Airworthiness Directives; Airbus SAS Airplanes, 30601-30604 [2020-10629]
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Federal Register / Vol. 85, No. 98 / Wednesday, May 20, 2020 / Rules and Regulations
Issued on May 14, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–10744 Filed 5–19–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0452; Product
Identifier 2020–NM–062–AD; Amendment
39–19910; AD 2020–09–14]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2020–03–
12, which applied to all Airbus SAS
Model A350–941 and –1041 airplanes.
AD 2020–03–12 required revising the
existing airplane flight manual (AFM) to
define a liquid-prohibited zone in the
flight deck and provide procedures
following liquid spillage on the center
pedestal. This AD continues to require
revising the existing AFM, and also
requires installing a removable
integrated control panel (ICP) cover in
the flight deck and further revising the
AFM to include instructions for ICP
cover use, as specified in a European
Union Aviation Safety Agency (EASA)
AD, which is incorporated by reference.
This AD was prompted by the FAA’s
determination that a removable
integrated control panel (ICP) cover
must be installed to prevent damage
from spillage and that the existing AFM
must be revised. The FAA is issuing this
AD to address the unsafe condition on
these products.
DATES: This AD becomes effective June
4, 2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of June 4, 2020.
The FAA must receive comments on
this AD by July 6, 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.
SUMMARY:
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• 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: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For material incorporated by reference
(IBR) in this AD, contact the EASA,
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
89990 1000; email ADs@easa.europa.eu;
internet www.easa.europa.eu. You may
find this IBR material on the EASA
website at https://ad.easa.europa.eu.
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–
0452.
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–
0452; 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 AD, 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.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued AD 2020–03–12,
Amendment 39–19837 (85 FR 7863,
February 12, 2020) (‘‘AD 2020–03–12’’),
which applied to all Airbus SAS Model
A350–941 and –1041 airplanes. AD
2020–03–12 required revising the
existing AFM to define a liquidprohibited zone in the flight deck and
provide procedures following liquid
spillage on the center pedestal. The
FAA issued AD 2020–03–12 to address
the potential for dual-engine
uncommanded engine inflight
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30601
shutdown (IFSD), possibly resulting in a
forced landing with consequent damage
to the airplane and injury to occupants.
Actions Since AD 2020–03–12 Was
Issued
Since the FAA issued AD 2020–03–
12, Airbus developed mod 116010,
introducing a removable cover for the
ICP, which protects the ICP completely,
including engine master levers,
thumbwheels, and rotary knob, and
provided modification instructions.
Airbus also published a new AFM
temporary revision (TR) defining a
liquid-prohibited zone in the cockpit,
procedures for ICP removable cover use,
and the procedures to be followed in the
case of inadvertent liquid spillage on
the center pedestal. The FAA has
determined that the removable ICP
cover must be installed and the existing
AFM must be revised to include these
new procedures.
The EASA, which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2020–0090, dated April 20, 2020
(‘‘EASA AD 2020–0090’’) (also referred
to as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for certain Airbus SAS Model A350–941
and –1041 airplanes. EASA AD 2020–
0090 supersedes EASA Emergency AD
2020–0020–E, dated February 5, 2020,
corrected February 6, 2020 (which
corresponds to FAA AD 2020–03–12).
This AD was prompted by two reports
of abnormal operation of the
components of the ENG START panel or
Electronic Centralized Aircraft
Monitoring (ECAM) Control Panel (ECP)
due to liquid spillage in the system, and
the subsequent uncommanded engine
IFSD of one engine in each case. This
AD was also prompted by the FAA’s
determination that a removable
integrated control panel (ICP) cover
must be installed to prevent damage
from spillage and that the existing AFM
must be revised. The FAA is issuing this
AD to address the potential for dualengine IFSD, possibly resulting in a
forced landing with consequent damage
to the airplane and injury to occupants.
See the MCAI for additional background
information.
Explanation of Retained Requirements
Although this AD does not explicitly
restate the requirements of AD 2020–
03–12, this AD retains all of the
requirements of AD 2020–03–12. Those
requirements are referenced in EASA
AD 2020–0090, which, in turn, is
referenced in paragraph (g) of this AD.
