Airworthiness Directives; Airbus SAS Airplanes
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Issuing agencies
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A318, A319, A320, and A321 series airplanes. This AD was prompted by unclear and incomplete placard instructions for the doghouse door lock. This AD requires installing improved handling instruction placards on affected doghouses and re-identifying the doghouses, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also prohibits the installation of affected doghouses under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 87 Issue 173 (Thursday, September 8, 2022)</title>
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[Federal Register Volume 87, Number 173 (Thursday, September 8, 2022)]
[Rules and Regulations]
[Pages 54863-54865]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-19279]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0675; Project Identifier MCAI-2021-01406-T;
Amendment 39-22156; AD 2022-18-05]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Airbus SAS Model A318, A319, A320, and A321 series airplanes. This AD
was prompted by unclear and incomplete placard instructions for the
doghouse door lock. This AD requires installing improved handling
instruction placards on affected doghouses and re-identifying the
doghouses, as specified in a European Union Aviation Safety Agency
(EASA) AD, which is incorporated by reference. This AD also prohibits
the installation of affected doghouses under certain conditions. The
FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective October 13, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 13,
2022.
ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#0342477043666270622d6676716c73622d6676"><span class="__cf_email__" data-cfemail="eaabae99aa8f8b998bc48f9f98859a8bc48f9f">[email protected]</span></a>; internet easa.europa.eu.
You may find this IBR material on the EASA website at
ad.easa.europa.eu. You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St., Des
Moines, WA. For information on the availability of this material at the
FAA, call 206-231-3195. It is also available in the AD docket at
<a href="http://regulations.gov">regulations.gov</a> by searching for and locating Docket No. FAA-2022-0675.
[[Page 54864]]
Examining the AD Docket
You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> by searching for
and locating Docket No. FAA-2022-0675; 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 mandatory
continuing airworthiness information (MCAI), any comments received, and
other information. The address for Docket Operations is U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229;
email <a href="/cdn-cgi/l/email-protection#f5a39994919c989c87dba0998c949b9a83b5939494db929a83"><span class="__cf_email__" data-cfemail="94c2f8f5f0fdf9fde6bac1f8edf5fafbe2d4f2f5f5baf3fbe2">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0279, dated December 15, 2021
(EASA AD 2021-0279) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus SAS Model Airbus A318-111, A318-112,
A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115,
A319-131, A319-132, A319-133, A319-151N, A319-153N, A319-171N, A320-
211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-
233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N,
A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231,
A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N,
A321-253NX, A321-271N, A321-271NX, A321-272N, and A321-272NX airplanes.
Model A320-215 airplanes are not certificated by the FAA and are not
included on the U.S. type certificate data sheet; this AD therefore
does not include those airplanes in the applicability.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all Airbus SAS Model
A318, A319, A320, and A321 series airplanes. The NPRM published in the
Federal Register on June 13, 2022 (87 FR 35684). The NPRM was prompted
by unclear and incomplete placard instructions for the doghouse door
lock. The NPRM proposed to require installing improved handling
instruction placards on affected doghouses and re-identifying the
doghouses, as specified in EASA AD 2021-0279. The NPRM also proposed to
prohibit the installation of affected doghouses under certain
conditions.
The FAA is issuing this AD to address the possible failure of the
doghouse door lock latch, which could result in locking the door in the
closed position and preventing access to the emergency equipment in the
doghouse, possibly resulting in injury to occupants. See the MCAI for
additional background information.
Discussion of Final Airworthiness Directive
Comments
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
requires adopting this AD as proposed. Except for minor editorial
changes, this AD is adopted as proposed in the NPRM. None of the
changes will increase the economic burden on any operator. Accordingly,
the FAA is issuing this AD to address the unsafe condition on these
products.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0279 specifies procedures for installing improved
handling instruction placards on affected doghouses and re-identifying
the doghouses, and prohibits installation of affected doghouses under
certain conditions. 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 would affect 1,825 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Labor cost Parts cost product operators
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1 work-hour x $85 per hour = $85............................. $ * $85 $155,125
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* The FAA has received no definitive data on which to base the cost estimates for the replacement placards
specified in this AD.
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.
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,
[[Page 54865]]
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.
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:
2022-18-05 Airbus SAS: Amendment 39-22156; Docket No. FAA-2022-0675;
Project Identifier MCAI-2021-01406-T.
(a) Effective Date
This airworthiness directive (AD) is effective October 13, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the Airbus SAS airplanes identified in
paragraphs (c)(1) through (4) of this AD, certificated in any
category.
(1) All Model A318-111, A318-112, A318-121, and A318-122
airplanes.
(2) All Model A319-111, A319-112, A319-113, A319-114, A319-115,
A319-131, A319-132, A319-133, A319-151N, A319-153N, and A319-171N
airplanes.
(3) All Model A320-211, A320-212, A320-214, A320-216, A320-231,
A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N,
A320-272N, and A320-273N airplanes.
(4) All Model A321-111, A321-112, A321-131, A321-211, A321-212,
A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N,
A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N,
and A321-272NX airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by unclear and incomplete placard
instructions for the doghouse door lock, which could lead to
incorrect operation of the doghouse door lock. The FAA is issuing
this AD to address the possible failure of the doghouse door lock
latch, which could result in locking the door in the closed position
and preventing access to the emergency equipment in the doghouse,
possibly resulting in injury to occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2021-0279, dated December 15, 2021 (EASA AD 2021-0279).
(h) Exceptions to EASA AD 2021-0279
(1) Where EASA AD 2021-0279 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2021-0279 does not apply
to this AD.
(3) Where paragraph (1) of EASA AD 2021-0279 refers to affected
airplanes, replace the text ``For Group 1 aeroplanes'' with ``Group
1 airplanes except for airplanes identified in paragraph (2) of EASA
AD 2021-0279.''
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (j) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#0b32264a5d58264a4259263c383b264a4644484b6d6a6a256c647d"><span class="__cf_email__" data-cfemail="8ab3a7cbdcd9a7cbc3d8a7bdb9baa7cbc7c5c9caecebeba4ede5fc">[email protected]</span></a>. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or EASA; or Airbus SAS's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(3) Required for Compliance (RC): Except as required by
paragraph (i)(2) of this AD, 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.
(j) Related Information
For more information about this AD, contact Vladimir Ulyanov,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 206-231-3229; email <a href="/cdn-cgi/l/email-protection#80d6ece1e4e9ede9f2aed5ecf9e1eeeff6c0e6e1e1aee7eff6"><span class="__cf_email__" data-cfemail="87d1ebe6e3eeeaeef5a9d2ebfee6e9e8f1c7e1e6e6a9e0e8f1">[email protected]</span></a>.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 2021-0279,
dated December 15, 2021.
(ii) [Reserved]
(3) For EASA AD 2021-0279, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#b1f0f5c2f1d4d0c2d09fd4c4c3dec1d09fd4c4"><span class="__cf_email__" data-cfemail="6e2f2a1d2e0b0f1d0f400b1b1c011e0f400b1b">[email protected]</span></a>; internet easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St.,
Des Moines, WA. For information on the availability of this material
at the FAA, call 206-231-3195.
(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
<a href="/cdn-cgi/l/email-protection#066074286f6875766365726f6968466867746728616970"><span class="__cf_email__" data-cfemail="94f2e6bafdfae7e4f1f7e0fdfbfad4faf5e6f5baf3fbe2">[email protected]</span></a>, or go to: <a href="http://archives.gov/federal-register/cfr/ibr-locations.html">archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on August 17, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-19279 Filed 9-7-22; 8:45 am]
BILLING CODE 4910-13-P
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