This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents.

Rules and Regulations Federal Register

9283 

Vol. 90, No. 27 

Tuesday, February 11, 2025 

1Available at https://www.whitehouse.gov/ 

presidential-actions/2025/01/regulatory-freezepending-review/. 

2To view the final rule, go to 

www.regulations.gov, and enter APHIS–2015–0008 

in the Search field. 

3To view the notice’s delay of effective date, go 

to www.regulations.gov, and enter APHIS–2014– 

0062 in the Search field. 

DEPARTMENT OF AGRICULTURE 

Office of the Secretary 

7 CFR Part 1 

[Docket No. APHIS–2015–0008] 

RIN 0579–AE68 

Privacy Act Regulations; Delay of 

Effective Date 

AGENCY: Office of the Secretary, U.S. 

Department of Agriculture (USDA). 

ACTION: Final rule; delay of effective 

date. 

SUMMARY: On January 10, 2025, we 

published a final rule that exempted a 

system of records, titled ‘‘Smuggling 

Interdiction and Trade Compliance 

(SITC) National Information 

Communication Activity System 

(SNICAS), USDA/APHIS–21,’’ from 

certain provisions of the Privacy Act. In 

addition, it also amended the Privacy 

Act regulations to reflect an 

administrative change to the list of 

system of records that are exempt from 

certain provisions of the Privacy Act. 

The final rule was scheduled to go into 

effect on February 10, 2025. This 

document delays the effective date until 

April 11, 2025. 

DATES: As of February 7, 2025, the 

effective date for the final rule 

amending 7 CFR 1.123 published on 

January 10, 2025 (90 FR 1847), is 

delayed until April 11, 2025. 

FOR FURTHER INFORMATION CONTACT: Ms. 

Tonya Woods, Director, Freedom of 

Information Act and Privacy Act Staff, 

4700 River Road, Unit 50, Riverdale, 

MD 20737; (301) 851–4076. 

SUPPLEMENTARY INFORMATION: In 

accordance with the memorandum of 

January 20, 2025, from the President to 

executive departments and agencies, 

titled ‘‘Regulatory Freeze Pending 

Review,’’ 1 this action delays the 

effective date of the rule, ‘‘Privacy Act 

Regulations,’’ published in the Federal 

Register on January 10, 2025 (90 FR 

1847–1848; APHIS–2015–0008).2

The final rule USDA’s Privacy Act 

regulations in 7 CFR 1.123 to exempt a 

system of records, titled ‘‘Smuggling 

Interdiction and Trade Compliance 

(SITC) National Information 

Communication Activity System 

(SNICAS), USDA/APHIS–21,’’ from 

certain provisions of the Privacy Act in 

order to avoid interference with law 

enforcement functions. In addition, we 

updated the list of systems exempt from 

certain provisions of the Privacy Act in 

accordance with 5 U.S.C. 552a(k)(2) to 

reflect administrative changes as a result 

of a notice published in the Federal 

Register on November 16, 2001 (66 FR 

57698–57700, Docket No. 99–024–1), 

announcing that USDA combined three 

system of records (Plant Protection and 

Quarantine Program-Regulatory Actions, 

USDA/APHIS–1; Veterinary Services 

Programs-Animal Quarantine 

Regulatory Actions, USDA/APHIS–3; 

and Veterinary Services Programs— 

Animal Welfare and Horse Protection 

Regulatory Actions, USDA/APHIS–4) 

into one system of record: Investigative 

and Enforcement Records Regarding 

Regulatory Activities, USDA/APHIS–1. 

The reason for combining the system of 

records was to bring all records 

concerning investigation and 

enforcement together. However, USDA’s 

Privacy Act regulations were not 

amended to reflect this consolidation, 

which we proposed to rectify. 

In this issue of the Federal Register, 

we are also publishing a delay of 

effective date for the exemptions in the 

system of records notice, ‘‘Smuggling 

Interdiction and Trade Compliance 

(SITC) National Information 

Communication Activity System 

(SNICAS), USDA/APHIS–21,’’ 

associated with this action.3

This action is exempt from notice and 

comment under 5 U.S.C. 553 and is 

effective immediately upon publication 

today in the Federal Register, based on 

the good cause exceptions in 5 U.S.C. 

553(b)(B) and 553(d)(3), respectively. 

Seeking public comment is 

impracticable, unnecessary, and 

contrary to the public interest. The 

delay in the effective date until April 

11, 2025, is necessary to give 

Department officials the opportunity for 

further review and consideration of new 

regulation, consistent with the 

President’s memorandum of January 20, 

2025. Given the imminence of the 

effective date and the brief length of the 

delay of the effective date, seeking prior 

public comment on this delay would 

have been impractical, as well as 

contrary to the public interest in the 

orderly promulgation and 

implementation of regulations. 