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Federal Register / Vol. 85, No. 98 / Wednesday, May 20, 2020 / Rules and Regulations
Related IBR Material Under 1 CFR Part
51
EASA AD 2020–0090 describes
procedures for installation of the ICP
removable cover in the cockpit and
amendment of the AFM to define a
liquid-prohibited zone in the cockpit,
provide procedures for ICP removable
cover use, and provide procedures
following liquid spillage on the center
pedestal. 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
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 the State
of Design Authority, the FAA has been
notified of the unsafe condition
described in the MCAI referenced
above. The FAA is issuing this AD
because the FAA has evaluated all
pertinent information and determined
the unsafe condition exists and is likely
to exist or develop on other products of
the same type design.
Requirements of This AD
This AD requires accomplishing the
actions specified in EASA AD 2020–
0090 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, in EASA
AD 2020–0090 is incorporated by
reference in this AD. This AD, therefore,
requires compliance with EASA AD
2020–0090 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 the
EASA AD does not mean that operators
need comply only with that section. For
example, where the AD requirement
refers to ‘‘all required actions and
compliance times,’’ compliance with
this AD requirement is not limited to
the section titled ‘‘Required Action(s)
and Compliance Time(s)’’ in the EASA
AD. Service information specified in
EASA AD 2020–0090 that is required for
compliance with EASA AD 2020–0090
is available on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0452.
Interim Action
The FAA considers this AD interim
action. If final action is later identified,
the FAA might consider further
rulemaking then.
FAA’s Justification and Determination
of the Effective Date
An unsafe condition exists that
requires the immediate adoption of this
AD without providing an opportunity
for public comments prior to adoption.
The FAA has found that the risk to the
flying public justifies waiving notice
and comment prior to adoption of this
rule because abnormal operation of the
components of the ENG START panel or
ECP due to liquid spillage in the system
could result in dual-engine IFSD,
possibly resulting in a forced landing
with consequent damage to the airplane
and injury to occupants. Therefore, the
FAA finds good cause that notice and
opportunity for prior public comment
are impracticable. In addition, for the
reasons stated above, the FAA finds that
good cause exists for making this
amendment effective in less than 30
days.
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.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
the FAA did not precede it by notice
and opportunity for public comment.
The FAA invites you to send any
written relevant data, views, or
arguments about this AD. Send your
comments to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2020–0452; Product Identifier
2020–NM–062–AD’’ at the beginning of
your comments. The FAA specifically
invites comments on the overall
regulatory, economic, environmental,
and energy aspects of this AD. The FAA
will consider all comments received by
the closing date and may amend this AD
based on those comments.
The FAA will post all comments
received, 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 received about this AD.
Costs of Compliance
The FAA estimates that this AD
affects 13 airplanes of U.S. registry. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Actions
Labor cost
Retained actions from AD 2020–03–12 .........
New actions ....................................................
1 work-hour × $85 per hour = $85 .................
2 work-hours × $85 per hour = $170 .............
Cost per
product
Parts cost
$0
*0
$85
170
Cost on U.S.
operators
$1,105
2,210
* The FAA has received no definitive data regarding cost estimates for these parts.
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
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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
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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
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Federal Register / Vol. 85, No. 98 / Wednesday, May 20, 2020 / Rules and Regulations
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 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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing airworthiness directive (AD)
2020–03–12, Amendment 39–19837 (85
FR 7863, February 12, 2020), and adding
the following new AD:
■
2020–09–14 Airbus SAS: Amendment 39–
19910; Docket No. FAA–2020–0452;
Product Identifier 2020–NM–062–AD.
(a) Effective Date
This AD becomes effective June 4, 2020.
(b) Affected ADs
This AD replaces AD 2020–03–12,
Amendment 39–19837 (85 FR 7863, February
12, 2020) (‘‘AD 2020–03–12’’).
(c) Applicability
This AD applies to Airbus SAS Model
A350–941 and –1041 airplanes, certificated
in any category, as identified in European
Union Aviation Safety Agency (EASA) AD
VerDate Sep<11>2014
16:29 May 19, 2020
Jkt 250001
2020–0090, dated April 20, 2020 (‘‘EASA AD
2020–0090’’).
(d) Subject
Air Transport Association (ATA) of
America Code 31, Instruments.
(e) Reason
This AD was prompted by two reports of
abnormal operation of the components of the
ENG START panel or Electronic Centralized
Aircraft Monitoring (ECAM) Control Panel
(ECP) due to liquid spillage in the system,
and the subsequent uncommanded engine
inflight shutdown (IFSD) of one engine in
each case. This AD was also prompted by the
FAA’s determination that a removable
integrated control panel (ICP) cover must be
installed to prevent damage from spillage and
the existing AFM must be revised. The FAA
is issuing this AD to address the potential for
dual-engine IFSD, possibly resulting in a
forced landing with consequent damage to
the airplane and injury to occupants.
