Airworthiness Directives; Airbus SAS Airplanes, 51960-51962 [2019-21238]
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Federal Register / Vol. 84, No. 190 / Tuesday, October 1, 2019 / Rules and Regulations
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(h) New Requirement of This AD:
Modification
Within 6 months after the effective date of
this AD, do the actions specified in
paragraphs (h)(1) and (2) of this AD.
(1) Install the Airbus temporary quick
change (ATQC) as specified in paragraph
(h)(1)(i) or (ii) of this AD, as applicable.
(i) For airplanes with flight warning system
(FWS) standard S4/2.0: Install ATQC
standard V4 for FWS standard S4/2.0, in
accordance with the Accomplishment
Instructions of Airbus Service Bulletin A350–
31–P028, dated September 17, 2018.
(ii) For airplanes with FWS standard S5/
2.2: Install ATQC standard V4 for FWS
standard S5/2.2, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A350–31–P029, dated
September 17, 2018. After installation of
ATQC standard V4, ATQC standard V5 for
FWS standard S5/2.2 may be installed, in
accordance with the Accomplishment
Instructions of Airbus Service Bulletin A350–
31–P032, dated February 28, 2019.
(2) Activate ECAM temporary change code
No. 27AF, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A350–31–P030, dated
September 17, 2018.
(i) Other FAA AD Provisions
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards 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 International Section, send it
to the attention of the person identified in
paragraph (j)(2) of this AD. Information may
be emailed to 9-ANM-116-AMOCREQUESTS@faa.gov.
(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
2018–22–13 are approved as AMOCs for the
corresponding provisions of this AD.
(2) Contacting the Manufacturer: As of the
effective date of this AD, for any requirement
in this AD to obtain corrective actions from
a manufacturer, the action must be
accomplished using a method approved by
the Manager, International Section, Transport
Standards Branch, FAA; or the European
Union Aviation Safety Agency (EASA); or
Airbus SAS’s EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
(3) Required for Compliance (RC): If any
service information contains procedures or
tests that are identified as RC, those
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
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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
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2018–0213R1, dated November 9, 2018, for
related information. This MCAI may be
found in the AD docket on the internet at
https://www.regulations.gov by searching for
and locating Docket No. FAA–2019–0193.
(2) For more information about this AD,
contact Kathleen Arrigotti, Aerospace
Engineer, International Section, Transport
Standards 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.
(3) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A350–31–P028,
dated September 17, 2018.
(ii) Airbus Service Bulletin A350–31–P029,
dated September 17, 2018.
(iii) Airbus Service Bulletin A350–31–
P030, dated September 17, 2018.
(iv) Airbus Service Bulletin A350–31–
P032, dated February 28, 2019.
(v) Airbus A350 Temporary Revision (TR)
113, Issue 1, dated August 17, 2018.
(4) For service information identified in
this AD, contact Airbus SAS, Airworthiness
Office—EAL, Rond-Point Emile Dewoitine
No: 2, 31700 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5 61
93 45 80; email continuedairworthiness.a350@airbus.com; internet
https://www.airbus.com.
(5) You may view this service information
at the FAA, Transport Standards Branch,
2200 South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
(6) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fedreg.legal@nara.gov, or go to https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
August 9, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–21241 Filed 9–30–19; 8:45 am]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0498; Product
Identifier 2019–NM–073–AD; Amendment
39–19742; AD 2019–19–06]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Airbus SAS Model A330–202, –243,
–243F, –302, –323, and –343 airplanes.
This AD was prompted by a report that
cracks have been found within the ring
gears of the slat geared rotary actuators
(SGRAs) due to a change in the
manufacturing process and inadequate
post-production non-destructive testing
for potential cracking. This AD requires
an inspection to determine the part
number and serial number of the
SGRAs, and replacement of each
affected SGRA with a serviceable part,
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 November 5,
2019.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of November 5, 2019.
ADDRESSES: For the material
incorporated by reference (IBR) in this
AD, contact the EASA, KonradAdenauer-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, Transport Standards Branch, 2200
South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
It is also available in the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0498.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
E:\FR\FM\01OCR1.SGM
01OCR1
51961
Federal Register / Vol. 84, No. 190 / Tuesday, October 1, 2019 / Rules and Regulations
and locating Docket No. FAA–2019–
0498; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the regulatory evaluation, 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,
International Section, Transport
Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax: 206–231–3229.
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2019–0093, dated April 26, 2019
(‘‘EASA AD 2019–0093’’) (also referred
to as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for certain Airbus SAS Model A330–
202, –243, –243F, –302, –323, and –343
airplanes.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Airbus SAS Model
A330–202, –243, –243F, –302, –323, and
–343 airplanes. The NPRM published in
the Federal Register on July 3, 2019 (84
FR 31772). The NPRM was prompted by
a report that cracks have been found
within the ring gears of the SGRAs due
to a change in the manufacturing
process and inadequate post-production
non-destructive testing for potential
cracking. The NPRM proposed to
require an inspection to determine the
part number and serial number of the
SGRAs, and replacement of each
affected SGRA with a serviceable part.
