Federal Register / Vol. 89, No. 250 / Tuesday, December 31, 2024 / Proposed Rules 107063 

(b) The committees must discuss 

related proposals with other 

committees. 

(c) The committees shall make 

recommendations to the House of 

Delegates as a whole concerning each 

proposal. The House of Delegates report 

shall show any proposed change in 

wording, record the votes on each 

proposal, and suggest an effective date 

for each proposal recommended for 

adoption. The individual committee 

reports shall be submitted to the 

chairperson of the House of Delegates, 

who will combine them into one report 

showing, in numerical sequence, the 

committee recommendations on each 

proposal. Once completed, the 

combined committee report will be 

distributed electronically to the Official 

State Agencies prior to the delegates 

voting on the final day of the House of 

Delegates conference. 

(d) The Technical Committee 

meetings shall be open to any interested 

person. Advocates for or against any 

proposal may appear before the 

appropriate committee and present their 

views. 

§ 149.7 House of Delegates consideration 

of proposed changes. 

(a) The chairperson of the House of 

Delegates shall be a representative of the 

Department. 

(b) At the time designated for voting 

on proposed changes by the official 

delegates, the chairman of the General 

Conference Committee and all 

committee chairpersons shall sit at the 

speaker’s table and assist the 

chairperson of the House of Delegates. 

(c) The chairperson shall set the rules 

of order for the General Conference 

Committee. 

(d) Proposals that have not been 

submitted in accordance with § 149.5 

will be considered by the House of 

Delegates only with the unanimous 

consent of the General Conference 

Committee. Any such proposals must be 

referred to the appropriate committee 

for consideration before being presented 

for action by the House of Delegates. 

(e) Voting will be by States, and each 

official delegate, as determined by 

§ 149.5, will be allowed one vote on 

each proposal pertaining to the program 

prescribed by the subpart which they 

represent. 

(f) A roll call of States for a recorded 

vote will be used when requested by a 

delegate or at the discretion of the 

chairman. 

(g) All motions on proposed changes 

shall be for adoption. 

(h) Proposed changes shall be adopted 

by a two-thirds majority vote of the 

official delegates present and voting. 

(i) The House of Delegates conference 

shall be open to any interested person. 

§ 149.8 Approval of House of Delegates 

recommendations by the Department. 

Proposals adopted by the official 

delegates will be recommended to the 

Department for incorporation into the 

provisions of the US SHIP in part 148 

of this subchapter and this part. The 

Department reserves the right to 

approve or disapprove the 

recommendations of the House of 

Delegates as an integral part of its 

sponsorship of the US SHIP. 

§ 149.9 Changes to the US SHIP Program 

Standards. 

The US SHIP Program Standards 

document contains content on the 

testing requirements for diseases 

covered by the regulations in part 148 

of this subchapter, approved procedures 

for maintaining biosecurity at 

participating swine operations, 

traceability requirements for 

participating swine operations, and 

calculations for official delegate 

allocations. Changes to the US SHIP 

Program Standards document for any of 

the foregoing will be made in the 

following manner: 

(a) Normal process for updating the 

US SHIP Program Standards document. 

(1) APHIS will publish a notice in the 

Federal Register providing the proposed 

changes to the US SHIP Program 

Standards document and the basis for 

the changes. The notice will request 

public comment. 

(2) If no comments are received on the 

notice, or if the comments received do 

not call into question the basis for the 

changes, APHIS will publish a 

subsequent notice in the Federal 

Register announcing that the changes 

have been made to the US SHIP Program 

Standards document and making 

available the revised US SHIP Program 

Standards document. If comments 

identify concerns with the proposed 

revisions, APHIS will consider and 

address those comments as appropriate 

prior to taking any action to revise the 

US SHIP Program Standards. 

(b) Process for making immediate 

changes to the US SHIP Program 

Standards document. (1) If the 

Administrator determines that 

procedures for maintaining biosecurity 

and animal traceability at participating 

swine operations that are described in 

the US SHIP Program Standards 

document are not adequate or that 

testing procedures must be revised in 

order to ensure that they provide 

reliable assurances regarding test 

results, APHIS will make the relevant 

change to the US SHIP Program 

Standards document. As soon as is 

feasible, APHIS will publish a notice in 

the Federal Register announcing the 

change, as well as the basis for the 

change. The notice will request public 

comment. 

