Proposed Rule2022-28613
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
January 12, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). This proposed AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This proposed AD would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 88 Issue 8 (Thursday, January 12, 2023)</title>
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[Federal Register Volume 88, Number 8 (Thursday, January 12, 2023)]
[Proposed Rules]
[Pages 2035-2038]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-28613]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1660; Project Identifier MCAI-2022-01268-T]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Airbus SAS Model A300 B4-600, B4-600R, and F4-600R series
airplanes, and Model A300 C4-605R Variant F airplanes (collectively
called Model A300-600 series airplanes). This proposed AD was prompted
by a determination that new or more restrictive airworthiness
limitations are necessary. This proposed AD would require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations, as
specified in a European Union Aviation Safety Agency (EASA) AD, which
is proposed for incorporation by reference (IBR). 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 February
27, 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-2022-1660; 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 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#96d7d2e5d6f3f7e5f7b8f3e3e4f9e6f7b8f3e3"><span class="__cf_email__" data-cfemail="ca8b8eb98aafabb9abe4afbfb8a5baabe4afbf">[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-2022-1660.
<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: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, International Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone 206-231-3225; email
<a href="/cdn-cgi/l/email-protection#5430353a7a263b303d3a35143235357a333b22"><span class="__cf_email__" data-cfemail="b3d7d2dd9dc1dcd7daddd2f3d5d2d29dd4dcc5">[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-2022-1660; Project Identifier
MCAI-2022-01268-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
[[Page 2036]]
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 Dan
Rodina, Aerospace Engineer, Large Aircraft Section, International
Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3225; email <a href="/cdn-cgi/l/email-protection#187c7976366a777c717679587e7979367f776e"><span class="__cf_email__" data-cfemail="e084818ece928f84898e81a0868181ce878f96">[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 2022-0194, dated September 23, 2022
(EASA AD 2022-0194) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus A300B4-601, A300B4-603, A300B4-620,
A300B4-622, A300B4-605R, A300B4-622R, A300C4-605R Variant F, A300C4-
620, A300F4-605R, A300F4-622R, and A300F4-608ST airplanes. Model
A300C4-620 and A300F4-608ST 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 new or more restrictive airworthiness
limitations tasks related to the trimmable horizontal stabilizer
actuators (THSA) are necessary. EASA AD 2022-0194 specifies that
revised tasks (limitations) in Airbus A300-600 Airworthiness
Limitations Section (ALS), Part 4, System Equipment Maintenance
Requirements (SEMR) Revision 03, dated August 28, 2017, are required by
EASA AD 2017-0202, dated October 12, 2017 (which corresponds to FAA AD
2018-18-21, Amendment 39-19400 (83 FR 47054, September 18, 2018) (AD
2018-18-21)). EASA AD 2022-0194 also specifies that incorporation of
EASA AD 2022-0194 invalidates (terminates) prior instructions for the
tasks specified in Airbus A300-600 Airworthiness Limitations Section
(ALS), Part 4, System Equipment Maintenance Requirements (SEMR)
Revision 03, Variation 3.1, dated June 30, 2022, only. For this
proposed AD, the corresponding action is specified in paragraph (j)(2)
of this proposed AD, which states that accomplishing the actions
specified in this proposed AD terminates the corresponding requirements
of AD 2018-18-21, for the tasks identified in the service information
referenced in EASA AD 2022-0194 only.
The MCAI also states that EASA AD 2015-0081, dated May 7, 2015
(EASA AD 2015-0081) requires replacement of certain THSA. EASA AD 2015-
0081 corresponds to FAA AD 2016-15-01, Amendment 39-18592 (81 FR 47696,
July 22, 2016) (AD 2016-15-01). AD 2016-15-01 required inspecting THSA
part numbers, serial numbers, and flight cycles on certain THSAs; and
repetitive replacement of certain THSAs. The THSA limitation task
specified in this proposed AD addresses the actions required by AD
2016-15-01. Paragraph (j)(1) of this proposed AD therefore terminates
AD 2016-15-01, for Model A300-600 series airplanes only.
The FAA is proposing this AD to address the risks associated with
the effects of aging on airplane systems. The unsafe condition, if not
addressed, could change system characteristics, leading to an increased
potential for failure of certain life-limited parts, and reduced
structural integrity or controllability of the airplane. You may
examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under Docket No.
FAA-2022-1660.
Related Service Information Under 1 CFR Part 51
The FAA reviewed EASA AD 2022-0194, which specifies new or more
restrictive airworthiness limitations for certain THSAs. 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 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 the State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
described 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 revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations, which are specified in EASA AD
2022-0194 described previously, as incorporated by reference. Any
differences with EASA AD 2022-0194 are identified as exceptions in the
regulatory text of this proposed AD.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance (AMOC) according to
paragraph (k)(1) 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 2022-0194 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2022-0194 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 2022-0194 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 2022-
0194. Service information required by EASA AD 2022-0194 for compliance
will be available at <a href="http://regulations.gov">regulations.gov</a> by searching for and locating
Docket No. FAA-2022-1660 after the FAA final rule is published.
