Airworthiness Directives; Airbus SAS Airplanes, 42687-42689 [2021-16564]
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Federal Register / Vol. 86, No. 148 / Thursday, August 5, 2021 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0131; Project
Identifier MCAI–2020–01628–T; Amendment
39–21658; AD 2021–15–11]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus SAS Model A330–200, –300,
–800, and –900 series airplanes; and
Model A340–200, –300, –500, and –600
series airplanes. This AD was prompted
by reports that certain oxygen supply
solenoid valves are a potential source of
increased flow resistance within the
flightcrew oxygen system. This AD
requires a special detailed inspection
(flow test) of certain solenoid valves,
and replacement if necessary, as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
incorporated by reference. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective September 9,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 9, 2021.
ADDRESSES: For material incorporated
by reference (IBR) in this AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; 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–2021–
0131.
khammond on DSKJM1Z7X2PROD with RULES
SUMMARY:
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–2021–
0131; or in person at Docket Operations
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16:02 Aug 04, 2021
Jkt 253001
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
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.
FOR FURTHER INFORMATION CONTACT:
Vladimir Ulyanov, Aerospace Engineer,
Large Aircraft Section, International
Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax 206–231–3229; email
vladimir.ulyanov@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2020–0273,
dated December 9, 2020 (EASA AD
2020–0273) (also referred to as the
Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an
unsafe condition for all Airbus SAS
Model A330–201, A330–202, A330–203,
A330–223, A330–243, A330–301, A330–
302, A330–303, A330–321, A330–322,
A330–323, A330–341, A330–342, A330–
343, A330–743L, A330–841, A330–941,
A340–211, A340–212, A340–213, A340–
311, A340–312, A340–313, A340–541,
A340–542, A340–642, and A340–643
airplanes. Model A330–743L, A340–
542, and A340–643 airplanes are not
certificated by the FAA and are not
included on the U.S. type certificate
data sheet; this AD therefore does not
include those airplanes in the
applicability.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all Airbus SAS Model A330–
200, –300, –800, and –900 series
airplanes; and Model A340–200, –300,
–500, and –600 series airplanes. The
NPRM published in the Federal
Register on March 8, 2021 (86 FR
13239). The NPRM was prompted by
reports that certain oxygen supply
solenoid valves are a potential source of
increased flow resistance within the
flightcrew oxygen system. The NPRM
proposed to require a special detailed
inspection (flow test) of certain solenoid
valves, and replacement if necessary, as
specified in EASA AD 2020–0273.
The FAA is issuing this AD to address
increased flow resistance within the
flightcrew oxygen system, which could
lead to a reduced flow of oxygen supply
to the flightcrew oxygen masks, and in
combination with in-flight
depressurization, smoke in the flight
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42687
deck, or a smoke evacuation procedure,
could lead to flightcrew hypoxia and
loss of useful consciousness, resulting
in loss of control of the airplane. See the
MCAI for additional background
information.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The following presents
the comments received on the NPRM
and the FAA’s response to each
comment.
Request To Allow Additional Source of
Service Information
Delta Air Lines (DAL) asked that the
FAA add a paragraph (h)(3) to the
proposed AD which would allow
operators to use the serial numbers
identified in Safran Service Information
Letter (SIL) SIL120, dated May 20, 2019,
instead of the year of manufacture, to
determine whether a solenoid valve is
an affected part, as defined in EASA AD
2020–0273. DAL stated that the SIL
contains the serial numbers and year of
manufacture of affected solenoid valves.
The FAA agrees to clarify. EASA AD
2020–0273 does not specify how to
determine whether a solenoid valve is
an affected part. The FAA agrees that
operators can use Safran SIL120 as an
additional source of guidance for
identification of the affected parts by the
serial numbers. The FAA has added
Note 1 to paragraph (g) of this AD
stating that additional guidance for
identification of affected parts can be
found in Safran Service Information
Letter SIL120, dated May 20, 2019.
Request Not To Return Affected Valves
to Manufacturer
DAL asked that the requirement to
send any affected solenoid valves back
to Zodiac for repair, in which is
specified as ‘‘Required for Compliance’’
(RC) in the applicable service
information identified in EASA AD
2020–0273 be excluded in the proposed
AD. DAL stated that all affected parts
must pass a flow test with no defects
found prior to the next flight of the
airplane after installation on the
airplane.