Done in Washington, DC, this 6th day of 

February 2025. 

Michael Watson, 

Administrator, Animal and Plant Health 

Inspection Service. 

[FR Doc. 2025–02485 Filed 2–7–25; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2140; Project 

Identifier MCAI–2024–00242–T; Amendment 

39–22942; AD 2025–02–09] 

RIN 2120–AA64 

Airworthiness Directives; Embraer S.A. 

(Type Certificate Previously Held by 

Yabora ̃ Indu ́ stria Aerona ́utica S.A.; 

Embraer S.A.) Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for all 

Embraer S.A. Model EMB–120, –120ER, 

–120FC, –120QC, and –120RT airplanes. 

This AD was prompted by a structural 

assessment, which found that the 

fuselage longitudinal skin splice and 

panel between certain frames are 

susceptible to cracking. This AD 

requires performing repetitive 

inspections of the fuselage center I 

longitudinal skin splice and applicable 

corrective actions, as specified in an 

Ageˆncia Nacional de Aviac ̧a ̃o Civil 

(ANAC) AD, which is incorporated by 

reference (IBR). The FAA is issuing this 

AD to address the unsafe condition on 

these products. 


KHAMMOND on DSK9W7S144PROD with RULES
9284 Federal Register / Vol. 90, No. 27 / Tuesday, February 11, 2025 / Rules and Regulations 

DATES: This AD is effective March 18, 

2025. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of March 18, 2025. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–2140; 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: 

• For ANAC material identified in 

this AD, contact National Civil Aviation 

Agency (ANAC), Aeronautical Products 

Certification Branch (GGCP), Rua Dr. 

Orlando Feirabend Filho, 230—Centro 

Empresarial Aquarius—Torre B— 

Andares 14 a 18, Parque Residencial 

Aquarius, CEP 12.246–190—Sa ̃o Jose ́

dos Campos—SP, Brazil; telephone 55 

(12) 3203–6600; email pac@anac.gov.br; 

website anac.gov.br/en/. You may find 

this material on the ANAC website at 

sistemas.anac.gov.br/certificacao/DA/ 

DAE.asp. 

• 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 at regulations.gov 

under Docket No. FAA–2024–2140. 

FOR FURTHER INFORMATION CONTACT: 

Hassan Ibrahim, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; phone: 

206–231–3653; email: 

Hassan.M.Ibrahim@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to all Embraer S.A. Model EMB– 

120, –120ER, –120FC, –120QC, and 

–120RT airplanes. The NPRM published 

in the Federal Register on September 

17, 2024 (89 FR 75977). The NPRM was 

prompted by AD 2024–04–02R01, 

effective May 31, 2024, issued by 

ANAC, which is the aviation authority 

for Brazil (ANAC AD 2024–04–02R01) 

(also referred to as the MCAI). The 

MCAI states that a structural assessment 

found that the fuselage center I 

longitudinal skin splice and panel 

between frames 22 and 23 are 

susceptible to cracking. 

In the NPRM, the FAA proposed to 

require performing repetitive 

inspections of the fuselage center I 

longitudinal skin splice and applicable 

corrective actions, as specified in ANAC 

AD 2024–04–02R01. The FAA is issuing 

this AD to address the unsafe condition 

on these products. 

You may examine the MCAI in the 

AD docket at regulations.gov under 

Docket No. FAA–2024–2140. 

Discussion of Final Airworthiness 

Directive 

Comments 

The FAA received a comment from 

Embraer. The following presents the 

comment received on the NPRM and the 

FAA’s response. 

Request for Extension of Compliance 

Times 

Embraer requested the FAA extend 

the compliance times of the proposed 

AD. The commenter stated analysis of 

data of the lower fuselage center I 

longitudinal skin splice and panel 

between frames 22 and 23 under 

operational conditions showed the 

probability of cracks is less than one 

percent at 60,000 flight cycles. The 

commenter stated inspections prior to 

the accumulation of 50,000 total flight 

cycles, or within 800 flight cycles after 

the effective date of this AD, whichever 

occurs later, as specified in the 

proposed AD, is overly conservative. 

The commenter suggested inspections 

prior to the accumulation of 60,000 total 

flight cycles, or within 2,000 flight 

cycles after the effective date of this AD, 

whichever occurs later, would meet the 

intent of this AD. Embraer added that 

the compliance times of this AD should 

be extended to avoid an unnecessary 

burden for operators. 

