material on the ANAC website at <a href="https://sistemas.anac.gov.br/certificacao/DA/DAE.asp">https://sistemas.anac.gov.br/certificacao/DA/DAE.asp</a>.
(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 service information 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#aaccd884c3c4d9dacfc9dec3c5c4eac4cbd8cb84cdc5dc"><span class="__cf_email__" data-cfemail="dbbda9f5b2b5a8abbeb8afb2b4b59bb5baa9baf5bcb4ad">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on May 26, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-11962 Filed 6-2-22; 8:45 am]
BILLING CODE 4910-13-P
</pre><script data-cfasync="false" src="/cdn-cgi/scripts/5c5dd728/cloudflare-static/email-decode.min.js"></script></body>
</html>Indexed from Federal Register on June 3, 2022.
This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.