The FAA agrees with the commenter
for the reasons provided. The FAA has
revised paragraph (i) of this AD to
exclude the requirement to send any
affected solenoid valve back to Zodiac
for repair.
Conclusion
The FAA reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
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Federal Register / Vol. 86, No. 148 / Thursday, August 5, 2021 / Rules and Regulations
final rule with the changes described
previously and minor editorial changes.
The FAA has determined that these
minor changes:
• Are consistent with the intent that
was proposed in the NPRM for
addressing the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
The FAA also determined that these
changes will not increase the economic
burden on any operator or increase the
scope of this final rule.
Related Service Information Under 1
CFR Part 51
EASA AD 2020–0273 describes
procedures for doing a special detailed
inspection (flow test) of certain solenoid
valves by using the flightcrew oxygen
masks and replacing any solenoid valve
that fails the flow test with a serviceable
part. 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 112 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
3 work-hours × $85 per hour = $255 ..........................................................................................
$0
$255
$28,560
The FAA estimates the following
costs to do any necessary replacement
that would be required based on the
results of any actions. The FAA has no
way of determining the number of
aircraft that might need replacement:
ESTIMATED COSTS OF ON-CONDITION ACTION
Labor cost
Parts cost
Cost per
product
1 work-hour × $85 per hour = $85 ............................................................................................................................
Up to $5,496
Up to $5,581.
khammond on DSKJM1Z7X2PROD with RULES
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
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Jkt 253001
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.
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 adding
the following new airworthiness
directive:
■
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2021–15–11 Airbus SAS: Amendment 39–
21658; Docket No. FAA–2021–0131;
Project Identifier MCAI–2020–01628–T.
(a) Effective Date
This airworthiness directive (AD) is
effective September 9, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus SAS
airplanes, certificated in any category,
identified in paragraphs (c)(1) through (8) of
this AD.
(1) Model A330–201, –202, –203, –223, and
–243 airplanes.
(2) Model A330–301, –302, –303, –321,
–322, –323, –341, –342, and –343 airplanes.
(3) Model A330–841 airplanes.
(4) Model A330–941 airplanes.
(5) Model A340–211, –212, and –213
airplanes.
(6) Model A340–311, –312, and –313
airplanes.
(7) Model A340–541 airplanes.
(8) Model A340–642 airplanes.
(d) Subject
Air Transport Association (ATA) of
America Code 35, Oxygen.
(e) Reason
This AD was prompted by reports that
certain oxygen supply solenoid valves are a
potential source of increased flow resistance
within the flightcrew oxygen system. The
FAA is issuing this AD to address increased
flow resistance within the flightcrew oxygen
system, which could lead to a reduced flow
of oxygen supply to the flightcrew oxygen
masks, and in combination with in-flight
depressurization, smoke in the flight deck, or
a smoke evacuation procedure, could lead to
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Federal Register / Vol. 86, No. 148 / Thursday, August 5, 2021 / Rules and Regulations
flightcrew hypoxia and loss of useful
consciousness, resulting in loss of control of
the airplane.
(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, European Union Aviation
Safety Agency (EASA) AD 2020–0273, dated
December 9, 2020 (EASA AD 2020–0273).
Note 1 to paragraph (g): Guidance for
identifying affected oxygen supply solenoid
valves as defined in EASA AD 2020–0273,
can be found in Safran Service Information
Letter SIL120, dated May 20, 2019.
(h) Exceptions to EASA AD 2020–0273
(1) Where EASA AD 2020–0273 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) The ‘‘Remarks’’ section of EASA AD
2020–0273 does not apply to this AD.
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(i) No Reporting or Parts Return Required
Although the service information
referenced in EASA AD 2020–0273 specifies
to submit certain information and return any
affected solenoid valve to the manufacturer
for repair, this AD does not require those
actions.
(j) 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 (k) of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the responsible
Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be 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
2020–0273 that contains RC procedures and
tests: Except as required by paragraph (j)(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
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42689
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.
DEPARTMENT OF TRANSPORTATION
(k) Related Information
Airworthiness Directives; Airbus SAS
Airplanes
For more information about this AD,
contact Vladimir Ulyanov, Aerospace
Engineer, Large Aircraft Section,
International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198;
telephone and fax 206–231–3229; email
vladimir.ulyanov@faa.gov.