(2) APHIS may make further revisions 

to the US SHIP Program Standards 

document based on the comments 

received. 

Done in Washington, DC, this 23rd day of 

December 2024. 

Donna Lalli, 

Acting Administrator, Animal and Plant 

Health Inspection Service. 

[FR Doc. 2024–31386 Filed 12–30–24; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2718; Project 

Identifier MCAI–2024–00319–T] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to adopt a 

new airworthiness directive (AD) for all 

Airbus SAS Model A319–111, –112, 

–113, –114, –115, –131, –132, and –133 

airplanes; Model A320–211, –212, –214, 

–216, –231, –232, –233, –251N, –252N, 

–253N, –271N, –272N, and –273N 

airplanes; Model A321–211, –212, –213, 

–231, –232, –251N, –251NX, –252N, 

–252NX, –253N, –253NX, –253NY, 

–271N, –271NX, –272N, and –272NX 

airplanes; Airbus SAS Model A330–200 

series airplanes; Model A330–300 series 

airplanes; Model A330–800 series 

airplanes; Model A330–900 series 

airplanes; Model A350–941 and –1041 

airplanes; and Model A380–800 series 

airplanes. This proposed AD was 

prompted by a report of corrosion and 

cracks on the broadband antenna 

adapter plate during an inspection. This 

proposed AD would require repetitive 

general visual inspections (GVI) of the 

broadband antenna adapter plate, skirt, 

vents, and attachment fittings and limit 

the installation of affected parts under 

certain conditions, 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. 


khammond on DSK9W7S144PROD with PROPOSALS
107064 Federal Register / Vol. 89, No. 250 / Tuesday, December 31, 2024 / Proposed Rules 

DATES: The FAA must receive comments 

on this proposed AD by February 14, 

2025. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

regulations.gov. Follow the instructions 

for submitting comments. 

• Fax: 202–493–2251. 

• 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. 

• 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 regulations.gov under Docket 

No. FAA–2024–2718; 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: 

• For EASA material identified in this 

proposed AD, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne, 

Germany; telephone +49 221 8999 000; 

email ADs@easa.europa.eu; website 

easa.europa.eu. You may find this 

material on the EASA website at 

ad.easa.europa.eu. It is also available at 

regulations.gov under Docket No. FAA– 

2024–2718. 

• 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. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aviation Safety Engineer, FAA, 

1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; telephone 206– 

231–3225; email Dan.Rodina@faa.gov. 

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 the ADDRESSES section. Include 

‘‘Docket No. FAA–2024–2718; Project 

Identifier MCAI–2024–00319–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 

regulations.gov, 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 Rodina, Aviation 

Safety Engineer, FAA, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 

11590; telephone 206–231–3225; email 

Dan.Rodina@faa.gov. 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 2024–0199, 

dated October 18, 2024 (EASA AD 

2024–0199) (also referred to as the 

MCAI), to correct an unsafe condition 

for Airbus SAS Model A319–111, –112, 

–113, –114, –115, –131, –132, and –133 

airplanes; Model A320–211, –212, –214, 

–215, –216, –231, –232, –233, –251N, 

–252N, –253N, –271N, –272N, and 

–273N airplanes; Model A321–211, 

–212, –213, –231, –232, –251N, –251NX, 

–252N, –252NX, –253N, –253NX, 

–253NY, –271N, –271NX, –272N, and 

–272NX airplanes; Airbus SAS Model 

A330–200 series airplanes; Model 

A330–300 series airplanes; Model 

A330–800 series airplanes; Model 

A330–900 series airplanes; Model 

A350–941 and –1041 airplanes; and 

Model A380–800 series airplanes. 

