Rule2024-11587
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
May 29, 2024
Effective
July 3, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2021-21- 02, which applied to certain Airbus SAS Model A318, A319, A320, A321, A330-200, A330-200 Freighter, A330-300, A330-800, A330-900, A340-200, A340-300, A340-500, A340-600, and A380-800 series airplanes. AD 2021- 21-02 required replacing certain parts manufacturer approval (PMA) Ni- Cd batteries with serviceable Ni-Cd batteries or maintaining the electrical storage capacity of those PMA Ni-Cd batteries during airplane storage or parking. This AD was prompted by a determination that the on-wing preservation procedures originally provided in that AD did not ensure the expected preservation of the battery capacity. This AD adds airplanes to the applicability and requires replacing each affected part with a serviceable part before release to service of an airplane after a storage or parking period, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 104 (Wednesday, May 29, 2024)</title>
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[Federal Register Volume 89, Number 104 (Wednesday, May 29, 2024)]
[Rules and Regulations]
[Pages 46319-46322]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-11587]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-0221; Project Identifier AD-2023-01233-T;
Amendment 39-22762; AD 2024-11-01]
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 superseding Airworthiness Directive (AD) 2021-21-
02, which applied to certain Airbus SAS Model A318, A319, A320, A321,
A330-200, A330-200 Freighter, A330-300, A330-800, A330-900, A340-200,
A340-300, A340-500, A340-600, and A380-800 series airplanes. AD 2021-
21-02 required replacing certain parts manufacturer approval (PMA) Ni-
Cd batteries with serviceable Ni-Cd batteries or maintaining the
electrical storage capacity of those PMA Ni-Cd batteries during
airplane storage or parking. This AD was prompted by a determination
that the on-wing preservation procedures originally provided in that AD
did not ensure the expected preservation of the battery capacity. This
AD adds airplanes to the applicability and requires replacing each
affected part with a serviceable part before release to service of an
airplane after a storage or parking period, as applicable. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective July 3, 2024.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-0221; 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, 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: Dan Rodina, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206-
231-3225; email <a href="/cdn-cgi/l/email-protection#d9bdb8b7f7abb6bdb0b7b899bfb8b8f7beb6af"><span class="__cf_email__" data-cfemail="197d7877376b767d707778597f7878377e766f">[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 2021-21-02, Amendment 39-21762 (86 FR
62898, November 15, 2021) (AD 2021-21-02). AD 2021-21-02 applied to
certain Airbus SAS Model A318, A319, A320, A321, A330-200, A330-200
Freighter, A330-300, A330-800, A330-900, A340-200, A340-300, A340-500,
A340-600, and A380-800 series airplanes. The NPRM published in the
Federal Register on February 9, 2024 (89 FR 9074). The NPRM was
prompted by a determination that the on-wing preservation procedures
originally provided in that AD did not ensure the expected preservation
of the battery capacity. In the NPRM, the FAA proposed to add Model
A300 series airplanes; 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); Model A310 series airplanes;
and Model A350-941 and -1041 airplanes to the applicability. The FAA
proposed that the superseding AD would retain none of the requirements
of AD 2021-21-02. The FAA proposed to require replacing each affected
part with a serviceable part before release to service of an airplane
after a storage or parking period, as applicable. The FAA is issuing
this AD to address reduced battery endurance performance, which could
possibly result in failure to supply the minimum essential electrical
power during abnormal or emergency conditions.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from Air Line Pilots Association,
International (ALPA), who supported the SNPRM/NPRM without change.
The FAA received additional comments from American Airlines (AA)
and United Airlines (UAL). The following presents the comments received
on the NPRM and the FAA's response to each comment.
Request for Clarification of Terms
AAL requested clarification of ``parking and storage'' as intended
by
[[Page 46320]]
the proposed AD. The commenter asked whether ``parking and storage''
included extended heavy maintenance checks, such as an S-check that is
abnormally extended beyond the 6-month time-limit due to inspection
findings or material sourcing issues, or extended downtime for aircraft
repair or modification such as a large repair for aircraft tug
collision damage or a large-scale interior modification.
The FAA agrees to clarify. It is the responsibility of the operator
to apply the relevant instructions provided in the aircraft maintenance
manual (AMM) related to extended heavy maintenance checks or downtime
for aircraft repair or modification. A dedicated preservation regime
shall be defined in line with the maintenance activity requirements
(for example, the need to keep batteries connected), based upon the
applicable AMM parking and storage procedures. If a battery meets the
definition of a ``serviceable part'' as specified in paragraphs (g)(2)
and (3) of this AD, then the requirement to replace after ``parking and
storage'' does not apply because it is not an affected part. However,
if the battery meets the definition of an ``affected part'' as
specified in paragraph (g)(1) of this AD, the requirement to replace
after ``parking and storage'' does apply.
