Airworthiness Directives; Airbus SAS Airplanes, 54480-54482 [2019-22153]
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54480
Federal Register / Vol. 84, No. 197 / Thursday, October 10, 2019 / Rules and Regulations
8. Equipment—General—Powerplant
Instruments (Compliance with § 23.1305
requirements):
a. In place of compliance with
§ 23.1305, the applicant will comply
with the following:
(1) The following are required
powerplant instruments:
(a) A fuel quantity indicator for each
fuel tank, installed in accordance with
§ 23.1337(b).
(b) An oil pressure indicator.
(c) An oil temperature indicator.
(d) A tachometer indicating propeller
speed.
(e) A coolant temperature indicator.
(f) An indicating means for the fuel
strainer or filter required by § 23.997 to
indicate the occurrence of
contamination of the strainer or filter
before it reaches the capacity
established in accordance with
§ 23.997(d).
1. No indicator is required if the
engine can operate normally for a
specified period with the fuel strainer
exposed to the maximum fuel
contamination as specified in MIL–
5007D and provisions for replacing the
fuel filter at this specified period (or a
shorter period) are included in the
maintenance schedule for the engine
installation.
(g) Power setting, in percentage.
(h) Fuel temperature.
(i) Fuel flow (engine fuel
consumption).
9. Operating Limitations and
Information—Powerplant limitations—
Fuel grade or designation (Compliance
with § 23.1521(d) requirements):
Instead of compliance with
§ 23.1521(d), the applicant must comply
with the following:
The minimum fuel designation (for
diesel engines) must be established so it
is not less than that required for the
operation of the engines within the
limitations in paragraphs (b) and (c) of
§ 23.1521.
10. Markings and Placards—
Miscellaneous markings and placards—
Fuel, oil, and coolant filler openings
(Compliance with § 23.1557(c)(1)
requirements):
Instead of compliance with
§ 23.1557(c)(1), the applicant must
comply with the following:
a. Fuel filler openings must be marked
at or near the filler cover with—
(1) For diesel engine-powered
airplanes—
(a) The words ‘‘Jet Fuel’’; and
(b) The permissible fuel designations,
or references to the Airplane Flight
Manual (AFM) for permissible fuel
designations.
(c) A warning placard or note that
states the following or similar:
VerDate Sep<11>2014
16:03 Oct 09, 2019
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‘‘Warning—this airplane equipped
with an aircraft diesel engine, service
with approved fuels only.’’
The colors of this warning placard
should be black and white.
11. Powerplant—Fuel system—Fuelfreezing:
If the fuel in the tanks cannot be
shown to flow suitably under all
possible temperature conditions, then
fuel temperature limitations are
required. These will be considered as
part of the essential operating
parameters for the aircraft and must be
limitations.
a. The takeoff temperature limitation
must be determined by testing or
analysis to define the minimum coldsoaked temperature of the fuel that the
airplane can operate on.
b. The minimum operating
temperature limitation must be
determined by testing to define the
minimum operating temperature
acceptable after takeoff (with minimum
takeoff temperature established in (a) of
this paragraph).
12. Powerplant Installation—
Vibration levels:
a. Vibration levels throughout the
engine operating range must be
evaluated and:
(1) Vibration levels imposed on the
airframe must be less than or equivalent
to those of the gasoline engine; or
(2) Any vibration level that is higher
than that imposed on the airframe by
the replaced gasoline engine must be
considered in the modification and the
effects on the technical areas covered by
the following paragraphs must be
investigated: 14 CFR part 23, §§ 23.251;
23.613; 23.627; 23.629 (or CAR 3.159, as
applicable to various models); 23.572;
23.573; 23.574 and 23.901.
b. Vibration levels imposed on the
airframe can be mitigated to an
acceptable level by use of isolators,
dampers clutches, and similar
provisions, so unacceptable vibration
levels are not imposed on the previously
certificated structure.
13. Powerplant Installation—One
cylinder inoperative:
It must be shown by test or analysis,
or by a combination of methods, that the
airframe can withstand the shaking or
vibratory forces imposed by the engine
if a cylinder becomes inoperative. Diesel
engines of conventional design typically
have extremely high levels of vibration
when a cylinder becomes inoperative.