The FAA is issuing this AD to address
cracking of an SGRA, which, in
combination with an independent
failure on the second SGRA of the same
slat surface, could lead to an
uncontrolled movement of the affected
slat surface in flight, or detachment of
the slat surface, and could possibly
result in damage to the stabilizers and
reduced controllability 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 FAA received no
comments on the NPRM or on the
determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data
and determined that air safety and the
public interest require adopting this
final rule as proposed, except for 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.
Related IBR Material Under 1 CFR Part
51
EASA AD 2019–0093 describes
procedures for an inspection to
determine the part number and serial
number of the SGRAs, and replacement
of each affected part 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 2 airplanes of U.S. registry. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Up to 2 work-hours × $85 per hour = Up to $170 ....................................................
The FAA estimates the following
costs to do any necessary on-condition
action that would be required based on
$0
the results of any required actions. The
FAA has no way of determining the
Cost on U.S.
operators
Cost per product
Up to $170 ..............
Up to $340.
number of aircraft that might need this
on-condition action:
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Labor cost
Cost per
product
Parts cost
Up to 15 work-hours × $85 per hour = Up to $1,275 .....................................................................................
(*)
Up to $1,275.*
* 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 the
cost estimate.
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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.
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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.
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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.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
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Federal Register / Vol. 84, No. 190 / Tuesday, October 1, 2019 / Rules and Regulations
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to transport category
airplanes and associated appliances to
the Director of the System Oversight
Division.
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:
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2019–19–06 Airbus SAS: Amendment 39–
19742; Docket No. FAA–2019–0498;
Product Identifier 2019–NM–073–AD.
(a) Effective Date
This AD is effective November 5, 2019.
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(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus SAS Model
A330–202, –243, –243F, –302, –323, and
–343 airplanes, certificated in any category,
as identified in European Union Aviation
Safety Agency (EASA) AD 2019–0093, dated
April 26, 2019 (‘‘EASA AD 2019–0093’’).
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(e) Reason
This AD was prompted by a report that
cracks have been found within the ring gears
of the slat geared rotary actuators (SGRAs)
due to a change in the manufacturing process
and inadequate post-production nondestructive testing for potential cracking. The
FAA is issuing this AD to address cracking
of an SGRA, which, in combination with an
independent failure on the second SGRA of
the same slat surface, could lead to an
uncontrolled movement of the affected slat
surface in flight, or detachment of the slat
surface, and could possibly result in damage
to the stabilizers and reduced controllability
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, EASA AD 2019–0093. All
provisions specified in EASA AD 2019–0093
apply in this AD.
(h) Exceptions to EASA AD 2019–0093
(1) For purposes of determining
compliance with the requirements of this AD:
Where EASA AD 2019–0093 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) The ‘‘Remarks’’ section of EASA AD
2019–0093 does not apply to this AD.
(i) No Reporting Requirement
Although EASA AD 2019–0093 specifies to
submit certain information to the
manufacturer, this AD does not include that
requirement.
PART 39—AIRWORTHINESS
DIRECTIVES
§ 39.13
(d) Subject
Air Transport Association (ATA) of
America Code 27, Flight control.
(j) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards 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 International Section, send it
to the attention of the person identified in
paragraph (k) of this AD. Information may be
emailed to: 9-ANM-116-AMOC-REQUESTS@
faa.gov. 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.
(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, International Section,
Transport Standards Branch, FAA; or EASA;
or Airbus SAS’s EASA Design Organization
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Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
(3) Required for Compliance (RC): For any
service information referenced in EASA AD
2019–0093 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, International Section, Transport
Standards Branch, FAA, 2200 South 216th
St., Des Moines, WA 98198; telephone and
fax: 206–231–3229.
(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 2019–0093, dated April 26, 2019.
(ii) [Reserved]
(3) For information about EASA AD 2019–
0093, 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,
Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information
on the availability of this material at the
FAA, call 206–231–3195. 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–2019–0498.
(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 in Des Moines, Washington, on
September 19, 2019.
Suzanne Masterson,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–21238 Filed 9–30–19; 8:45 am]
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]]>Agencies
[Federal Register Volume 84, Number 190 (Tuesday, October 1, 2019)]
[Rules and Regulations]
[Pages 51960-51962]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-21238]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0498; Product Identifier 2019-NM-073-AD; Amendment
39-19742; AD 2019-19-06]
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
certain Airbus SAS Model A330-202, -243, -243F, -302, -323, and -343
airplanes. This AD was prompted by a report that cracks have been found
within the ring gears of the slat geared rotary actuators (SGRAs) due
to a change in the manufacturing process and inadequate post-production
non-destructive testing for potential cracking. This AD requires an
inspection to determine the part number and serial number of the SGRAs,
and replacement of each affected SGRA with a serviceable part, 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 November 5, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 5,
2019.
