Rule2023-02530
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
February 7, 2023
Effective
March 14, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting 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), and A310 series airplanes. This AD was prompted by a determination that a new airworthiness limitation is necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate a new airworthiness limitation, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 88 Issue 25 (Tuesday, February 7, 2023)</title>
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[Federal Register Volume 88, Number 25 (Tuesday, February 7, 2023)]
[Rules and Regulations]
[Pages 7862-7864]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2023-02530]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0812; Project Identifier MCAI-2022-00445-T;
Amendment 39-22208; AD 2022-21-09]
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 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), and A310 series airplanes. This AD was
prompted by a determination that a new airworthiness limitation is
necessary. This AD requires revising the existing maintenance or
inspection program, as applicable, to incorporate a new airworthiness
limitation, as specified in a European Union Aviation Safety Agency
(EASA) AD, which is incorporated by reference. The FAA is issuing this
AD to address the unsafe condition on these products.
DATES: This AD is effective March 14, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publications listed in this AD as of March 14,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0812; 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.
Material Incorporated by Reference:
<bullet> For material incorporated by reference 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#1f5e5b6c5f7a7e6c7e317a6a6d706f7e317a6a"><span class="__cf_email__" data-cfemail="f7b6b384b792968496d9928285988796d99282">[email protected]</span></a>; website easa.europa.eu. You may
find this IBR material on the EASA website at ad.easa.europa.eu.
<bullet> You may view this material at the FAA, Airworthiness
Products Section,
[[Page 7863]]
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>
under Docket No. FAA-2022-0812.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, International Validation Branch, FAA, 2200 South
216th Street, Des Moines, WA 98198; telephone 206-231-3225; email
<a href="/cdn-cgi/l/email-protection#5a3e3b347428353e33343b1a3c3b3b743d352c"><span class="__cf_email__" data-cfemail="3a5e5b541448555e53545b7a5c5b5b145d554c">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
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
A300-600 and A310 series airplanes. The NPRM published in the Federal
Register on July 8, 2022 (87 FR 40752). The NPRM was prompted by AD
2022-0060, dated April 1, 2022, issued by EASA, which is the Technical
Agent for the Member States of the European Union (referred to after
this as the MCAI). The MCAI states that a new airworthiness limitation
is necessary. The FAA is issuing this AD to address safety-significant
latent failures that would, in combination with one or more other
specific failures or events, result in a hazardous or catastrophic
failure condition of hydraulic systems.
In the NPRM, the FAA proposed to require revising the existing
maintenance or inspection program, as applicable, to incorporate a new
airworthiness limitation, as specified in EASA AD 2022-0060.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0812.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from the Air Line Pilots Association,
International, which supported the NPRM without change.
Conclusion
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
referenced above. The FAA reviewed the relevant data, considered the
comment received, and determined that air safety requires adopting this
AD as proposed. Accordingly, the FAA is issuing this AD to address the
unsafe condition on this product. 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.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0060 specifies procedures for a new airworthiness
limitation for airplane hydraulic systems: Certification Maintenance
Requirement (CMR) task 291000-00004-1-C ``Main and Auxiliary (Hydraulic
Power)--Functional Check of the 3 Hydraulic Reservoirs for Air
Leakage.''
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 120 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. 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
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, 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:
2022-21-09 Airbus SAS: Amendment 39-22208; Docket No. FAA-2022-0812;
Project Identifier MCAI-2022-00445-T.
(a) Effective Date
This airworthiness directive (AD) is effective March 14, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus SAS airplanes identified in
paragraphs (c)(1) through (5) of this AD, certificated in any
category.
(1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes.
(2) Model A300 B4-605R and B4-622R airplanes.
(3) Model A300 C4-605R Variant F airplanes.
(4) Model A300 F4-605R and F4-622R airplanes.
(5) Model A310-203, -204, -221, -222, -304, -322, -324, and -325
airplanes.
[[Page 7864]]
(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 a new airworthiness
limitation is necessary. The FAA is issuing this AD to address
safety-significant latent failures that would, in combination with
one or more other specific failures or events, result in a hazardous
or catastrophic failure condition of hydraulic systems.
(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
2022-0060, dated April 1, 2022 (EASA AD 2022-0060).
(h) Exceptions to EASA AD 2022-0060
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2022-0060 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2022-0060 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 2022-0060 is at the applicable
``threshold'' as incorporated by the requirements of paragraph (3)
of EASA AD 2022-0060, or within 90 days after the effective date of
this AD, whichever occurs later.
(4) The provisions specified in paragraph (4) of EASA AD 2022-
0060 do not apply to this AD.
(5) The ``Remarks'' section of EASA AD 2022-0060 does not apply
to this AD.
(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 2022-0060.
(j) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, 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 Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (k) of this
AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#cef7e38f989de38f879ce3f9fdfee38f83818d8ea8afafe0a9a1b8"><span class="__cf_email__" data-cfemail="ac9581edfaff81ede5fe819b9f9c81ede1e3efeccacdcd82cbc3da">[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, Large Aircraft
Section, 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.
(k) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th Street, Des Moines, WA 98198;
telephone and fax 206-231-3225; email <a href="/cdn-cgi/l/email-protection#84e0e5eaaaf6ebe0edeae5c4e2e5e5aae3ebf2"><span class="__cf_email__" data-cfemail="86e2e7e8a8f4e9e2efe8e7c6e0e7e7a8e1e9f0">[email protected]</span></a>.
(l) 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 2022-0060,
dated April 1, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0060, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#36777245765357455718534344594657185343"><span class="__cf_email__" data-cfemail="6425201724010517054a0111160b14054a0111">[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#93f5e1bdfafde0e3f6f0e7fafcfdd3fdf2e1f2bdf4fce5"><span class="__cf_email__" data-cfemail="5f392d7136312c2f3a3c2b3630311f313e2d3e71383029">[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 October 3, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
Editorial Note: This document was received for publication by
the Office of the Federal Register on February 2, 2023.
[FR Doc. 2023-02530 Filed 2-6-23; 8:45 am]
BILLING CODE 4910-13-P
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