Proposed Rule2023-13011
Airworthiness Directives; Airbus SAS Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
June 20, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A330-200 series; A330-200 Freighter series; A330-300 series; A330-800 series; A330-900 series; A340-200 series; and A340-300 series airplanes. This proposed AD was prompted by reports of cracks found in the scroll housing assembly of Honeywell GTCP331-350 auxiliary power units (APUs). This proposed AD would require replacing each affected APU or re-identifying certain APU scroll housing assemblies, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). This proposed AD would also prohibit the installation of affected parts under certain conditions. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
<html>
<head>
<title>Federal Register, Volume 88 Issue 117 (Tuesday, June 20, 2023)</title>
</head>
<body><pre>
[Federal Register Volume 88, Number 117 (Tuesday, June 20, 2023)]
[Proposed Rules]
[Pages 39796-39799]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2023-13011]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1217; Project Identifier MCAI-2023-00477-T]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Airbus SAS Model A330-200 series; A330-200 Freighter series;
A330-300 series; A330-800 series; A330-900 series; A340-200 series; and
A340-300 series airplanes. This proposed AD was prompted by reports of
cracks found in the scroll housing assembly of Honeywell GTCP331-350
auxiliary power units (APUs). This proposed AD would require replacing
each affected APU or re-identifying certain APU scroll housing
assemblies, as specified in a European Union Aviation Safety Agency
(EASA) AD, which is proposed for incorporation by reference (IBR). This
proposed AD would also prohibit the installation of affected parts
under certain conditions. The FAA is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by August 4,
2023.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2023-1217; 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 NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
<bullet> For EASA material that is proposed for IBR in this NPRM,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#19585d6a597c786a78377c6c6b766978377c6c"><span class="__cf_email__" data-cfemail="8ecfcafdceebeffdefa0ebfbfce1feefa0ebfb">[email protected]</span></a>; website easa.europa.eu. You
may find this material on the EASA website at ad.easa.europa.eu. It is
also available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2023-1217.
<bullet> For Honeywell service information identified in this NPRM,
contact Honeywell International, Inc., 111 South 34th Street, Phoenix,
AZ 85034; phone: (800) 601-3099; fax: (602) 365-5577; website:
<a href="http://myaerospace.honeywell.com/wps/portal">myaerospace.honeywell.com/wps/portal</a>.
<bullet> You may view this service information 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.
FOR FURTHER INFORMATION CONTACT: Timothy Dowling, Aviation Safety
[[Page 39797]]
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone 206-231-3667; email <a href="/cdn-cgi/l/email-protection#8bdfe2e6e4ffe3f2a5dba5cfe4fce7e2e5eccbedeaeaa5ece4fd"><span class="__cf_email__" data-cfemail="7d29141012091504532d5339120a1114131a3d1b1c1c531a120b">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2023-1217; Project Identifier
MCAI-2023-00477-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="http://regulations.gov">regulations.gov</a>, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Timothy Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone 206-231-3667; email
<a href="/cdn-cgi/l/email-protection#73271a1e1c071b0a5d235d371c041f1a1d14331512125d141c05"><span class="__cf_email__" data-cfemail="ecb8858183988495c2bcc2a8839b8085828bac8a8d8dc28b839a">[email protected]</span></a>. Any commentary that the FAA receives which
is not specifically designated as CBI will be placed in the public
docket for this rulemaking.
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2023-0056, dated March 16, 2023
(EASA AD 2023-0056) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus SAS Model 330-201, -202, -203, -223, -
223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, -
343, -841, -941, and -743L airplanes, and Model A340-211, -212, -213, -
311, -312, and -313 airplanes. Model A330-743L airplanes are not
certificated by the FAA and are not included on the U.S. type
certificate data sheet; this proposed AD therefore does not include
those airplanes in the applicability. The MCAI states that cracks were
found in the scroll housing assembly of Honeywell GTCP331-350 APUs.
This condition, if not addressed, could lead to hot air leakage and
consequent damage to the APU compartment and loss of the APU doors,
possibly resulting in damage to the airplane.
The FAA is proposing this AD to address the unsafe condition on
these products.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2023-1217.
Related Service Information Under 1 CFR Part 51
EASA AD 2023-0056 specifies procedures for replacing each affected
APU or re-identifying certain APU scroll housing assemblies (those
having part number (P/N) 5053-181-001-501 or P/N 0331207990 and `SR-1'
next to the part number marking). EASA AD 2023-0056 also prohibit the
installation of affected parts under certain conditions.
Honeywell Service Bulletin 5053-181-49-7895, dated July 21, 2006,
specifies procedures for, among other actions, re-identifying affected
APU scroll housing assemblies. While Honeywell distributes this
document, Aeronamic develops the technical content.