(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, EASA AD 2020–0090.
(h) Exceptions to EASA AD 2020–0090
(1) Where EASA AD 2020–0090 refers to
‘‘the effective date of EASA AD 2020–0020–
E,’’ this AD requires using February 14, 2020
(the effective date of AD 2020–03–12).
(2) Where EASA AD 2020–0090 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) ‘‘Note 1’’ of EASA AD 2020–0090 does
not apply to this AD. However, after the
actions required by paragraph (g) of this AD
have been accomplished on an airplane, that
airplane may be operated with a damaged or
missing ICP removable cover, provided
provisions that address the ICP removable
cover are included in the operator’s approved
minimum equipment list (MEL).
(4) The ‘‘Remarks’’ section of EASA AD
2020–0090 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 local Flight Standards
District 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: 9-ANM-116AMOC-REQUESTS@faa.gov.
(i) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
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30603
of the local flight standards district office/
certificate holding district office.
(ii) AMOCs approved previously for AD
2020–03–12 are approved as AMOCs for the
corresponding provisions of EASA AD 2020–
0090 that are required by 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
EASA; or Airbus SAS’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(3) Required for Compliance (RC): For any
service information referenced in EASA AD
2020–0090 that contains RC procedures and
tests: Except as required by paragraph (i)(2)
of this AD, RC procedures and tests must be
done to comply with this AD; any procedures
or tests that are not identified as RC are
recommended. Those procedures and tests
that are 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
procedures and tests identified as RC can be
done and the airplane can be put back in an
airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(j) Related Information
For more information about this AD,
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.
(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) European Union Aviation Safety Agency
(EASA) AD 2020–0090, dated April 20, 2020.
(ii) [Reserved]
(3) For information about EASA AD 2020–
0090, contact the EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; telephone
+49 221 89990 6017; email ADs@
easa.europa.eu; Internet
www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://
ad.easa.europa.eu.
(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. This material may be found
in the AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2020–0452.
(5) You may view this material that is
incorporated by reference at the National
Archives and Records Administration
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Federal Register / Vol. 85, No. 98 / Wednesday, May 20, 2020 / Rules and Regulations
(NARA). For information on the availability
of this material at NARA, email fedreg.legal@
nara.gov, or go to: https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on May 6, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2020–10629 Filed 5–19–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
14 CFR Part 71
[Docket No. FAA–2019–0972; Airspace
Docket No. 19–ANM–30]
RIN 2120–AA66
Correction of Class E Airspace;
Mountain Home, ID
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule, correction.
AGENCY:
This action removes
exclusionary language from the Final
Rule published in the Federal Register
on March 31, 2020 for Mountain Home
Municipal Airport’s Class E airspace
extending upward from 700 feet above
the surface. If the exclusionary language
remains in the Final Rule, the FAA’s
Aeronautical Information Service will
be required to recalculate the airport’s
airspace boundaries whenever
Mountain Home Air Force Base’s Class
D and E Surface areas are modified.
However, the removal of the language
does not affect the charted boundaries
or operating requirements of the
airspace.
SUMMARY:
Effective 0901 UTC, July 16,
2020. The Director of the Federal
Register approves this incorporation by
reference action under Title 1 Code of
Federal Regulations part 51, subject to
the annual revision of FAA Order
7400.11 and publication of conforming
amendments.
ADDRESSES: FAA Order 7400.11D,
Airspace Designations and Reporting
Points, and subsequent amendments can
be viewed online at https://
www.faa.gov//air_traffic/publications/.
For further information, you can contact
the Airspace Policy Group, Federal
Aviation Administration, 800
Independence Avenue SW, Washington,
DC 20591; telephone: (202) 267–8783.
The Order is also available for
inspection at the National Archives and
Records Administration (NARA). For
information on the availability of FAA
Order 7400.11D at NARA, email
fedreg.legal@nara.gov or go to https://
DATES:
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www.archives.gov/federal-register/cfr/
ibr-locations.html.