Model A320–215 airplanes are not 

certificated by the FAA and are not 

included on the U.S. type certificate 

data sheet; this AD therefore does not 

include those airplanes in the 

applicability. The MCAI states that 

corrosion and cracks were found on the 

broadband antenna adapter plate during 

an inspection. Further investigation 

determined that the broadband antenna 

adapter plate and skirt assembly-adapter 

are made of material susceptible to 

corrosion cracking, and that the 

recommended maintenance programs 

do not ensure timely detection of cracks 

and damage in this area. 

The FAA is proposing this AD to 

address the corrosion and cracks on the 

broadband antenna adapter plate and 

skirt assembly-adapter. The unsafe 

condition, if not addressed, could lead 

to in-flight detachment of the radome, 

antenna, and affected parts, which 

could impact the tail section of the 

airplane, possibly resulting in damage 

and reduced control of the airplane. 

You may examine the MCAI in the 

AD docket at regulations.gov under 

Docket No. FAA–2024–2718. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

EASA AD 2024–0199 specifies 

procedures for repetitive general visual 

inspections (GVI) for cracks and 

corrosion of the broadband antenna 

adapter plate, skirt, vents, and 

attachment fittings, and, depending on 

findings, corrective actions including 

repair or replacement of the affected 

parts. EASA AD 2024–0199 also limits 

the installation of affected parts under 

certain conditions and requires 

reporting of the inspection results after 

each inspection. 

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. 

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 this State of 

Design Authority, it has notified the 

FAA of the unsafe condition described 

in the MCAI referenced 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. 


khammond on DSK9W7S144PROD with PROPOSALS
Federal Register / Vol. 89, No. 250 / Tuesday, December 31, 2024 / Proposed Rules 107065 

Proposed AD Requirements in This 

NPRM 

This proposed AD would require 

accomplishing the actions specified in 

EASA AD 2024–0199 described 

previously, except for any differences 

identified as exceptions in the 

regulatory text 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 2024–0199 by 

reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2024–0199 

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 2024–0199 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 2024–0199. 

Material required by EASA AD 2024– 

0199 for compliance will be available at 

regulations.gov under Docket No. FAA– 

2024–2718 after the FAA final rule is 

published. 

Interim Action 

The FAA considers that this proposed 

AD would be an interim action. The 

FAA anticipates that further AD action 

will follow. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 4 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this proposed AD: 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per 

product 

Cost on 

U.S. 

operators 

Up to 61 work-hours × $85 per hour = $5,185 ....................................................................................... $0 Up to 

$5,185 

Up to 

$20,740 

The FAA estimates the following 

costs to do any on-condition action that 

would be required based on the results 

of any required actions. The FAA has no 

way of determining the number of 

aircraft that might need this oncondition action: 

ESTIMATED COSTS OF ON-CONDITION

ACTIONS

Labor cost Parts cost Cost per 

product 

50 work-hours × 

$85 per hour 

= $4,250 ........ $10,000 $14,250 

The FAA has received no definitive 

data on which to base the cost estimates 

for the repairs specified in this proposed 

AD. 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to a penalty for failure to comply with 

a collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a currently valid 

OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public 

reporting for this collection of 

information is estimated to take 

approximately 1 hour per response, 

including the time for reviewing 

instructions, searching existing data 

sources, gathering and maintaining the 

data needed, and completing and 

reviewing the collection of information. 

All responses to this collection of 

information are mandatory. Send 

comments regarding this burden 

estimate or any other aspect of this 

collection of information, including 

suggestions for reducing this burden, to: 

Information Collection Clearance 

Officer, Federal Aviation 

Administration, 10101 Hillwood 

Parkway, Fort Worth, TX 76177–1524. 

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, 

the FAA proposes to amend 14 CFR part 

39 as follows: 


khammond on DSK9W7S144PROD with PROPOSALS
107066 Federal Register / Vol. 89, No. 250 / Tuesday, December 31, 2024 / Proposed Rules 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive: 

Airbus SAS: Docket No. FAA–2024–2718; 

Project Identifier MCAI–2024–00319–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by February 14, 

2025. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Airbus SAS Model 

airplanes specified in paragraphs (c)(1) 

through (6) of this AD, certificated in any 

category. 

(1) Model A319–111, –112, –113, –114, 

–115, –131, –132, and –133 airplanes. 