The FAA disagrees with the request. 

Embraer did not provide data to support 

its request to extend the compliance 

times of the proposed AD. However, 

ANAC, the state of design authority, has 

advised the FAA that it defined the 

threshold, intervals, and grace period 

based on a methodology considering the 

findings in the full-scale fatigue test 

(FSFT) and conservative equivalent 

damage. The FAA concurs with ANAC’s 

determination. The FAA has not 

changed this AD as a result of this 

comment. 

Conclusion 

This product has been approved by 

the aviation authority of another 

country and is approved for operation in 

the United States. Pursuant to the FAA’s 

bilateral agreement with this State of 

Design Authority, it has notified the 

FAA of the unsafe condition described 

in the MCAI referenced above. The FAA 

reviewed the relevant data, considered 

the comment received, and determined 

that air safety requires adopting this AD 

as proposed. Accordingly, the FAA is 

issuing this AD to address the unsafe 

condition on this product. Except for 

minor editorial changes, this AD is 

adopted as proposed in the NPRM. 

None of the changes will increase the 

economic burden on any operator. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

ANAC AD 2024–04–02R01 specifies 

initial and repetitive high-frequency 

eddy current inspections for 

discrepancies (including cracks, 

corrosion, scratches, and nicks) of the 

fuselage center I longitudinal skin splice 

and panel between frames 22 and 23, 

from the internal and external sides of 

the fuselage. ANAC AD 2024–04–02R01 

further specifies corrective actions 

including obtaining and implementing 

instructions for repair and reporting of 

the inspection results. 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 ADDRESSES

section. 

Costs of Compliance 

The FAA estimates this AD affects 51 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this AD: 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per product Cost on U.S. operators 

4 work-hours × $85 per hour = $340 per 

inspection cycle.

$0 $340 per inspection cycle ......................... $17,340 per inspection cycle. 


KHAMMOND on DSK9W7S144PROD with RULES
Federal Register / Vol. 90, No. 27 / Tuesday, February 11, 2025 / Rules and Regulations 9285 

The FAA has received no definitive 

data on which to base the cost estimates 

for the corrective actions specified in 

this 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 

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 

■ 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: 

2025–02–09 Embraer S.A. (Type Certificate 

Previously Held by Yabora ̃ Indu ́ stria 

Aerona ́utica S.A.; Embraer S.A.): 

Amendment 39–22942; Docket No. 

FAA–2024–2140; Project Identifier 

MCAI–2024–00242–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective March 18, 2025. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Embraer S.A. (Type 

Certificate previously held by Yabora ̃

Indu ́ stria Aerona ́utica S.A.; Embraer S.A.) 

Model EMB–120, –120ER, –120FC, –120QC, 

and –120RT airplanes, certificated in any 

category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 53, Fuselage. 

(e) Unsafe Condition 

This AD was prompted by a structural 

assessment that indicated the fuselage center 

I longitudinal skin splice and panel between 

frames 22 and 23 are susceptible to cracking. 

The FAA is issuing this AD to address 

undetected cracks in the fuselage center I 

longitudinal skin splice and panel between 

frames 22 and 23. The unsafe condition, if 

not addressed, could result in undetected 

fuselage crack propagation, and 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, Ageˆncia Nacional de 

Aviac ̧a ̃o Civil (ANAC) AD 2024–04–02R01, 

effective May 31, 2024 (ANAC AD 2024–04– 

02R01). 

(h) Exceptions to ANAC AD 2024–04–02R01 

(1) Where ANAC AD 2024–04–02R01 refers 

to its effective date, this AD requires using 

the effective date of this AD. 

(2) Where paragraphs (b)(1) and (2) of 

ANAC AD 2024–04–02R01 specify the initial 

compliance time for the high-frequency eddy 

current inspection of the fuselage center I 

longitudinal skin splice—frames 22 and 23, 

from the internal and external side of the 

fuselage, for this AD, the initial compliance 

time for doing the high-frequency eddy 

current inspection is prior to the 

accumulation of 50,000 total flight cycles, or 

within 800 flight cycles after the effective 

date of this AD, whichever occurs later. 

(3) Where paragraphs (d)(1) and (2) of 

ANAC AD 2024–04–02R01 specify the initial 

compliance time for the high-frequency eddy 

current inspection of the fuselage center I 

skin panel—frames 22 and 23, from the 

external side of the fuselage, for this AD, the 

initial compliance time for doing the highfrequency eddy current inspection is prior to 

the accumulation of 50,000 total flight cycles, 

or within 800 flight cycles after the effective 

date of this AD, whichever occurs later. 