[[Page 2037]]
Airworthiness Limitation ADs Using the New Process
The FAA's process of incorporating by reference MCAI ADs as the
primary source of information for compliance with corresponding FAA ADs
has been limited to certain MCAI ADs (primarily those with service
bulletins as the primary source of information for accomplishing the
actions required by the FAA AD). However, the FAA is now expanding the
process to include MCAI ADs that require a change to airworthiness
limitation documents, such as airworthiness limitation sections.
For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged.
Operators must revise the existing maintenance or inspection program,
as applicable, to incorporate the information specified in the new
airworthiness limitation document. The airworthiness limitations must
be followed according to 14 CFR 91.403(c) and 91.409(e).
The previous format of the airworthiness limitation ADs included a
paragraph that specified that no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and intervals
are approved as an AMOC in accordance with the procedures specified in
the AMOC paragraph under ``Additional AD Provisions.'' This new format
includes a ``New Provisions for Alternative Actions and Intervals''
paragraph that does not specifically refer to AMOCs, but operators may
still request an AMOC to use an alternative action or interval.
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:
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. 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 agency estimates the average 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.
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 has 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-2022-1660; Project Identifier MCAI-2022-
01268-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by February 27, 2023.
(b) Affected ADs
This AD affects AD 2016-15-01, Amendment 39-18592 (81 FR 47696,
July 22, 2016) (AD 2016-15-01); and AD 2018-18-21, Amendment 39-
19400 (83 FR 47054, September 18, 2018) (AD 2018-18-21).
(c) Applicability
This AD applies to all Airbus SAS Model A300 B4-601, B4-603, B4-
620, and B4-622 airplanes, Model A300 B4-605R and B4-622R airplanes;
and Model A300 C4-605R Variant F airplanes; and Model A300 F4-605R
and F4-622R airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Unsafe Condition
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 risks associated with the effects of
aging on airplane systems. The unsafe condition, if not addressed,
could change system characteristics, leading to an increased
potential for failure of certain life-limited parts, and reduced
structural integrity or controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2022-0194, dated September 23, 2022 (EASA AD 2022-0194).
(h) Exceptions to EASA AD 2022-0194
(1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2022-0194.
(2) Paragraph (3) of EASA AD 2022-0194 specifies revising ``the
approved AMP'' within 12 months after its effective date, but this
AD requires revising the existing maintenance or inspection program,
as applicable, within 90 days after the effective date of this AD.
(3) The initial compliance time for doing the tasks specified in
paragraph (3) of EASA AD 2022-0194 is on or before the applicable
``limitations'' and ``associated thresholds'' as incorporated by the
requirements of paragraph (3) of EASA AD 2022-0194, or within 90
days after the effective date of this AD, whichever occurs later.
(4) This AD does not adopt the provisions specified in paragraph
(4) of EASA AD 2022-0194.
(5) This AD does not adopt the ``Remarks'' section of EASA AD
2022-0194.
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(i) Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals are allowed unless they
are approved as specified in the provisions of the ``Ref.
Publications'' section of EASA AD 2022-0194.
(j) Terminating Actions for AD 2016-15-01 and AD 2018-18-21
(1) Accomplishing the actions required by this AD terminates all
requirements of AD 2016-15-01 for Model A300-600 series airplanes
only.
(2) Accomplishing the actions required by this AD terminates the
corresponding requirements of AD 2018-18-21, for the tasks
identified in the service information referenced in EASA AD 2022-
0194 only.
(k) 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 (l) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#6e57432f383d432f273c43595d5e432f23212d2e080f0f40090118"><span class="__cf_email__" data-cfemail="231a0e6275700e626a710e1410130e626e6c60634542420d444c55">[email protected]</span></a>. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office/
certificate holding district office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
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.
(l) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
206-231-3225; email <a href="/cdn-cgi/l/email-protection#d6b2b7b8f8a4b9b2bfb8b796b0b7b7f8b1b9a0"><span class="__cf_email__" data-cfemail="66020708481409020f08072600070748010910">[email protected]</span></a>.
(m) 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 2022-0194,
dated September 23, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0194, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#2362675063464250420d4656514c53420d4656"><span class="__cf_email__" data-cfemail="4b0a0f380b2e2a382a652e3e39243b2a652e3e">[email protected]</span></a>; website 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#482e3a6621263b382d2b3c2127260826293a29662f273e"><span class="__cf_email__" data-cfemail="1076623e797e6360757364797f7e507e7162713e777f66">[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 December 29, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-28613 Filed 1-11-23; 8:45 am]
BILLING CODE 4910-13-P
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