FOR FURTHER INFORMATION CONTACT:
Matthew Van Der Wal, Federal Aviation
Administration, Western Service Center,
Operations Support Group, 2200 S
216th Street, Des Moines, WA 98198;
telephone (206) 231–3695.
SUPPLEMENTARY INFORMATION:
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it would
amend Class E airspace at Mountain
Home Municipal Airport, Mountain
Home, ID, to ensure the safety and
management of Instrument Flight Rules
(IFR) operations at the airport.
History
The FAA included exclusionary
language in the Final Rule that becomes
effective on July 16, 2020 (85 FR 17744,
March 31, 2020). This action will
update the language in the final rule,
but will not affect the airspace’s charted
boundaries.
Class E5 airspace designations are
published in paragraph 6005 of FAA
Order 7400.11D, dated August 8, 2019,
and effective September 15, 2019, which
is incorporated by reference in 14 CFR
71.1. The Class E airspace designation
listed in this document will be
published subsequently in the Order.
Availability and Summary of
Documents for Incorporation by
Reference
This document amends FAA Order
7400.11D dated August 8, 2019, and
effective September 15, 2019. FAA
Order 7400.11D is publicly available as
listed in the ADDRESSES section of this
document. FAA Order 7400.11D lists
Class A, B, C, D, and E airspace areas,
air traffic service routes, and reporting
points.
The Rule
The FAA is amending Title 14, Code
of Federal Regulations (14 CFR) part 71
by removing the exclusionary language
from Mountain Home Municipal
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Airport’s Class E airspace extending
upward from 700 feet above the surface.
If the exclusionary language is not
removed, it will require the FAA’s
Aeronautical Information Service to
recalculate the Municipal Airport’s
airspace boundaries whenever changes
occur to Mountain Home Air Force
Base’s surface areas but will not affect
the airspace’s charted boundaries.
Regulatory Notices and Analyses
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
current, is non-controversial, and
unlikely to result in adverse or negative
comments. It, therefore: (1) Is not a
‘‘significant regulatory action’’ under
Executive Order 12866; (2) is not a
‘‘significant rule’’ under DOT
Regulatory Policies and Procedures (44
FR 11034; February 26, 1979); and (3)
does not warrant preparation of a
regulatory evaluation as the anticipated
impact is so minimal. Since this is a
routine matter that only affects air traffic
procedures and air navigation, it is
certified that this rule, when
promulgated, does not have a significant
economic impact on a substantial
number of small entities under the
criteria of the Regulatory Flexibility Act.
Environmental Review
The FAA has determined that this
action qualifies for categorical exclusion
under the National Environmental
Policy Act in accordance with FAA
Order 1050.1F, ‘‘Environmental
Impacts: Policies and Procedures,’’
paragraph 5–6.5a. This airspace action
is not expected to cause any potentially
significant environmental impacts, and
no extraordinary circumstances exist
that warrant preparation of an
environmental assessment.
Lists of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference,
Navigation (Air).
Adoption of the Amendment
In consideration of the foregoing, the
Federal Aviation Administration
amends 14 CFR part 71 as follows:
PART 71—DESIGNATION OF CLASS A,
B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND
REPORTING POINTS
1. The authority citation for Part 71
continues to read as follows:
■
Authority: 49 U.S.C. 106(f), 106(g); 40103,
40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR,
1959–1963 Comp., p. 389.
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]]>Agencies
[Federal Register Volume 85, Number 98 (Wednesday, May 20, 2020)]
[Rules and Regulations]
[Pages 30601-30604]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-10629]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0452; Product Identifier 2020-NM-062-AD; Amendment
39-19910; AD 2020-09-14]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-03-
12, which applied to all Airbus SAS Model A350-941 and -1041 airplanes.
AD 2020-03-12 required revising the existing airplane flight manual
(AFM) to define a liquid-prohibited zone in the flight deck and provide
procedures following liquid spillage on the center pedestal. This AD
continues to require revising the existing AFM, and also requires
installing a removable integrated control panel (ICP) cover in the
flight deck and further revising the AFM to include instructions for
ICP cover use, as specified in a European Union Aviation Safety Agency
(EASA) AD, which is incorporated by reference. This AD was prompted by
the FAA's determination that a removable integrated control panel (ICP)
cover must be installed to prevent damage from spillage and that the
existing AFM must be revised. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD becomes effective June 4, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 4,
2020.
The FAA must receive comments on this AD by July 6, 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: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For material incorporated by reference (IBR) in this AD, contact
the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49
221 89990 1000; email [email protected]; internet www.easa.europa.eu.