Data must be provided to the airframe
installer/modifier so either appropriate
design considerations or operating
procedures, or both, can be developed to
prevent airframe and propeller damage.
14. Powerplant Installation—High
Energy Engine Fragments:
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It may be possible for diesel engine
cylinders (or portions thereof) to fail
and physically separate from the engine
at high velocity (due to the high internal
pressures). This failure mode will be
considered possible in engine designs
with removable cylinders or other nonintegral block designs. The following is
required:
a. It must be shown that the engine
construction type (massive or integral
block with non-removable cylinders) is
inherently resistant to liberating high
energy fragments in the event of a
catastrophic engine failure; or,
b. It must be shown by the design of
the engine, that engine cylinders, other
engine components or portions thereof
(fragments) cannot be shed or blown off
the engine in the event of a catastrophic
engine failure; or
c. It must be shown that all possible
liberated engine parts or components do
not have adequate energy to penetrate
engine cowlings; or
d. Assuming infinite fragment energy,
and analyzing the trajectory of the
probable fragments and components,
any hazard due to liberated engine parts
or components will be minimized and
the possibility of crew injury is
eliminated. Minimization must be
considered during initial design and not
presented as an analysis after design
completion.
Issued in Kansas City, Missouri, on
October 3, 2019.
William Schinstock,
Acting Manager, Small Airplane Standards
Branch, Policy and Innovation Division,
Aircraft Certification Service.
[FR Doc. 2019–22118 Filed 10–9–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0497; Product
Identifier 2019–NM–052–AD; Amendment
39–19751; AD 2019–19–15]
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 certain
Airbus SAS Model A318, A319, A320,
and A321 series airplanes. This AD was
prompted by a determination that new
SUMMARY:
E:\FR\FM\10OCR1.SGM
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Federal Register / Vol. 84, No. 197 / Thursday, October 10, 2019 / Rules and Regulations
or more restrictive airworthiness
limitations are necessary. This AD
requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective November
14, 2019.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of November 14, 2019.
ADDRESSES: For service information
identified in this final rule, contact
Airbus, Airworthiness Office—EIAS, 1
Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France; telephone +33 5
61 93 36 96; fax +33 5 61 93 44 51; email
account.airworth-eas@airbus.com;
internet https://www.airbus.com. You
may view this service information at the
FAA, Transport Standards Branch, 2200
South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
It is also available on the internet at
https://www.regulations.gov by searching
for and locating Docket No. FAA–2019–
0497.
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–2019–
0497; 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:
Sanjay Ralhan, Aerospace Engineer,
International Section, Transport
Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax 206–231–3223.
SUPPLEMENTARY INFORMATION:
Discussion
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2019–0056, dated March 19, 2019
(referred to after this as the Mandatory
Continuing Airworthiness Information,
or ‘‘the MCAI’’), to correct an unsafe
condition for all Airbus SAS Model
A318, A319, A320, and A321 series
VerDate Sep<11>2014
16:03 Oct 09, 2019
Jkt 250001
airplanes. You may examine the MCAI
in the AD docket on the internet at
https://www.regulations.gov by searching
for and locating Docket No. FAA–2019–
0497.
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
A318, A319, A320, and A321 series
airplanes. The NPRM published in the
Federal Register on July 1, 2019 (84 FR
31244). The NPRM was prompted by a
determination that new or more
restrictive airworthiness limitations are
necessary. The NPRM proposed to
require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations.
The FAA is issuing this AD to address
the failure of certain life-limited parts,
which could result in reduced structural
integrity 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 Service Information Under 1
CFR Part 51
Airbus has issued Airbus A318/A319/
A320/A321 Airworthiness Limitations
Section (ALS) Part 1 Safe Life
Airworthiness Limitations (SL–ALI),
Revision 06, Issue 02, dated November
30, 2018. This service information
describes new maintenance
requirements and airworthiness
limitations. This service information is
reasonably available because the
interested parties have access to it
through their normal course of business
or by the means identified in the
ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD
affects 1,497 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
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54481
The FAA has determined that revising
the existing maintenance or inspection
program takes an average of 90 workhours per operator, although the agency
recognizes that this number may vary
from operator to operator. In the past,
the FAA has estimated that this action
takes 1 work-hour per airplane. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), the FAA has
determined that a per-operator estimate
is more accurate than a per-airplane
estimate. Therefore, the FAA estimates
the total cost per operator to be $7,650
(90 work-hours × $85 per work-hour).
