AD 2019-03-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
A safety-significant latent failure (that is not annunciated), which, in combination with one or more other specific failures or events, could result in a hazardous or catastrophic failure condition.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revising the operator's maintenance or inspection program, as applicable, to incorporate new maintenance requirements and airworthiness limitations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 work-hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320 series airplanes; and Model A321 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320 series airplanes; and Model A321 series airplanes. This AD was prompted by a revision of an airworthiness limitation item (ALI) document, which requires more restrictive maintenance requirements and airworthiness limitations. This AD requires revising the operator's maintenance or inspection program, as applicable, to incorporate new maintenance requirements and airworthiness limitations. We are issuing this AD to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to the Airbus SAS airplanes identified in
paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD,
certificated in any category, with an original certificate of
airworthiness or original export certificate of airworthiness issued
on or before June 13, 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.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 84, Number 39 (Wednesday, February 27, 2019)]
[Rules and Regulations]
[Pages 6315-6317]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2019-03268]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0554; Product Identifier 2018-NM-064-AD; Amendment
39-19569; AD 2019-03-17]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Airbus SAS Model A318 series airplanes; Model A319 series airplanes;
Model A320 series airplanes; and Model A321 series airplanes. This AD
was prompted by a revision of an airworthiness limitation item (ALI)
document, which requires more restrictive maintenance requirements and
airworthiness limitations. This AD requires revising the operator's
maintenance or inspection program, as applicable, to incorporate new
maintenance requirements and airworthiness limitations. We are issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective April 3, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 3,
2019.
ADDRESSES: For service information identified in this final rule,
contact Airbus SAS, Airworthiness Office--EIAS, Rond-Point Emile
Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36
96; fax +33 5 61 93 44 51; email <a href="/cdn-cgi/l/email-protection#2f4e4c4c405a415b014e465d58405d5b47024a4e5c6f4e465d4d5a5c014c4042"><span class="__cf_email__" data-cfemail="234240404c564d570d424a51544c51574b0e46425063424a514156500d404c4e">[email protected]</span></a>;
internet <a href="http://www.airbus.com">http://www.airbus.com</a>. 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0554.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0554; 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 (phone: 800-647-
5527) 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
We 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 series airplanes; Model A319 series airplanes; Model A320 series
airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, -
232, -251N, -253N, and -271N airplanes. The NPRM published in the
Federal Register on July 17, 2018 (83 FR 33159). The NPRM was prompted
by a revision of an ALI document, which requires more restrictive
maintenance requirements and airworthiness limitations. The NPRM
proposed to require revising the operator's maintenance or inspection
program, as applicable, to incorporate new maintenance requirements and
airworthiness limitations.
We issued a supplemental NPRM (SNPRM) to amend 14 CFR part 39 by
adding an AD that would apply to certain Airbus SAS Model A318 series
airplanes; Model A319 series airplanes; Model A320 series airplanes;
and Model A321 series airplanes. The SNPRM published in the Federal
Register on November 8, 2018 (83 FR 55830). We issued the SNPRM to
include revised restrictive requirements and add airplanes to the
applicability.
We are issuing this AD to address a safety-significant latent
failure (that is not annunciated), which, in combination with one or
more other specific failures or events, could result in a hazardous or
catastrophic failure condition.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2018-0180, dated August 27, 2018 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for certain Airbus SAS Model A318 series
airplanes; Model A319 series airplanes; Model A320 series airplanes;
and Model A321 series airplanes. The MCAI states:
The airworthiness limitations for the Airbus A320 family
aeroplanes, which are approved by EASA, are currently defined and
published in the A318/A319/A320/A321 ALS [Airworthiness Limitations
Section] document(s). The airworthiness limitations applicable to
the Certification Maintenance Requirements (CMR), which are approved
by EASA, are published in ALS Part 3.
Failure to accomplish these instructions could result in an
unsafe condition.
Previously, EASA issued AD 2017-0168 to require accomplishment
of all maintenance tasks as described in ALS Part 3 at Revision 05.
[[Page 6316]]
Since that [EASA] AD was issued, Airbus published the ALS,
including new and/or more restrictive requirements, and new A321
models were certified and added to the Applicability of the ALS.
For the reason described above, this [EASA] AD retains the
requirements of EASA AD 2017-0168, which is superseded, expands the
Applicability and requires accomplishment of the actions specified
in the ALS.
You may examine the MCAI in the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0554.