ADDRESSES: For the 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, Transport Standards Branch, 2200 South 216th St., Des Moines, WA.
For information on the availability of this material at the FAA, call
206-231-3195. It is also available in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2019-0498.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for
[[Page 51961]]
and locating Docket No. FAA-2019-0498; or in person at Docket
Operations between 9 a.m. and 5 p.m., Monday through Friday, except
Federal holidays. The AD docket contains this final rule, the
regulatory evaluation, 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,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax: 206-231-3229.
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2019-0093, dated April 26, 2019
(``EASA AD 2019-0093'') (also referred to as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Airbus SAS Model A330-202, -243, -243F, -302, -
323, and -343 airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Airbus SAS
Model A330-202, -243, -243F, -302, -323, and -343 airplanes. The NPRM
published in the Federal Register on July 3, 2019 (84 FR 31772). The
NPRM was prompted by a report that cracks have been found within the
ring gears of the SGRAs due to a change in the manufacturing process
and inadequate post-production non-destructive testing for potential
cracking. The NPRM proposed to require an inspection to determine the
part number and serial number of the SGRAs, and replacement of each
affected SGRA with a serviceable part.
The FAA is issuing this AD to address cracking of an SGRA, which,
in combination with an independent failure on the second SGRA of the
same slat surface, could lead to an uncontrolled movement of the
affected slat surface in flight, or detachment of the slat surface, and
could possibly result in damage to the stabilizers and reduced
controllability 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 FAA received no comments on the NPRM or
on the determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed,
except for 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.
Related IBR Material Under 1 CFR Part 51
EASA AD 2019-0093 describes procedures for an inspection to
determine the part number and serial number of the SGRAs, and
replacement of each affected part 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 2 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Labor cost Parts cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 2 work-hours x $85 per hour = Up $0 Up to $170................ Up to $340.
to $170.
----------------------------------------------------------------------------------------------------------------
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
------------------------------------------------------------------------
Up to 15 work-hours x $85 per (*) Up to $1,275.*
hour = Up to $1,275.
------------------------------------------------------------------------
* 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 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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the
[[Page 51962]]
Compliance and Airworthiness Division, but during this transition
period, the Executive Director has delegated the authority to issue ADs
applicable to transport category airplanes and associated appliances to
the Director of the System Oversight Division.
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 (AD):
2019-19-06 Airbus SAS: Amendment 39-19742; Docket No. FAA-2019-0498;
Product Identifier 2019-NM-073-AD.
(a) Effective Date
This AD is effective November 5, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus SAS Model A330-202, -243, -243F, -302,
-323, and -343 airplanes, certificated in any category, as
identified in European Union Aviation Safety Agency (EASA) AD 2019-
0093, dated April 26, 2019 (``EASA AD 2019-0093'').
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
control.
(e) Reason
This AD was prompted by a report that cracks have been found
within the ring gears of the slat geared rotary actuators (SGRAs)
due to a change in the manufacturing process and inadequate post-
production non-destructive testing for potential cracking. The FAA
is issuing this AD to address cracking of an SGRA, which, in
combination with an independent failure on the second SGRA of the
same slat surface, could lead to an uncontrolled movement of the
affected slat surface in flight, or detachment of the slat surface,
and could possibly result in damage to the stabilizers and reduced
controllability 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, EASA AD 2019-0093. All provisions specified in EASA
AD 2019-0093 apply in this AD.
(h) Exceptions to EASA AD 2019-0093
(1) For purposes of determining compliance with the requirements
of this AD: Where EASA AD 2019-0093 refers to its effective date,
this AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2019-0093 does not apply
to this AD.
(i) No Reporting Requirement
Although EASA AD 2019-0093 specifies to submit certain
information to the manufacturer, this AD does not include that
requirement.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards 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 International Section, 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 local flight
standards district office/certificate holding district 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, International
Section, Transport Standards 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 2019-0093 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, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax: 206-231-3229.
(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 2019-0093,
dated April 26, 2019.
(ii) [Reserved]
(3) For information about EASA AD 2019-0093, 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, Transport Standards
Branch, 2200 South 216th St., Des Moines, WA. For information on the
availability of this material at the FAA, call 206-231-3195. 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-
2019-0498.
(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 in Des Moines, Washington, on September 19, 2019.
Suzanne Masterson,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-21238 Filed 9-30-19; 8:45 am]
BILLING CODE 4910-13-P
