Proposed Rule2024-25615
Airworthiness Directives; Airbus Helicopters
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
November 5, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Helicopters (Airbus) Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. This proposed AD was prompted by a manufacturer assessment that determined additional actions are necessary to improve particle detection for main gearboxes (MGBs) with certain planet gear bearings installed. This proposed AD would require repetitively inspecting the MGB bevel wheel for the presence of particles, repetitively inspecting the MGB magnetic plug for particles, and prohibit installing an affected MGB unless certain requirements are met. These actions are specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 214 (Tuesday, November 5, 2024)</title>
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[Federal Register Volume 89, Number 214 (Tuesday, November 5, 2024)]
[Proposed Rules]
[Pages 87821-87825]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-25615]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2419; Project Identifier MCAI-2023-00366-R]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
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 Helicopters (Airbus) Model AS350B, AS350B1, AS350B2,
AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N,
AS355NP, EC130B4, and EC130T2 helicopters. This proposed AD was
prompted by a manufacturer assessment that determined additional
actions are necessary to improve particle detection for main gearboxes
(MGBs) with certain planet gear bearings installed. This proposed AD
would require repetitively inspecting the MGB bevel wheel for the
presence of particles, repetitively inspecting the MGB magnetic plug
for particles, and prohibit installing an affected MGB unless certain
requirements are met. These actions are specified in a European Union
Aviation Safety Agency (EASA) AD, which is proposed for incorporation
by reference. The FAA is proposing this AD to address the unsafe
condition on these products.
DATES: The FAA must receive comments on this NPRM by December 20, 2024.
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.
[[Page 87822]]
<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-2024-2419; 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 EASA AD, any comments received, and
other information. The street address for Docket Operations is listed
above.
Material Incorporated by Reference:
<bullet> For EASA material identified in this proposed AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221
8999 000; email: <a href="/cdn-cgi/l/email-protection#acede8dfecc9cddfcd82c9d9dec3dccd82c9d9"><span class="__cf_email__" data-cfemail="2d6c695e6d484c5e4c0348585f425d4c034858">[email protected]</span></a>; website: easa.europa.eu. You may
find the EASA material on the EASA website at ad.easa.europa.eu.
<bullet> You may view this material at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. For information on the availability of this
material at the FAA, call (817) 222-5110. The EASA material is also
available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2024-2419.
Other Related Material: For Airbus material identified in this
proposed AD, contact Airbus Helicopters, 2701 North Forum Drive, Grand
Prairie, TX 75052; phone: (972) 641-0000 or (800) 232-0323; fax: (972)
641-3775; or at <a href="http://airbus.com/en/products-services/helicopters/hcare-services/airbusworld">airbus.com/en/products-services/helicopters/hcare-services/airbusworld</a>.
FOR FURTHER INFORMATION CONTACT: Dan McCully, Aviation Safety Engineer,
FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; phone: (404)
474-5548; email: <a href="/cdn-cgi/l/email-protection#ed9a848181848c80c3808e8e98818194ad8b8c8cc38a829b"><span class="__cf_email__" data-cfemail="bccbd5d0d0d5ddd192d1dfdfc9d0d0c5fcdadddd92dbd3ca">[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-2024-2419; Project Identifier
MCAI-2023-00366-R'' 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 Dan
McCully, Aviation Safety Engineer, FAA, 1600 Stewart Ave., Suite 410,
Westbury, NY 11590; phone: (404) 474-5548; email:
<a href="/cdn-cgi/l/email-protection#5b2c323737323a36753638382e3737221b3d3a3a753c342d"><span class="__cf_email__" data-cfemail="83f4eaefefeae2eeadeee0e0f6efeffac3e5e2e2ade4ecf5">[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 2023-0044, dated February 28, 2023,
(EASA AD 2023-0044) to correct an unsafe condition on Airbus Model AS
350 B, AS 350 D, AS 350 B1, AS 350 B2, AS 350 BA, AS 350 BB, AS 350 B3,
EC 130 B4, EC 130 T2, AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS355
N, and AS355 NP helicopters. EASA advises that after a fleet design
review for detection of particles in the MGB, it was determined that
additional maintenance actions are necessary to improve detection of
particles in the MGB. The FAA is proposing this AD to detect and
correct the presence of particles in the MGB, which if not addressed,
could result in reduced or loss of control of the helicopter.
You may examine EASA AD 2023-0044 in the AD docket at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2024-2419.