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.
We are 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
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:
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10OCR1
54482
Federal Register / Vol. 84, No. 197 / Thursday, October 10, 2019 / Rules and Regulations
(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.
this AD to address the failure of certain lifelimited parts, which could result in reduced
structural integrity of the airplane.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Within 90 days after the effective date of
this AD, revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
Airbus A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part
1 Safe Life Airworthiness Limitations (SL–
ALI), Revision 06, Issue 02, dated November
30, 2018. The initial compliance time for
doing the tasks is at the time specified in
Airbus A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part
1 Safe Life Airworthiness Limitations (SL–
ALI), Revision 06, Issue 02, dated November
30, 2018, or within 90 days after the effective
date of this AD, whichever occurs later.
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 (AD):
■
2019–19–15 Airbus SAS: Amendment 39–
19751; Docket No. FAA–2019–0497;
Product Identifier 2019–NM–052–AD.
(a) Effective Date
This AD is effective November 14, 2019.
(b) Affected ADs
This AD affects AD 2018–17–19,
Amendment 39–19373 (83 FR 44460, August
31, 2018) (‘‘AD 2018–17–19’’).
(c) Applicability
This AD applies to the Airbus SAS
airplanes identified in paragraphs (c)(1)
through (4) of this AD, certificated in any
category, with an original airworthiness
certificate or original export certificate of
airworthiness issued on or before November
30, 2018.
(1) Model A318–111, –112, –121, and –122
airplanes.
(2) Model A319–111, –112, –113, –114,
–115, –131, –132, and –133 airplanes.
(3) Model A320–211, –212, –214, –216,
–231, –232, –233, –251N, and –271N
airplanes.
(4) Model A321–111, –112, –131, –211,
–212, –213, –231, –232, –251N, –251NX,
–252N, –252NX, –253N, –253NX, –271N,
–271NX, –272N, and –272NX airplanes.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time Limits/Maintenance
Checks.
(e) Reason
This AD was prompted by a determination
that new or more restrictive airworthiness
limitations are necessary. The FAA is issuing
VerDate Sep<11>2014
16:03 Oct 09, 2019
Jkt 250001
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Maintenance or Inspection Program
Revision
(h) No Alternative Actions, Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative life limits may be used unless
approved as an alternative method of
compliance (AMOC) in accordance with the
procedures specified in paragraph (j)(1) of
this AD.
(i) Terminating Action for AD 2018–17–19
Accomplishing the actions required by this
AD terminates all requirements of AD 2018–
17–19.
(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)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOCREQUESTS@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 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
DOA-authorized signature.
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Fmt 4700
Sfmt 4700
(k) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2019–0056, dated March 19, 2019; 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–2019–0497.
(2) For more information about this AD,
contact Sanjay Ralhan, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax 206–
231–3223.
(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) Airbus A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part
1 Safe Life Airworthiness Limitations (SL–
ALI), Revision 06, Issue 02, dated November
30, 2018.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Airbus, Airworthiness
Office—EIAS, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5 61
93 44 51; email account.airworth-eas@
airbus.com; internet https://www.airbus.com.
(4) 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.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Des Moines, Washington, on
September 23, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–22153 Filed 10–9–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2018–0495; Product
Identifier 2017–NM–089–AD; Amendment
39–19716; AD 2019–16–13]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
AGENCY:
E:\FR\FM\10OCR1.SGM
10OCR1
Agencies
[Federal Register Volume 84, Number 197 (Thursday, October 10, 2019)]
[Rules and Regulations]
[Pages 54480-54482]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-22153]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0497; Product Identifier 2019-NM-052-AD; Amendment
39-19751; AD 2019-19-15]
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 A318, A319, A320, and A321 series airplanes.
This AD was prompted by a determination that new
[[Page 54481]]
or more restrictive airworthiness limitations are necessary. This AD
requires revising the existing maintenance or inspection program, as
applicable, to incorporate new or more restrictive airworthiness
limitations. The FAA is issuing this AD to address the unsafe condition
on these products.