Request for One AD in the Future
UAL requested that in the future an attempt is made to include PMA
parts during ``initial release'' as opposed to having two ADs (UAL
stated ``no change to this AD'').
The FAA recognizes the efficiency of a single AD, but in the
future, may or may not issue separate ADs when PMA parts and non-PMA
parts (i.e., original equipment manufacturer (OEM) parts) are involved,
depending on potential implementation issues and what is in the best
interest of safety.
Comment on Duplicative Applicability
UAL stated that Docket FAA-2024-0029 indicated it applied to the
PMA batteries, as does the NPRM.
The FAA acknowledges that the NPRM that published in the Federal
Register on January 22, 2024 (89 FR 3897), for Docket FAA-2024-0029,
inadvertently referred to PMA batteries. However, in the final rule, AD
2024-08-08, Amendment 39-22741 (89 FR 35695, May 2, 2024) (AD 2024-08-
08), the FAA removed references to PMA batteries. Only this AD is
applicable to PMA batteries.
Updated Reference to Related AD
Note 1 to paragraph (h) of the proposed AD specifies that airplanes
on which a battery is replaced with a serviceable non-PMA Ni-Cd battery
are affected by AD 2021-20-08, Amendment 39-21746 (86 FR 57025, October
14, 2021), which provides requirements for non-PMA Ni-Cd batteries.
However, the FAA has superseded AD 2021-20-08 with AD 2024-08-08. AD
2024-08-08 adds airplanes to the applicability and requires replacement
of certain affected parts (i.e., certain non-PMA Ni-Cd batteries) with
serviceable parts as a precondition for return to service of airplanes
from storage or parking, as specified in European Union Aviation Safety
Agency (EASA) AD 2023-0196, dated November 10, 2023. You may examine
the AD docket for AD 2024-08-08 at <a href="http://regulations.gov">regulations.gov</a> under Docket No.
FAA-2024-0029. The FAA has added a reference to AD 2024-08-08 to Note 1
to paragraph (h) of this AD.
Conclusion
The FAA reviewed the relevant data, considered any comments
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 these products. Except for minor editorial changes, and
any other changes described previously, this AD is adopted as proposed
in the NPRM. None of the changes will increase the economic burden on
any operator.
Costs of Compliance
The FAA estimates that this AD affects 1,814 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.
Action Labor cost Parts cost product operators
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Replacements.............................. 5 work-hours x $85 per hour $0 $425 $770,950
= $425.
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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:
[[Page 46321]]
0
a. Removing Airworthiness Directive (AD) 2021-21-02, Amendment 39-21762
(86 FR 62898, November 15, 2021); and
0
b. Adding the following new AD:
2024-11-01 Airbus SAS: Amendment 39-22762; Docket No. FAA-2024-0221;
Project Identifier AD-2023-01233-T.
(a) Effective Date
This airworthiness directive (AD) is effective July 3, 2024.
(b) Affected ADs
This AD replaces AD 2021-21-02, Amendment 39-21762 (86 FR 62898,
November 15, 2021) (AD 2021-21-02).
(c) Applicability
This AD applies to Airbus SAS airplanes identified in paragraphs
(c)(1) through (14) of this AD, certificated in any category,
equipped with any parts manufacturer approval (PMA) part approved
for the type design nickel cadmium (Ni-Cd) batteries having a part
number identified in Figure 1 to the introductory text of paragraph
(c) of this AD.
[GRAPHIC] [TIFF OMITTED] TR29MY24.015
(1) Model A300 B4-2C, B4-102, B4-103, B4-120, B4-203, and B4-220
airplanes.
(2) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes.
(3) Model A300 B4-605R and B4-622R airplanes.
(4) Model A300 C4-203, C4-605R variant F, and C4-620 airplanes.
(5) Model A300 F4-203, F4-605R, F4-608ST, and F4-622R airplanes.
(6) Model A310-203, -203C, -204, -221, -222, -304, -308, -322, -
324, and -325 airplanes.
(7) Model A318-111, -112, -121, and -122 airplanes.
(8) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -
151N, -153N, and -171N airplanes.
(9) Model A320-211, -212, -214, -215, -216, -231, -232, -233, -
251N, -252N, -253N, -271N, -272N, and -273N airplanes.