Material Incorporated by Reference Under 1 CFR Part 51
EASA AD 2023-0044 requires repetitive borescope visual inspections
of the bevel wheel of the affected MGB for particles, collecting and
analyzing any found particles, and depending on the results, further
actions, accomplishing corrective action in accordance with the ASB
defined within, or contacting AH [Airbus Helicopters] for further
corrective action. EASA AD 2023-0044 also requires accomplishing a
borescope visual inspection of the bevel wheel of the affected MGB for
particles following the detection of any particles at the MGB magnetic
plug during accomplishment of certain maintenance tasks and depending
on the results, taking corrective action. Lastly, EASA AD 2023-0044
prohibits installing an affected MGB on any helicopter unless it is a
serviceable part as defined within and certain requirements are met.
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.
Other Related Material
The FAA reviewed Airbus Alert Service Bulletin No. AS350-05.01.04,
No. AS355-05.00.87, and No. EC130-05A040, each Revision 0, and each
dated January 25, 2023. This material specifies procedures for
borescope inspecting the MGB bevel wheel for particles and, depending
on the results, replacing a damaged epicyclic module or bevel reduction
module with an airworthy part, and collecting the particles using a
vacuum pump and analyzing the particles.
FAA's Determination
These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA is proposing this AD
after evaluating all known relevant information and determining that
the unsafe condition described previously is likely to exist or develop
on other helicopters of these same type designs.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in EASA AD 2023-0044, described previously, as incorporated by
reference, except for any differences identified as exceptions in the
[[Page 87823]]
regulatory text of this proposed AD and except as discussed under
``Differences Between this Proposed AD and EASA AD 2023-0044.''
This proposed AD would require certain actions within compliance
times specified in certain material referenced for compliance in EASA
AD 2023-0044, particularly for corrective actions for scales, flakes,
or splinters. Depending on the measurements of the scales, flakes, or
splinters, corrective actions include close monitoring, metallurgical
analysis within 50 hours time-in-serivce, or removing each affected
module and additional actions when certain criteria are exceeded.
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 2023-0044 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2023-0044 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 2023-0044 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-
0044. Material referenced in EASA AD 2023-0044 for compliance will be
available at <a href="http://www.regulations.gov">www.regulations.gov</a> by searching for and locating Docket
No. FAA-2024-2419 after the FAA final rule is published.
Differences Between This Proposed AD and EASA AD 2023-0044
EASA AD 2023-0044 applies to Model AS350BB helicopters, whereas
this proposed AD would not because that model is not FAA-type
certificated.
Where Note 1 in the material referenced in EASA AD 2023-0044
specifies the option of 1 mechanical technician and 1 crew member, for
this proposed AD, the pilot is only permitted to turn the tail rotor
(b) because the other actions specified in the note must be
accomplished by persons authorized under 14 CFR 43.3. Therefore, for
the purposes of this proposed AD, the owner/operator (pilot) may turn
the tail rotor (b) and must enter compliance with the applicable
paragraph of this proposed AD in the helicopter maintenance records in
accordance with 14 CFR 43.9(a) and 91.417(a)(2)(v). The pilot may
perform this action because it only involves turning the tail rotor
(b). This action can be performed equally well by a pilot or a
mechanic. This action is an exception to the FAA's standard maintenance
regulations.
This proposed AD would not require complying with paragraph (2) of
EASA AD 2023-0044. Instead, this proposed AD would require repetitively
inspecting the MGB magnetic plug for particles and, if there is any
particle, accomplishing a borescope visual inspection, as specified in
paragraphs (h)(6)(i) and (ii) of this proposed AD.
Where the material referenced in EASA AD 2023-0044 specifies
contacting Airbus Helicopters for a certain action, this proposed AD
would require accomplishing action in accordance with a method approved
the FAA, EASA, or Airbus Helicopters' EASA Design Organization
Approval.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 522 helicopters of U.S. Registry. Labor rates are estimated at
$85 per work-hour. Based on these numbers, the FAA estimates the
following costs to comply with this proposed AD.
A repetitive visual borescope inspection of the MGB bevel wheel
would take 1 work-hour for an estimated cost of $85 per helicopter and
$44,370 for the U.S. fleet, per inspection cycle.
If necessary, collecting and performing a metallurgical analysis of
the detected particles would take 6 work-hours for an estimated cost of
$510 per helicopter, per analysis.
Repetitively inspecting the magnetic plugs of the MGB would take 1
work-hour for an estimated cost of $85 per helicopter and $44,370 for
the U.S. fleet, per inspection cycle.
If required, close monitoring would take 2 work-hours for an
estimated cost of $170 per helicopter, per close monitoring cycle.
Accomplishing a visual borescope inspection of the MGB bevel wheel
as a result of an MGB magnetic plug inspection would take 1 work-hour
for an estimated cost of $85 per helicopter.
If necessary, replacing an epicyclic module would take 56 work-
hours and parts would cost $50,524 (overhauled) for an estimated cost
of $55,284 per module.