DATES: This AD is effective November 14, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 14,
2019.
ADDRESSES: For service information identified in this final rule,
contact Airbus, Airworthiness Office--EIAS, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax
+33 5 61 93 44 51; email [email protected]; internet
https://www.airbus.com. You may view this service information at the
FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA.
For information on the availability of this material at the FAA, call
206-231-3195. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0497.
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-2019-
0497; 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: Sanjay Ralhan, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax 206-231-3223.
SUPPLEMENTARY INFORMATION:
Discussion
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0056, dated March 19, 2019 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for all Airbus SAS Model A318, A319, A320,
and A321 series airplanes. You may examine the MCAI in the AD docket on
the internet at https://www.regulations.gov by searching for and
locating Docket No. FAA-2019-0497.
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 A318, A319, A320, and A321 series airplanes. The NPRM published
in the Federal Register on July 1, 2019 (84 FR 31244). The NPRM was
prompted by a determination that new or more restrictive airworthiness
limitations are necessary. The NPRM proposed to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations.
The FAA is issuing this AD to address the failure of certain life-
limited parts, which could result in reduced structural integrity 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 Service Information Under 1 CFR Part 51
Airbus has issued Airbus A318/A319/A320/A321 Airworthiness
Limitations Section (ALS) Part 1 Safe Life Airworthiness Limitations
(SL-ALI), Revision 06, Issue 02, dated November 30, 2018. This service
information describes new maintenance requirements and airworthiness
limitations. This service information is reasonably available because
the interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 1,497 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. In the past, the FAA has estimated that this action takes
1 work-hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the FAA estimates the total cost per
operator to be $7,650 (90 work-hours x $85 per work-hour).
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.
We are 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 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:
[[Page 54482]]
(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):
2019-19-15 Airbus SAS: Amendment 39-19751; Docket No. FAA-2019-0497;
Product Identifier 2019-NM-052-AD.
(a) Effective Date
This AD is effective November 14, 2019.
(b) Affected ADs
This AD affects AD 2018-17-19, Amendment 39-19373 (83 FR 44460,
August 31, 2018) (``AD 2018-17-19'').
(c) Applicability
This AD applies to the Airbus SAS airplanes identified in
paragraphs (c)(1) through (4) of this AD, certificated in any
category, with an original airworthiness certificate or original
export certificate of airworthiness issued on or before November 30,
2018.
(1) Model A318-111, -112, -121, and -122 airplanes.
(2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133
airplanes.
(3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N,
and -271N airplanes.
(4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -
251N, -251NX, -252N, -252NX, -253N, -253NX, -271N, -271NX, -272N,
and -272NX airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Reason
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address the failure of certain life-limited
parts, which could result in reduced structural integrity of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision
Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Airbus A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part 1 Safe Life
Airworthiness Limitations (SL-ALI), Revision 06, Issue 02, dated
November 30, 2018. The initial compliance time for doing the tasks
is at the time specified in Airbus A318/A319/A320/A321 Airworthiness
Limitations Section (ALS) Part 1 Safe Life Airworthiness Limitations
(SL-ALI), Revision 06, Issue 02, dated November 30, 2018, or within
90 days after the effective date of this AD, whichever occurs later.
(h) No Alternative Actions, Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative life
limits may be used unless approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (j)(1) of this AD.
(i) Terminating Action for AD 2018-17-19
Accomplishing the actions required by this AD terminates all
requirements of AD 2018-17-19.
(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)(2) 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 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 DOA-authorized signature.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2019-0056, dated March 19, 2019; 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-2019-0497.
(2) For more information about this AD, contact Sanjay Ralhan,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax 206-231-3223.
(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) Airbus A318/A319/A320/A321 Airworthiness Limitations Section
(ALS) Part 1 Safe Life Airworthiness Limitations (SL-ALI), Revision
06, Issue 02, dated November 30, 2018.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Airbus, Airworthiness Office--EIAS, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5
61 93 44 51; email [email protected]; internet https://www.airbus.com.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on September 23, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-22153 Filed 10-9-19; 8:45 am]
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