You may find this IBR material on the EASA website at https://ad.easa.europa.eu. 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-2020-0452.
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-
0452; 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 AD, 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.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued AD 2020-03-12, Amendment 39-19837 (85 FR 7863,
February 12, 2020) (``AD 2020-03-12''), which applied to all Airbus SAS
Model A350-941 and -1041 airplanes. AD 2020-03-12 required revising the
existing AFM to define a liquid-prohibited zone in the flight deck and
provide procedures following liquid spillage on the center pedestal.
The FAA issued AD 2020-03-12 to address the potential for dual-engine
uncommanded engine inflight shutdown (IFSD), possibly resulting in a
forced landing with consequent damage to the airplane and injury to
occupants.
Actions Since AD 2020-03-12 Was Issued
Since the FAA issued AD 2020-03-12, Airbus developed mod 116010,
introducing a removable cover for the ICP, which protects the ICP
completely, including engine master levers, thumbwheels, and rotary
knob, and provided modification instructions. Airbus also published a
new AFM temporary revision (TR) defining a liquid-prohibited zone in
the cockpit, procedures for ICP removable cover use, and the procedures
to be followed in the case of inadvertent liquid spillage on the center
pedestal. The FAA has determined that the removable ICP cover must be
installed and the existing AFM must be revised to include these new
procedures.
The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0090, dated April 20, 2020
(``EASA AD 2020-0090'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Airbus SAS Model A350-941 and -1041 airplanes.
EASA AD 2020-0090 supersedes EASA Emergency AD 2020-0020-E, dated
February 5, 2020, corrected February 6, 2020 (which corresponds to FAA
AD 2020-03-12).
This AD was prompted by two reports of abnormal operation of the
components of the ENG START panel or Electronic Centralized Aircraft
Monitoring (ECAM) Control Panel (ECP) due to liquid spillage in the
system, and the subsequent uncommanded engine IFSD of one engine in
each case. This AD was also prompted by the FAA's determination that a
removable integrated control panel (ICP) cover must be installed to
prevent damage from spillage and that the existing AFM must be revised.
The FAA is issuing this AD to address the potential for dual-engine
IFSD, possibly resulting in a forced landing with consequent damage to
the airplane and injury to occupants. See the MCAI for additional
background information.
Explanation of Retained Requirements
Although this AD does not explicitly restate the requirements of AD
2020-03-12, this AD retains all of the requirements of AD 2020-03-12.
Those requirements are referenced in EASA AD 2020-0090, which, in turn,
is referenced in paragraph (g) of this AD.
[[Page 30602]]
Related IBR Material Under 1 CFR Part 51
EASA AD 2020-0090 describes procedures for installation of the ICP
removable cover in the cockpit and amendment of the AFM to define a
liquid-prohibited zone in the cockpit, provide procedures for ICP
removable cover use, and provide procedures following liquid spillage
on the center pedestal. 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
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 the State of Design Authority,
the FAA has been notified of the unsafe condition described in the MCAI
referenced above. The FAA is issuing this AD because the FAA has
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
Requirements of This AD
This AD requires accomplishing the actions specified in EASA AD
2020-0090 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, in EASA AD 2020-
0090 is incorporated by reference in this AD. This AD, therefore,
requires compliance with EASA AD 2020-0090 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 the EASA AD does not mean
that operators need comply only with that section. For example, where
the AD requirement refers to ``all required actions and compliance
times,'' compliance with this AD requirement is not limited to the
section titled ``Required Action(s) and Compliance Time(s)'' in the
EASA AD. Service information specified in EASA AD 2020-0090 that is
required for compliance with EASA AD 2020-0090 is available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2020-0452.
Interim Action
The FAA considers this AD interim action. If final action is later
identified, the FAA might consider further rulemaking then.
FAA's Justification and Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies waiving notice and comment prior to adoption of this rule
because abnormal operation of the components of the ENG START panel or
ECP due to liquid spillage in the system could result in dual-engine
IFSD, possibly resulting in a forced landing with consequent damage to
the airplane and injury to occupants. Therefore, the FAA finds good
cause that notice and opportunity for prior public comment are
impracticable. In addition, for the reasons stated above, the FAA finds
that good cause exists for making this amendment effective in less than
30 days.