If necessary, replacing a bevel reduction module would take 56
work-hours and parts would cost $18,500 (overhaled) for an estimated
cost of $23,260 per module.
Certain corrective action could vary significantly from helicopter
to helicopter. The FAA has no data to determine the costs to accomplish
the corrective action.
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,
[[Page 87824]]
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 Helicopters: Docket No. FAA-2024-2419; Project Identifier
MCAI-2023-00366-R.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by December 20, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus Helicopters Model AS350B, AS350B1,
AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2,
AS355N, AS355NP, EC130B4, and EC130T2 helicopters, certificated in
any category.
(d) Subject
Joint Aircraft System Component (JASC) Code: 6320, Main Rotor
Gearbox.
(e) Unsafe Condition
This AD was prompted by an assessment performed by the
manufacturer which determined that additional actions are necessary
to improve particle detection for main gearboxes (MGBs) with certain
part-numbered planet gear bearings installed. The FAA is issuing
this AD to detect and correct particles in the MGB. The unsafe
condition, if not addressed, could result in reduced or loss of
control of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraphs (h) and (i) of this AD: Comply
with all required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency AD 2023-0044,
dated February 28, 2023 (EASA AD 2023-0044).
(h) Exceptions to EASA AD 2023-0044
(1) Where EASA AD 2023-0044 defines ``serviceable MGB'' as ``An
affected MGB which has accumulated less than 330 flight hours (FH)
since new (first installation on a helicopter), or since an
overhaul, or since an inspection in accordance with the instructions
of the ASB;'' for this AD, replace that text with ``An affected MGB
which has accumulated less than 330 total hours time-in-service
since new (zero total hours time-in-service), since last overhaul if
an overhaul has been accomplished, or since last inspection and any
specified corrective action in accordance with the instructions of
the ASB if an inspection and any specified corrective action by
following the instructions of the ASB have been accomplished.''
(2) Where EASA AD 2023-0044 requires compliance in terms of
flight hours, this AD requires using hours time-in-service (TIS).
(3) Where EASA AD 2023-0044 refers to its effective date, this
AD requires using the effective date of this AD.
(4) Where Note 1 in the material referenced in paragraph (1) of
EASA AD 2023-0044 specifies the option of 1 mechanical technician
and 1 crew member, for this AD, the pilot is only permitted to turn
the tail rotor (b). The owner/operator (pilot) holding at least a
private pilot certificate may turn the tail rotor (b) and must enter
compliance with paragraph (g) of this AD in the helicopter
maintenance records in accordance with 14 CFR 43.9(a) and
91.417(a)(2)(v). The record must be maintained as required by 14 CFR
91.417, 121.380, or 135.43. All other actions specified in Note 1 in
the material referenced in paragraph (1) of EASA AD 2023-0044 must
be accomplished by persons authorized under 14 CFR 43.3.
(5) Where Note 2 in the material referenced in paragraph (1) of
EASA AD 2023-0044 specifies contacting Airbus Helicopters for
further instructions if the bottom of the radius (a6) of the bevel
wheel (a3) or head screws (a4) (see Figure 2) are not clearly
visible, this AD requires, before further flight, accomplishing
action in accordance with a method approved by the FAA, EASA, or
Airbus Helicopters' EASA Design Organization Approval (DOA). If
approved by the DOA, the approval must include the DOA-authorized
signature.
(6) Instead of complying with paragraph (2) of EASA AD 2023-
0044, comply with the actions required by paragraphs (h)(6)(i) and
(ii) of this AD.
(i) After the effective date of this AD, and within the
compliance time intervals specified table 1 to paragraph (h)(6)(i)
of this AD, visually inspect the MGB magnetic plug for particles.
Note 1 to paragraph (h)(6)(i): Aircraft Maintenance Manual (AMM)
task 60-00-00, 6-2A, or AMM task 60-00-00, 6-2, or work card 60-00-
00-602, as applicable, provides information regarding inspecting the
MGB magnetic plug.
Table 1 to Paragraph (h)(6)(i)--MGB Magnetic Plug Inspections
----------------------------------------------------------------------------------------------------------------
Initial compliance
times (after the Interval compliance times
Helicopter model(s) effective date of this (thereafter) (hours TIS)
AD) (hours TIS)
----------------------------------------------------------------------------------------------------------------
AS350B, AS350B1, AS350BA, and AS350D........................ 5 30
AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP....... 5 30
AS350B2 and AS350B3......................................... 10 100
EC130B4..................................................... 5 150
EC130T2..................................................... 5 150
----------------------------------------------------------------------------------------------------------------
(ii) If there is any particle as a result of any MGB magnetic
plug inspection required by paragraph (h)(6)(i) of this AD, before
further flight, borescope inspect the bevel wheel of the affected
MGB for particles as required by paragraph (1) of EASA AD 2023-0044.