(2) Model A320–211, –212, –214, –216, 

–231, –232, –233, –251N, –252N, –253N, 

–271N, –272N, and –273N airplanes. 

(3) Model A321–211, –212, –213, –231, 

–232, –251N, –251NX, –252N, –252NX, 

–253N, –253NX, –253NY, –271N, –271NX, 

–272N, and –272NX airplanes. 

(4) Model A330–201, –202, –203, –223, 

–243, –301, –302, –303, –321, –322, –323, 

–341, –342, –343, –841, and –941 airplanes. 

(5) Model A350–941 and –1041 airplanes. 

(6) Model A380–841, –842, and –861 

airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 53, Fuselage. 

(e) Unsafe Condition 

This AD was prompted by a report that 

found corrosion and cracks on the broadband 

antenna adapter plate during an inspection. 

The FAA is issuing this AD to address the 

corrosion and cracks on the broadband 

antenna adapter plate and skirt assemblyadapter. The unsafe condition, if not 

addressed, could lead to in-flight detachment 

of the radome, antenna, and affected parts, 

which could impact the tail section of the 

airplane, possibly resulting in damage and 

reduced control 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 2024–0199, dated 

October 18, 2024 (EASA AD 2024–0199). 

(h) Exceptions to EASA AD 2024–0199 

(1) Where Appendix A in ‘‘the applicable 

SB’’ identified in EASA AD 2024–0199 

specifies a compliance time ‘‘from SB 

publication date,’’ this AD requires using the 

effective date of this AD. 

(2) Where EASA AD 2024–0199 specifies 

‘‘14 June 2024 [the effective date of EASA AD 

2024–0106],’’ this AD requires using the 

effective date of this AD. 

(3) This AD does not adopt the ‘‘Remarks’’ 

section of EASA AD 2024–0199. 

(4) Where paragraph (2) of EASA AD 2024– 

0199 specifies ‘‘If, during any GVI as required 

by paragraph (1) of this AD, any crack and/ 

or corrosion are detected on an affected part, 

before next flight, accomplish the applicable 

corrective action(s) in accordance with the 

instructions of the applicable SB, or contact 

Airbus for approved repair instructions and 

accomplish those instructions accordingly,’’ 

this AD requires replacing that text with ‘‘If, 

during any GVI as required by paragraph (1) 

of this AD, any crack and/or corrosion are 

detected on an affected part, the crack and/ 

or corrosion must be repaired before further 

flight using a method approved by the 

Manager, AIR–520, Continued Operational 

Safety 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.’’ 

(5) Paragraph (4) of EASA AD 2024–0199 

specifies to report inspection results to 

Airbus within a certain compliance time. For 

this AD, report inspection results at the 

applicable time specified in paragraph 

(h)(5)(i) or (ii) of this AD. 

(i) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 30 days after the inspection. 

(ii) If the inspection was done before the 

effective date of this AD: Submit the report 

within 30 days after the effective date of this 

AD. 

(i) Additional AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, AIR–520, Continued 

Operational Safety 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 Manager, AIR–520, Continued 

Operational Safety Branch, send it to the 

attention of the person identified in 

paragraph (j) of this AD and email to: 

AMOC@faa.gov. 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, AIR–520, Continued 

Operational Safety, 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 (i)(2) of this AD, if 

any material 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. 

(j) Additional 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 Dan.Rodina@faa.gov. 

(k) 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 this AD specifies otherwise. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2024–0199, dated October 18, 

2024. 

(ii) [Reserved] 

(3) For EASA material identified in this 

AD, contact EASA, Konrad-Adenauer-Ufer 3, 

50668 Cologne, Germany; telephone +49 221 

8999 000; email ADs@easa.europa.eu; 

website easa.europa.eu.You may find this 

material 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 at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

visit www.archives.gov/federal-register/cfr/ 

ibr-locationsoremailfr.inspection@nara.gov. 

Issued on December 23, 2024. 

Suzanne Masterson, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–31378 Filed 12–30–24; 8:45 am] 

BILLING CODE 4910–13–P 


khammond on DSK9W7S144PROD with PROPOSALS