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.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and the FAA did not precede it by notice and opportunity for
public comment. The FAA invites you to send any written relevant data,
views, or arguments about this AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2020-0452;
Product Identifier 2020-NM-062-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this AD. The FAA will
consider all comments received by the closing date and may amend this
AD based on those comments.
The FAA will post all comments received, 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 received about this AD.
Costs of Compliance
The FAA estimates that this AD affects 13 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Actions Labor cost Parts cost product operators
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Retained actions from AD 2020-03-12... 1 work-hour x $85 per $0 $85 $1,105
hour = $85.
New actions........................... 2 work-hours x $85 per * 0 170 2,210
hour = $170.
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* The FAA has received no definitive data regarding cost estimates for these parts.
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 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
[[Page 30603]]
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 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 removing airworthiness directive (AD)
2020-03-12, Amendment 39-19837 (85 FR 7863, February 12, 2020), and
adding the following new AD:
2020-09-14 Airbus SAS: Amendment 39-19910; Docket No. FAA-2020-0452;
Product Identifier 2020-NM-062-AD.
(a) Effective Date
This AD becomes effective June 4, 2020.
(b) Affected ADs
This AD replaces AD 2020-03-12, Amendment 39-19837 (85 FR 7863,
February 12, 2020) (``AD 2020-03-12'').
(c) Applicability
This AD applies to Airbus SAS Model A350-941 and -1041
airplanes, certificated in any category, as identified in European
Union Aviation Safety Agency (EASA) AD 2020-0090, dated April 20,
2020 (``EASA AD 2020-0090'').
(d) Subject
Air Transport Association (ATA) of America Code 31, Instruments.
(e) Reason
This AD was prompted by two reports of abnormal operation of the
components of the ENG START panel or Electronic Centralized Aircraft
Monitoring (ECAM) Control Panel (ECP) due to liquid spillage in the
system, and the subsequent uncommanded engine inflight shutdown
(IFSD) of one engine in each case. This AD was also prompted by the
FAA's determination that a removable integrated control panel (ICP)
cover must be installed to prevent damage from spillage and the
existing AFM must be revised. The FAA is issuing this AD to address
the potential for dual-engine IFSD, possibly resulting in a forced
landing with consequent damage to the airplane and injury to
occupants.
(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, EASA AD 2020-0090.
(h) Exceptions to EASA AD 2020-0090
(1) Where EASA AD 2020-0090 refers to ``the effective date of
EASA AD 2020-0020-E,'' this AD requires using February 14, 2020 (the
effective date of AD 2020-03-12).
(2) Where EASA AD 2020-0090 refers to its effective date, this
AD requires using the effective date of this AD.
(3) ``Note 1'' of EASA AD 2020-0090 does not apply to this AD.
However, after the actions required by paragraph (g) of this AD have
been accomplished on an airplane, that airplane may be operated with
a damaged or missing ICP removable cover, provided provisions that
address the ICP removable cover are included in the operator's
approved minimum equipment list (MEL).
(4) The ``Remarks'' section of EASA AD 2020-0090 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 local Flight
Standards District 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: [email protected].
(i) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(ii) AMOCs approved previously for AD 2020-03-12 are approved as
AMOCs for the corresponding provisions of EASA AD 2020-0090 that are
required by 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 EASA; or Airbus
SAS's EASA Design Organization Approval (DOA). If approved by the
DOA, the approval must include the DOA-authorized signature.
(3) Required for Compliance (RC): For any service information
referenced in EASA AD 2020-0090 that contains RC procedures and
tests: Except as required by paragraph (i)(2) of this AD, RC
procedures and tests must be done to comply with this AD; any
procedures or tests that are not identified as RC are recommended.
Those procedures and tests that are 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 procedures and tests identified as
RC can be done and the airplane can be put back in an airworthy
condition. Any substitutions or changes to procedures or tests
identified as RC require approval of an AMOC.
(j) Related Information
For more information about this AD, 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.
(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) European Union Aviation Safety Agency (EASA) AD 2020-0090,
dated April 20, 2020.
(ii) [Reserved]
(3) For information about EASA AD 2020-0090, contact the EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
89990 6017; email [email protected]; Internet www.easa.europa.eu.
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
(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. This material may be found in the AD
docket on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2020-0452.
(5) You may view this material that is incorporated by reference
at the National Archives and Records Administration
[[Page 30604]]
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on May 6, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-10629 Filed 5-19-20; 8:45 am]
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