(l) 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 2020–0273, dated December 9,
2020.
(ii) [Reserved]
(3) For EASA AD 2020–0273, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; 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–2021–0131.
(5) You may view this material that is
incorporated by reference at the National
Archives and Records Administration
(NARA). For information on the availability
of this material at NARA, email fedreg.legal@
nara.gov, or go to: https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on July 15, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–16564 Filed 8–4–21; 8:45 am]
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14 CFR Part 39
[Docket No. FAA–2021–0349; Project
Identifier MCAI–2021–00103–T; Amendment
39–21660; AD 2021–15–13]
RIN 2120–AA64
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus SAS Model A330–841 and –941
airplanes. This AD was prompted by
reports of missing or disbonded
pressure seals on two thrust reverser
(TR) translating cowls. This AD requires
a one-time inspection of each thrust
reverser for damage, seal bonding
rework, and replacement of translating
cowl pressure seals if necessary, as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
incorporated by reference. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective September 9,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of September 9, 2021.
ADDRESSES: For material incorporated
by reference (IBR) in this AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; 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–2021–
0349.
SUMMARY:
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–2021–
0349; 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,
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]]>Agencies
[Federal Register Volume 86, Number 148 (Thursday, August 5, 2021)]
[Rules and Regulations]
[Pages 42687-42689]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-16564]
[[Page 42687]]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0131; Project Identifier MCAI-2020-01628-T;
Amendment 39-21658; AD 2021-15-11]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Airbus SAS Model A330-200, -300, -800, and -900 series airplanes; and
Model A340-200, -300, -500, and -600 series airplanes. This AD was
prompted by reports that certain oxygen supply solenoid valves are a
potential source of increased flow resistance within the flightcrew
oxygen system. This AD requires a special detailed inspection (flow
test) of certain solenoid valves, and replacement if necessary, as
specified in a European Union Aviation Safety Agency (EASA) AD, which
is incorporated by reference. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective September 9, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September 9,
2021.
ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; 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-2021-0131.
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-2021-
0131; 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, 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.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229;
email [email protected].
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2020-0273, dated December 9, 2020
(EASA AD 2020-0273) (also referred to as the Mandatory Continuing
Airworthiness Information, or the MCAI), to correct an unsafe condition
for all Airbus SAS Model A330-201, A330-202, A330-203, A330-223, A330-
243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-
341, A330-342, A330-343, A330-743L, A330-841, A330-941, A340-211, A340-
212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-
642, and A340-643 airplanes. Model A330-743L, A340-542, and A340-643
airplanes are not certificated by the FAA and are not included on the
U.S. type certificate data sheet; this AD therefore does not include
those airplanes in the applicability.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all Airbus SAS Model
A330-200, -300, -800, and -900 series airplanes; and Model A340-200, -
300, -500, and -600 series airplanes. The NPRM published in the Federal
Register on March 8, 2021 (86 FR 13239). The NPRM was prompted by
reports that certain oxygen supply solenoid valves are a potential
source of increased flow resistance within the flightcrew oxygen
system. The NPRM proposed to require a special detailed inspection
(flow test) of certain solenoid valves, and replacement if necessary,
as specified in EASA AD 2020-0273.
The FAA is issuing this AD to address increased flow resistance
within the flightcrew oxygen system, which could lead to a reduced flow
of oxygen supply to the flightcrew oxygen masks, and in combination
with in-flight depressurization, smoke in the flight deck, or a smoke
evacuation procedure, could lead to flightcrew hypoxia and loss of
useful consciousness, resulting in loss of control of the airplane. See
the MCAI for additional background information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comments
received on the NPRM and the FAA's response to each comment.
Request To Allow Additional Source of Service Information
Delta Air Lines (DAL) asked that the FAA add a paragraph (h)(3) to
the proposed AD which would allow operators to use the serial numbers
identified in Safran Service Information Letter (SIL) SIL120, dated May
20, 2019, instead of the year of manufacture, to determine whether a
solenoid valve is an affected part, as defined in EASA AD 2020-0273.
DAL stated that the SIL contains the serial numbers and year of
manufacture of affected solenoid valves.
