Rule2022-27398
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
December 19, 2022
Effective
January 23, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2016-16- 06, which applied to certain Airbus SAS Model A300 B4-603, B4-605R, and B4-622R airplanes; and Model A310-304, -324, and -325 airplanes. AD 2016-16-06 required inspections around the rivet heads of the seal retainer run-out holes at certain frames and corrective actions if necessary. This AD was prompted by a report of a crack found on a certain door frame, and a determination that other frames may also be susceptible to cracking, and that additional airplanes may be affected by the unsafe condition. This AD continues to require the actions in AD 2016-16-06 and adds airplanes, 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 87 Issue 242 (Monday, December 19, 2022)</title>
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[Federal Register Volume 87, Number 242 (Monday, December 19, 2022)]
[Rules and Regulations]
[Pages 77480-77482]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-27398]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1168; Project Identifier MCAI-2022-00600-T;
Amendment 39-22259; AD 2022-25-03]
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: The FAA is superseding Airworthiness Directive (AD) 2016-16-
06, which applied to certain Airbus SAS Model A300 B4-603, B4-605R, and
B4-622R airplanes; and Model A310-304, -324, and -325 airplanes. AD
2016-16-06 required inspections around the rivet heads of the seal
retainer run-out holes at certain frames and corrective actions if
necessary. This AD was prompted by a report of a crack found on a
certain door frame, and a determination that other frames may also be
susceptible to cracking, and that additional airplanes may be affected
by the unsafe condition. This AD continues to require the actions in AD
2016-16-06 and adds airplanes, 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 January 23, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 23,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-1168; 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#81c0c5f2c1e4e0f2e0afe4f4f3eef1e0afe4f4"><span class="__cf_email__" data-cfemail="de9f9aad9ebbbfadbff0bbabacb1aebff0bbab">[email protected]</span></a>; website easa.europa.eu. You may
find this material on the EASA website at ad.easa.europa.eu.
<bullet> 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> under Docket No. FAA-2022-1168.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, FAA, International Validation Branch, 2200 South
216th St., Des Moines, WA 98198; telephone 206-231-3225; email
<a href="/cdn-cgi/l/email-protection#76121718580419121f18173610171758111900"><span class="__cf_email__" data-cfemail="7317121d5d011c171a1d12331512125d141c05">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2016-16-06, Amendment 39-18604 (81 FR
51320, August 4, 2016) (AD 2016-16-06). AD 2016-16-06 applied to
certain Airbus SAS Model A300 B4-603, B4-605R, and B4-622R airplanes;
and Model A310-304, -324, and -325 airplanes. AD 2016-16-06 required
inspections around the rivet heads of the seal retainer run-out holes
at certain frames and corrective actions if necessary. The FAA issued
AD 2016-16-06 to address cracking of the door frame, which could result
in reduced structural integrity of the airplane.
The NPRM published in the Federal Register on September 20, 2022
(87 FR 57424). The NPRM was prompted by AD 2022-0078, dated May 4,
2022, issued by EASA (EASA AD 2022-0078) (referred to after this as the
MCAI). The MCAI states that cracking on door frames could result in
reduced structural integrity 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-2022-1168.
In the NPRM, the FAA proposed to continue to require the actions in
AD 2016-16-06 and add airplanes, as specified in EASA AD 2022-0078. The
FAA is issuing this AD to address cracking on door frames, which could
result in reduced structural integrity of the airplane.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from FedEx Express, who 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.
[[Page 77481]]
None of the changes will increase the economic burden on any operator.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0078 specifies procedures for repetitive high
frequency eddy current (HFEC) inspections of rivet heads of the seal
retainer run-out holes at door frames (FR) 56A, FR 57A, and FR 73A for
any cracking, and repair.
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 affects 128 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Retained actions from AD 2016-16-06. 11 work-hours x $85 per $0 $935 $119,680
hour = $935.
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The FAA has received no definitive data on which to base the cost
estimate for the on-condition repair specified in this 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
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:
0
a. Removing Airworthiness Directive 2016-16-06, Amendment 39-18604 (81
FR 51320, August 4, 2016); and
0
b. Adding the following new airworthiness directive:
2022-25-03 Airbus SAS: Amendment 39-22259; Docket No. FAA-2022-1168;
Project Identifier MCAI-2022-00600-T
(a) Effective Date
This airworthiness directive (AD) is effective January 23, 2023.
(b) Affected ADs
This AD replaces AD 2016-16-06, Amendment 39-18604 (81 FR 51320,
August 4, 2016) (AD 2016-16-06).
(c) Applicability
This AD applies to all the Airbus SAS airplanes specified in
paragraphs (c)(1) through (3) of this AD, certificated in any
category.
(1) Model A300 B4-603 and -622 airplanes.
(2) Model A300 B4-605R and -622R airplanes.
(3) Model A310-203, -222, -304, -322, -324, and -325 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by a report of a crack found on door frame
(FR) 73A between stringers 24 and 25, and a determination that FR
56A and FR 57A may also be susceptible to cracking, and that
additional airplanes may be affected by the unsafe condition. The
FAA is issuing this AD to address cracking on door frames, which
could result in reduced structural integrity 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
2022-0078, dated May 4, 2022 (EASA AD 2022-0078).
(h) Exceptions to EASA AD 2022-0078
(1) Where EASA AD 2022-0078 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where EASA AD 2022-0078 refers to September 25, 2014 (the
effective date of EASA AD 2014-0202), this AD requires using
September 8, 2016 (the effective date of AD 2016-16-06).
(3) The ``Remarks'' section of EASA AD 2022-0078 does not apply
to this AD.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2022-0078
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) 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 (k) of this AD. Information may be
[[Page 77482]]
emailed to: <a href="/cdn-cgi/l/email-protection#320b1f7364611f737b601f0501021f737f7d71725453531c555d44"><span class="__cf_email__" data-cfemail="320b1f7364611f737b601f0501021f737f7d71725453531c555d44">[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 (j)(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.
(k) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3225; email <a href="/cdn-cgi/l/email-protection#4226232c6c302d262b2c23022423236c252d34"><span class="__cf_email__" data-cfemail="89ede8e7a7fbe6ede0e7e8c9efe8e8a7eee6ff">[email protected]</span></a>.
(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) European Union Aviation Safety Agency (EASA) AD 2022-0078,
dated May 4, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0078, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#58191c2b183d392b39763d2d2a372839763d2d"><span class="__cf_email__" data-cfemail="a6e7e2d5e6c3c7d5c788c3d3d4c9d6c788c3d3">[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#6107134f080f1211040215080e0f210f0013004f060e17"><span class="__cf_email__" data-cfemail="2c4a5e0245425f5c494f584543426c424d5e4d024b435a">[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 November 28, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-27398 Filed 12-16-22; 8:45 am]
BILLING CODE 4910-13-P
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