(10) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -
251N, -251NX, -252N, -252NX, -253N, -253NX, -271N, -271NX, -272N,
and -272NX airplanes.
(11) Model A330-201, -202, -203, -223, -223F, -243, -243F, -301,
-302, -303, -321, -322, -323, -341, -342, -343, -743L, -841, and -
941 airplanes.
(12) Model A340-211, -212, -213, -311, -312, -313, -541, -542, -
642, and -643 airplanes.
(13) Model A350-941 and A350-1041 airplanes.
(14) Model A380-841, -842, and -861 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 24, Electrical
Power.
(e) Unsafe Condition
This AD was prompted by a report that repetitive disconnection
and reconnection of certain Ni-Cd batteries during airplane parking
or storage could lead to a reduction in capacity of those batteries.
The unsafe condition, if not addressed, could lead to reduced
battery endurance performance and possibly result in failure to
supply the minimum essential electrical power during abnormal or
emergency conditions.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definitions
(1) For the purposes of this AD, an ``affected PMA Ni-Cd
battery'' is defined as any PMA Ni-Cd battery approved for a Ni-Cd
battery identified in Figure 1 to the introductory text of paragraph
(c) of this AD, all serial numbers, except those which are a
serviceable PMA Ni-Cd battery as defined in paragraph (g)(2) of this
AD.
(2) For the purposes of this AD, a ``serviceable PMA Ni-Cd
battery'' is defined as a PMA Ni-Cd battery approved for a Ni-Cd
battery identified in Figure 1 to the introductory text of paragraph
(c) of this AD, all serial numbers, which was fully (re)charged at
constant current and, after (re)charging, was not stored on wing
during a period exceeding the applicable ``Time Limit'' specified in
Figure 1 to the introductory text of paragraph (c) of this AD.
Periodical, regular, and overhaul checks of a PMA Ni-Cd battery that
include the battery (re)charge at constant current are acceptable
methods to demonstrate that the battery was (re)charged.
(3) For the purposes of this AD, a ``serviceable non-PMA Ni-Cd
battery'' is defined as a type design Ni-Cd battery having a part
number identified in Figure 1 to the introductory text of paragraph
(c) of this AD, all serial numbers, which was fully (re)charged at
constant current and, after (re)charging, was not stored on wing
during a period exceeding the applicable ``Time Limit'' specified in
Figure 1 to the introductory text of paragraph (c) of this AD.
Periodical, regular, and overhaul checks of a non-PMA Ni-Cd battery
that include the battery (re)charge at constant current are
acceptable methods to demonstrate that the battery was (re)charged.
(h) Replacement
Before release to service of an airplane after a storage or
parking period, as applicable, replace each affected PMA Ni-Cd
battery with a serviceable PMA Ni-Cd battery or a serviceable non-
PMA Ni-Cd battery.
Note 1 to paragraph (h): Airplanes on which a battery is
replaced with a serviceable non-PMA Ni-Cd battery are affected by AD
2024-08-08, Amendment 39-22741 (89 FR 35695, May 2, 2024), which
provides requirements for non-PMA Ni-Cd batteries.
(i) Parts Installation Limitation
As of the effective date of this AD, release to service of an
airplane is allowed, provided all PMA Ni-Cd batteries approved for a
Ni-Cd battery identified in Figure 1 to the introductory text of
paragraph (c) of this AD that are installed on that airplane are
fully (re)charged at constant current and, after (re)charging, were
not stored on wing during a period exceeding the applicable ``Time
Limit'' specified in Figure 1 to the introductory text of paragraph
(c) of this AD.
(j) 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
[[Page 46322]]
appropriate. If sending information directly to the manager of the
certification office, 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#d8e1f5998e8bf599918af5efebe8f59995979b98beb9b9f6bfb7ae"><span class="__cf_email__" data-cfemail="fec7d3bfa8add3bfb7acd3c9cdced3bfb3b1bdbe989f9fd0999188">[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.
(k) Related Information
For more information about this AD, contact Dan Rodina, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 206-231-3225; email <a href="/cdn-cgi/l/email-protection#dabebbb4f4a8b5beb3b4bb9abcbbbbf4bdb5ac"><span class="__cf_email__" data-cfemail="f397929ddd819c979a9d92b3959292dd949c85">[email protected]</span></a>.
(l) Material Incorporated by Reference
None.
Issued on May 21, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-11587 Filed 5-28-24; 8:45 am]
BILLING CODE 4910-13-P
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