The FAA agrees to clarify. EASA AD 2020-0273 does not specify how
to determine whether a solenoid valve is an affected part. The FAA
agrees that operators can use Safran SIL120 as an additional source of
guidance for identification of the affected parts by the serial
numbers. The FAA has added Note 1 to paragraph (g) of this AD stating
that additional guidance for identification of affected parts can be
found in Safran Service Information Letter SIL120, dated May 20, 2019.
Request Not To Return Affected Valves to Manufacturer
DAL asked that the requirement to send any affected solenoid valves
back to Zodiac for repair, in which is specified as ``Required for
Compliance'' (RC) in the applicable service information identified in
EASA AD 2020-0273 be excluded in the proposed AD. DAL stated that all
affected parts must pass a flow test with no defects found prior to the
next flight of the airplane after installation on the airplane.
The FAA agrees with the commenter for the reasons provided. The FAA
has revised paragraph (i) of this AD to exclude the requirement to send
any affected solenoid valve back to Zodiac for repair.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this
[[Page 42688]]
final rule with the changes described previously and minor editorial
changes. The FAA has determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
The FAA also determined that these changes will not increase the
economic burden on any operator or increase the scope of this final
rule.
Related Service Information Under 1 CFR Part 51
EASA AD 2020-0273 describes procedures for doing a special detailed
inspection (flow test) of certain solenoid valves by using the
flightcrew oxygen masks and replacing any solenoid valve that fails the
flow test with a serviceable part. 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 112 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
3 work-hours x $85 per hour = $255........................... $0 $255 $28,560
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacement that would be required based on the results of any actions.
The FAA has no way of determining the number of aircraft that might
need replacement:
Estimated Costs of On-Condition Action
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
1 work-hour x $85 per hour = $85. Up to $5,496 Up to $5,581.
------------------------------------------------------------------------
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.
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:
2021-15-11 Airbus SAS: Amendment 39-21658; Docket No. FAA-2021-0131;
Project Identifier MCAI-2020-01628-T.
(a) Effective Date
This airworthiness directive (AD) is effective September 9,
2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus SAS airplanes, certificated in any
category, identified in paragraphs (c)(1) through (8) of this AD.
(1) Model A330-201, -202, -203, -223, and -243 airplanes.
(2) Model A330-301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes.
(3) Model A330-841 airplanes.
(4) Model A330-941 airplanes.
(5) Model A340-211, -212, and -213 airplanes.
(6) Model A340-311, -312, and -313 airplanes.
(7) Model A340-541 airplanes.
(8) Model A340-642 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Reason
This AD was prompted by reports that certain oxygen supply
solenoid valves are a potential source of increased flow resistance
within the flightcrew oxygen system. The FAA is issuing this AD to
address increased flow resistance within the flightcrew oxygen
system, which could lead to a reduced flow of oxygen supply to the
flightcrew oxygen masks, and in combination with in-flight
depressurization, smoke in the flight deck, or a smoke evacuation
procedure, could lead to
[[Page 42689]]
flightcrew hypoxia and loss of useful consciousness, resulting in
loss of control of the airplane.
(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, European Union Aviation Safety Agency (EASA) AD
2020-0273, dated December 9, 2020 (EASA AD 2020-0273).
Note 1 to paragraph (g): Guidance for identifying affected
oxygen supply solenoid valves as defined in EASA AD 2020-0273, can
be found in Safran Service Information Letter SIL120, dated May 20,
2019.
(h) Exceptions to EASA AD 2020-0273
(1) Where EASA AD 2020-0273 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2020-0273 does not apply
to this AD.
(i) No Reporting or Parts Return Required
Although the service information referenced in EASA AD 2020-0273
specifies to submit certain information and return any affected
solenoid valve to the manufacturer for repair, this AD does not
require those actions.
(j) 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 (k) of this AD. Information may be emailed to: [email protected]. 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 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 2020-0273 that contains RC procedures and
tests: Except as required by paragraph (j)(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.
(k) Related Information
For more information about this AD, contact Vladimir Ulyanov,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax 206-231-3229; email [email protected].
(l) 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 2020-0273,
dated December 9, 2020.
(ii) [Reserved]
(3) For EASA AD 2020-0273, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; 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-2021-0131.
(5) You may view this material that is incorporated by reference
at the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, email
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on July 15, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-16564 Filed 8-4-21; 8:45 am]
BILLING CODE 4910-13-P
