DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0584; Product Identifier 2020-NM-069-AD]
RIN 2120-AA64
Airworthiness Directives; Embraer S.A. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive
(AD)
for certain Embraer S.A. Model EMB-550 and EMB-545 airplanes. This
proposed AD was prompted by reports of cracks, delamination, and
failure of the flight deck side windows during certification fatigue
tests. This proposed AD would require repetitive inspections of the
flight deck side windows for any cracking or delamination, corrective
action if necessary, and eventual replacement of the windows, as
specified in an Agencia Nacional de Avia[ccedil]ao Civil
(ANAC) AD, which will be incorporated by reference. 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
31,
2020.
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 https://www.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.
For material incorporated by reference (IBR) in this AD, contact
National Civil Aviation Agency, Aeronautical Products Certification
Branch (GGCP), Rua Laurent Martins, n[ordm] 209, Jardim Esplanada, CEP
12242-431--Sao Jose dos Campos--SP, Brazil; telephone 55
(12) 3203-6600; email pac@anac.gov.br; internet www.anac.gov.br/en/.
You may find this IBR material on the ANAC website at https://sistemas.
anac.gov.br/certificacao/DA/DAE.asp. For service information
identified in this final rule, contact Embraer S.A., Technical
Publications Section (PC 560), Rodovia Presidente Dutra, km 134,
12247-004 Distrito Eugenio de Melo-Sao Jose dos Campos-SP-Brazil;
telephone +55 12 3927-0386; email distrib@embraer.com.br; internet https:
//www.mytechcare.embraer.com. You may view this IBR 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 on the internet at https://www.regulations.gov by searching for
and locating Docket No. FAA-2020-0584.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.
gov by searching for and locating Docket No. FAA-2020-0584;
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, 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: Kathleen Arrigotti, Aerospace
Engineer, Large Aircraft Section, International Validation Branch, FAA,
2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-
3218; Kathleen.Arrigotti@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 the ADDRESSES section. Include "Docket No. FAA-2020-0584;
Product Identifier 2020-NM-069-AD" 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 NPRM based on 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 the FAA receives, without change,
to https://www.regulations.gov, including any personal information you
provide. The FAA will also post a report summarizing each substantive
verbal contact the FAA receives 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 the
person identified in the FOR FURTHER INFORMATION CONTACT section. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.
Discussion
The ANAC, which is the aviation authority for Brazil, has issued
Brazilian AD 2020-04-01R01, effective May 22, 2020 ("Brazilian AD
2020-04-01R01") (also referred to as the Mandatory Continuing
Airworthiness Information, or "the MCAI"), to correct an unsafe
condition for certain Embraer S.A. Model EMB-550 and EMB-545 airplanes.
This proposed AD was prompted by reports of cracks, delamination,
and failure of the flight deck side windows during certification
fatigue tests. The FAA is proposing this AD to address such cracks and
delamination, which could cause the flight deck side windows to fail
and lead to an in-flight depressurization event. See the MCAI for
additional background information.
Related IBR Material Under 1 CFR Part 51
Brazilian AD 2020-04-01R01 describes procedures for repetitive
detailed inspections of the flight deck side windows for any cracking
or delamination, and replacement of the windows. 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.
FAA's Determination and Requirements of This Proposed AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, the FAA
has been notified of the unsafe condition described in the MCAI
referenced above. The FAA is proposing this AD because the FAA
evaluated all the relevant information and determined the unsafe
condition described previously is likely to exist or develop in other
products of the same type design.
Proposed AD Requirements
This proposed AD would require accomplishing the actions specified
in Brazilian AD 2020-04-01R01 described previously, as incorporated by
reference, except for any differences identified as exceptions in the
regulatory text of this AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA initially worked with Airbus and EASA to develop a
process to use certain EASA ADs as the primary source of information
for compliance with requirements for corresponding FAA ADs. The FAA has
since coordinated with other manufacturers and civil aviation
authorities (CAAs) to use this process. As a result, Brazilian AD 2020-
04-01R01 will be incorporated by reference in the FAA final rule. This
proposed AD would, therefore, require compliance with Brazilian AD
2020-04-01R01 in its entirety, through that incorporation, except for
any differences identified as exceptions in the regulatory text of this
proposed AD. Service information specified in Brazilian AD 2020-04-
01R01 that is required for compliance with Brazilian AD 2020-04-01R01
will be available on the internet at https://www.regulations.gov by
searching for and locating Docket No. FAA-2020-0584 after the FAA final
rule is published.
Costs of Compliance
The FAA estimates that this proposed AD affects 49 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
|
10 work-hour x $85 per hour =
$850 |
$0
|
$850
|
$41,650
|
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
Labor cost
|
Parts cost
|
Cost per product |
9 work-hours x $85 per hour =
$765 |
$9,280 per window |
$10,045
|
According to the manufacturer, some
or all of the costs of this
proposed 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 our 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
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) 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 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 (AD):
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