Comments
We gave the public the opportunity to participate in developing
this final rule. We have considered the comment received. United
Airlines indicated its support for the SNPRM.
Conclusion
We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this final rule as proposed, except for minor editorial changes. We
have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
SNPRM for addressing the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the SNPRM.
Related Service Information Under 1 CFR Part 51
Airbus has issued Airbus A318/A319/A320/A321 Airworthiness
Limitations Section (ALS) Part 3, Certification Maintenance
Requirements (CMR), Revision 06, dated June 13, 2018. The service
information describes maintenance instructions and airworthiness
limitations, including updated inspections and intervals, to be
incorporated into the operator's maintenance or inspection program.
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
We estimate that this AD affects 1,250 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
We have determined that revising the operator's maintenance or
inspection program takes an average of 90 work-hours per operator,
although we recognize that this number may vary from operator to
operator. In the past, we have estimated that this action takes 1 work-
hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), we have
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, we estimate 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:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) 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):
2019-03-17 Airbus SAS: Amendment 39-19569; Docket No. FAA-2018-0554;
Product Identifier 2018-NM-064-AD.
(a) Effective Date
This AD is effective April 3, 2019.
(b) Affected ADs
This AD affects AD 2017-25-04, Amendment 39-19118 (82 FR 58098,
December 11, 2017) (``AD 2017-25-04'').
(c) Applicability
This AD applies to the Airbus SAS airplanes identified in
paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD,
certificated in any category, with an original certificate of
airworthiness or original export certificate of airworthiness issued
on or before June 13, 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 revision of an airworthiness
limitation item (ALI) document, which requires more restrictive
maintenance requirements and airworthiness limitations. We are
issuing this AD to address a safety-significant latent failure (that
is not annunciated), which, in combination with one or more other
specific failures or events,
[[Page 6317]]
could result in a hazardous or catastrophic failure condition.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of Maintenance or Inspection Program
Within 90 days after the effective date of this AD, revise the
operator's maintenance or inspection program, as applicable, to
incorporate the information specified in Airbus A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part 3, Certification
Maintenance Requirements (CMR), Revision 06, dated June 13, 2018
(``ALS Part 3, CMR, R6''). The initial compliance time for
accomplishing the tasks specified in ALS Part 3, CMR, R6, is at the
applicable time specified in ALS Part 3, CMR, R6, or within 90 days
after the effective date of this AD, whichever occurs later.
(h) Terminating Actions for AD 2017-25-04
Accomplishing the actions required by paragraph (g) of this AD
terminates all of the requirements of AD 2017-25-04.
(i) No Alternative Actions or Intervals
After the operator's maintenance or inspection program, as
applicable, has been revised as required by paragraph (g) of this
AD, no alternative actions (e.g., inspections) or intervals may be
used unless the actions and intervals are approved as an alternative
method of compliance (AMOC) in accordance with the procedures
specified in paragraph (j)(1) of this AD.
(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: <a href="/cdn-cgi/l/email-protection#b68f9bf7f8fb9b8787809bf7fbf9f59be4f3e7e3f3e5e2e5f6d0d7d798d1d9c0"><span class="__cf_email__" data-cfemail="fdc4d0bcb3b0d0cccccbd0bcb0b2bed0afb8aca8b8aea9aebd9b9c9cd39a928b">[email protected]</span></a>.
(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 2017-25-04, or AD 2014-22-
08, Amendment 39-18013 (79 FR 67042, November 12, 2014), that allow
incorporation of ALS Part 3, CMR, R6, are considered approved as
AMOCs for the corresponding provisions of this AD.
(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 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.
(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 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
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0180, dated August 27, 2018, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2018-0554.
(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 3, Certification Maintenance Requirements (CMR), Revision
06, dated June 13, 2018.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Airbus SAS, Airworthiness Office--EIAS, Rond-Point Emile Dewoitine
No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax
+33 5 61 93 44 51; email <a href="/cdn-cgi/l/email-protection#630200000c160d174d020a11140c11170b4e06021023020a110116104d000c0e"><span class="__cf_email__" data-cfemail="badbd9d9d5cfd4ce94dbd3c8cdd5c8ced297dfdbc9fadbd3c8d8cfc994d9d5d7">[email protected]</span></a>; internet
<a href="http://www.airbus.com">http://www.airbus.com</a>.
(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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Des Moines, Washington, on February 14, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-03268 Filed 2-26-19; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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