If there is any particle as a result of the borescope inspection of
the bevel wheel, before further flight, collect and analyze the
particles as required by paragraph (3) of EASA AD 2023-0044.
(7) Where paragraph (3) of EASA AD 2023-0044 specifies ``If,
during any inspection as required by paragraph (1) or (2) of this
AD;'' for this AD, replace that text with ``If, during any
inspection as required by paragraph (1) of this AD.''
(8) Where the material referenced in paragraph (3) of EASA AD
2023-0044 specifies performing a metallurgical analysis and
contacting Airbus Helicopters if collected particles cannot be
characterized with Work Card 20-08-01-601, this AD does not require
contacting Airbus Helicopter but does require performing the
metallurgical analysis.
(9) This AD does not allow the ferry flight provision specified
in the material referenced in paragraph (3) of EASA AD 2023-0044;
for this AD, refer to paragraph (j) of this AD.
(10) Where the material referenced in paragraph (3) of EASA AD
2023-0044 specifies contacting Airbus Helicopters if the damaged
module cannot be identified, this AD requires, before further
flight, accomplishing action in accordance with a method approved by
the FAA, EASA, or Airbus Helicopters' EASA DOA. If approved by the
DOA, the approval must include the DOA-authorized signature.
(11) Where paragraph (5) of EASA AD 2023-0044 states ``to
contact AH for corrective action(s) instructions, and within the
compliance time specified therein, to accomplish those instructions
accordingly'' for this AD, replace that text with
[[Page 87825]]
``accomplishing corrective actions in accordance with a method
approved by the FAA, EASA, or Airbus Helicopters' EASA DOA. If
approved by the DOA, the approval must include the DOA-authorized
signature.''
(12) Where paragraph (7) of EASA AD 2023-0044 states ``since new
(first installation a helicopter), or since an overhaul, or since an
inspection in accordance with the instructions of the ASB, as
applicable, and, thereafter, as required by this AD;'' for this AD,
replace that text with ``since new (zero total hours time-in-
service), or since last overhaul if an overhaul has been
accomplished, or since last inspection and any specified corrective
action in accordance with the instructions of the ASB if an
inspection and any specified corrective action by following the
instructions of the ASB have been accomplished, and thereafter as
required by this AD.''.''
(13) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0044.
(i) No Reporting Requirement
Although the material referenced in EASA AD 2023-0044 specifies
to submit certain information to the manufacturer, this AD does not
require that action.
(j) Special Flight Permit
A special flight permit may be issued in accordance with 14 CFR
21.197 and 21.199 to permit a one-time, non-revenue flight to a
location where the actions required by this AD can be accomplished.
This flight must be performed with only essential flight crew.
(k) Alternative Methods of Compliance (AMOCs)
(1) 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 local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of 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#bf8692fee9ec92fef6ed92888c8f92fef2f0fcffd9dede91d8d0c9"><span class="__cf_email__" data-cfemail="e3dacea2b5b0cea2aab1ced4d0d3cea2aeaca0a3858282cd848c95">[email protected]</span></a>.
(2) 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.
(l) Related Information
For more information about this AD, contact Dan McCully,
Aviation Safety Engineer, FAA, 1600 Stewart Ave., Suite 410,
Westbury, NY 11590; phone: (404) 474-5548; email:
<a href="/cdn-cgi/l/email-protection#37405e5b5b5e565a195a5454425b5b4e7751565619505841"><span class="__cf_email__" data-cfemail="89fee0e5e5e0e8e4a7e4eaeafce5e5f0c9efe8e8a7eee6ff">[email protected]</span></a>.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the material listed in this paragraph
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2023-0044,
dated February 28, 2023.
(ii) [Reserved]
(3) For EASA material identified in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999
000; email: <a href="/cdn-cgi/l/email-protection#3c7d784f7c595d4f5d1259494e534c5d125949"><span class="__cf_email__" data-cfemail="ffbebb8cbf9a9e8c9ed19a8a8d908f9ed19a8a">[email protected]</span></a>; website: easa.europa.eu. You may
find the EASA material on the EASA website at ad.easa.europa.eu.
(4) You may view this material at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call (817) 222-5110.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#6c0a1e4205021f1c090f180503022c020d1e0d420b031a"><span class="__cf_email__" data-cfemail="deb8acf0b7b0adaebbbdaab7b1b09eb0bfacbff0b9b1a8">[email protected]</span></a>.
Issued on October 29, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-25615 Filed 11-4-24; 8:45 am]
BILLING CODE 4910-13-P
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</html>Indexed from Federal Register on November 5, 2024.
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