(4) Where paragraphs (b)(3) and (d)(3) of 

ANAC AD 2024–04–02R01 specify corrective 

actions, for this AD, if any discrepancy 

including cracking is detected during any 

inspection required by this AD, the 

discrepancy must be repaired before further 

flight using a method approved by the 

Manager, International Validation Branch, 

FAA; or ANAC; or Embraer’s ANAC Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(5) Paragraph (f) of ANAC AD 2024–04– 

02R01 specifies to report inspection results to 

ANAC and Embraer 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. 

(6) This AD does not adopt paragraph (g) 

of ANAC AD 2024–04–02R01. 

(i) Additional AD Provisions 

The following provisions also apply to this 

AD: 


KHAMMOND on DSK9W7S144PROD with RULES
9286 Federal Register / Vol. 90, No. 27 / Tuesday, February 11, 2025 / Rules and Regulations 

(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 manager of the International Validation 

Branch, mail it to the address identified in 

paragraph (j) of this AD. Information may be 

emailed 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, International Validation 

Branch, FAA; or ANAC; or ANAC’s 

authorized Designee. If approved by the 

ANAC Designee, the approval must include 

the Designee’s authorized signature. 

(j) Additional Information 

For more information about this AD, 

contact Hassan Ibrahim, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; phone: 206–231– 

3653; email: Hassan.M.Ibrahim@faa.gov. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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) Ageˆncia Nacional de Aviac ̧a ̃o Civil 

(ANAC) AD 2024–04–02R01, effective May 

31, 2024. 

(ii) [Reserved] 

(3) For ANAC material identified in this 

AD, contact ANAC, Aeronautical Products 

Certification Branch (GGCP), Rua Dr. Orlando 

Feirabend Filho, 230—Centro Empresarial 

Aquarius—Torre B—Andares 14 a 18, Parque 

Residencial Aquarius, CEP 12.246–190—Sa ̃o 

Jose ́ dos Campos—SP, Brazil; phone 55 (12) 

3203–6600; email pac@anac.gov.br; website 

anac.gov.br/en/. You may find this ANAC 

AD on the ANAC website 

sistemas.anac.gov.br/certificacao/DA/ 

DAE.asp. 

(4) You may view this material at the FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 2200 South 216th Street, 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-locations, or email fr.inspection@

nara.gov. 

Issued on January 23, 2025. 

Steven W. Thompson, 

Acting Deputy Director, Compliance & 

Airworthiness Division, Aircraft Certification 

Service. 

[FR Doc. 2025–02400 Filed 2–10–25; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2025–0198; Project 

Identifier MCAI–2024–00762–T; Amendment 

39–22956; AD 2025–03–08] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for all 

Airbus SAS Model A318, A319, A320, 

and A321 series airplanes; Model A330– 

200, –200 Freighter, –300, –800, and 

–900 series airplanes; and Model A340– 

200, –300, –500, and –600 series 

airplanes. This AD was prompted by 

reports of trimmable horizontal 

stabilizer actuators (THSAs) being 

delivered to operators having erroneous 

information (accumulated life) in the 

authorized release certificate. This AD 

requires contacting Collins Aerospace 

for amended authorized release 

certificates for the affected parts and 

replacing the affected parts if necessary, 

and prohibits the installation of affected 

parts, 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 February 26, 

2025. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of February 26, 2025. 

The FAA must receive comments on 

this AD by March 28, 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–2025–0198; 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 street address for 

Docket Operations is listed above. 

Material Incorporated by Reference: 

• For EASA material identified in this 

AD, contact EASA, Konrad-AdenauerUfer 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. 

• For Collins Aerospace material 

identified in this AD, contact Collins 

Aerospace, Product Support Department 

13, Avenue de L’Eguillette—Saint-Ouen 

L’Aumone, Boite Postale 7186 95056 

Cergy Pontoise Cedex, France; 

telephone 1–877–808–7575; email crc@

collins.com; website https://www.collins

aerospace.com/support. 

• 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 at regulations.gov 

under Docket No. FAA–2025–0198. 

FOR FURTHER INFORMATION CONTACT: 

Timothy Dowling, Aviation Safety 

Engineer, FAA, 2200 South 216th St., 

Des Moines, WA 98198; phone 206– 

231–3667; email timothy.p.dowling@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

The FAA invites you to send any 

written data, views, or arguments about 

this final rule. Send your comments to 

an address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2025–0198; Project Identifier MCAI– 

2024–00762–T’’ at the beginning of your 

comments. The most helpful comments 

reference a specific portion of the final 

rule, 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 final rule 

because of those comments. 


KHAMMOND on DSK9W7S144PROD with RULES