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 ADDRESSES.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI and
service information referenced above. The FAA is issuing this NPRM
after determining that the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in EASA AD 2023-0056 described previously, except for any differences
identified as exceptions in the regulatory text of this proposed AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate EASA AD 2023-0056 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2023-0056 in its entirety through that incorporation, except
for any differences identified as exceptions in the regulatory text of
this proposed AD. Using common terms that are the same as the heading
of a particular section in EASA AD 2023-0056 does not mean that
operators need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2023-
0056. Service information required by EASA AD 2023-0056 for compliance
will be available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2023-1217
after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 128 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
[[Page 39798]]
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Labor cost Parts cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 18 work-hours x $85 per hour = $1,612,820 Up to $1,614,350............... (*)
$1,530 (replace APU).
Up to 20 work-hours x $85 per hour = 3,141 Up to $4,841................... (*)
$1,700 (re-identify APU scroll
housing assembly).
----------------------------------------------------------------------------------------------------------------
* Operators have the option to replace the APU or re-identify the APU scroll housing assembly. Replacement or re-
identification is only required if an affected part is installed on an airplane. The FAA has no way of knowing
how many affected parts are installed on U.S.-registered airplanes or which option an operator will choose for
a given airplane with an affected part. Therefore, the FAA has no definitive data on which to provide a fleet
cost estimate for the required actions specified in this proposed AD.
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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
Airbus SAS: Docket No. FAA-2023-1217; Project Identifier MCAI-2023-
00477-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 4, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus SAS airplanes specified in
paragraphs (c)(1) through (7) of this AD, certificated in any
category.
(1) Model A330-201, -202, -203, -223, and -243 airplanes.
(2) Model A330-223F and -243F airplanes.
(3) Model A330-301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes.
(4) Model A330-841 airplanes.
(5) Model A330-941 airplanes.
(6) Model A340-211, -212, and -213 airplanes.
(7) Model A340-311, -312, and -313 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 49, Airborne
auxiliary power.
(e) Unsafe Condition
This AD was prompted by reports of cracks found in the scroll
housing assembly of Honeywell GTCP331-350 auxiliary power units
(APUs). The FAA is issuing this AD to address such cracks. The
unsafe condition, if not addressed, could result in hot air leakage
and consequent damage to the APU compartment and loss of the APU
doors, possibly resulting in damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2023-0056, dated March 16, 2023 (EASA AD 2023-0056).
(h) Exceptions to EASA AD 2023-0056
(1) Where EASA AD 2023-0056 refers to its effective date, this
AD requires using the effective date of this AD.
(2) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0056.
(3) Where EASA AD 2023-0056 specifies to re-identify an SR-1
affected part ``in accordance with the instructions of the SB,'' for
this AD, operators must use Honeywell Service Bulletin 5053-181-49-
7895, dated July 21, 2006.
Note 1 to paragraph (h)(3): Honeywell distributes this document;
Aeronamic develops the technical content.
(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#dae3f79b8c89f79b9388f7ede9eaf79b9795999abcbbbbf4bdb5ac"><span class="__cf_email__" data-cfemail="4f76620e191c620e061d62787c7f620e02000c0f292e2e61282039">[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
[[Page 39799]]
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) Additional Information
For more information about this AD, contact Timothy Dowling,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone 206-231-3667; email
<a href="/cdn-cgi/l/email-protection#63370a0e0c170b1a4d334d270c140f0a0d04230502024d040c15"><span class="__cf_email__" data-cfemail="3e6a5753514a5647106e107a5149525750597e585f5f10595148">[email protected]</span></a>.
(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.
(i) European Union Aviation Safety Agency (EASA) AD 2023-0056,
dated March 16, 2023.
(ii) Honeywell Service Bulletin 5053-181-49-7895, dated July 21,
2006.
Note 2 to paragraph (k)(2)(ii): Honeywell distributes this
document; Aeronamic develops the technical content.
(3) For EASA AD 2023-0056, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#97d6d3e4d7f2f6e4f6b9f2e2e5f8e7f6b9f2e2"><span class="__cf_email__" data-cfemail="96d7d2e5d6f3f7e5f7b8f3e3e4f9e6f7b8f3e3">[email protected]</span></a>; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) For Honeywell service information identified in this AD,
contact Honeywell service information identified in this AD, contact
Honeywell International, Inc., 111 South 34th Street, Phoenix, AZ
85034; phone: (800) 601-3099; fax: (602) 365-5577; website:
<a href="http://myaerospace.honeywell.com/wps/portal">myaerospace.honeywell.com/wps/portal</a>.
(5) You may view this service information 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.
(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 <a href="/cdn-cgi/l/email-protection#5c3a2e7235322f2c393f283533321c323d2e3d723b332a"><span class="__cf_email__" data-cfemail="1c7a6e3275726f6c797f687573725c727d6e7d327b736a">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on June 13, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-13011 Filed 6-16-23; 8:45 am]
BILLING CODE 4910-13-P
</pre><script data-cfasync="false" src="/cdn-cgi/scripts/5c5dd728/cloudflare-static/email-decode.min.js"></script></body>
</html>Indexed from Federal Register on June 20, 2023.
This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.