Federal Register / Vol. 89, No. 190 / Tuesday, October 1, 2024 / Proposed Rules 79789 

part 1227 of chapter XII of title 12 of the 

Code of Federal Regulations as follows: 

PART 1227—SUSPENDED 

COUNTERPARTY PROGRAM 

■ 1. The authority citation for part 1227 

continues to read as follows: 

Authority: 12 U.S.C. 4513, 4513b, 4514, 

4526. 

■ 2. Amend § 1227.2 by: 

■ a. Adding the definition of ‘‘Civil 

monetary penalty’’ in alphabetical 

order; 

■ b. Revising the definition of ‘‘Covered 

misconduct’’; 

■ c. Adding the definition of 

‘‘Prohibition order’’ in alphabetical 

order. 

The additions and revisions read as 

follows: 

§ 1227.2 Definitions. 

* * * * * 

Civil monetary penalty order means 

any order issued by the U.S. Department 

of Housing and Urban Development, 

U.S. Department of Agriculture, or U.S. 

Department of Veterans Affairs, 

pursuant to the relevant Federal 

agency’s authority to impose civil 

monetary penalties, that requires a 

person to pay an amount no less than 

$1,000,000. 

* * * * * 

Covered misconduct means: 

(1) Any conviction, prohibition order, 

civil monetary penalty order, or 

administrative sanction within the past 

three (3) years if the basis of such action 

involved fraud, embezzlement, theft, 

conversion, forgery, bribery, perjury, 

making false statements or claims, tax 

evasion, obstruction of justice, or any 

similar offense, or, with respect to a 

civil monetary penalty order only, 

breach of contract, in each case in 

connection with a mortgage, mortgage 

business, mortgage securities or other 

lending product, or ownership or 

management of real property. 

* * * * * 

Prohibition order means any order 

issued by: 

(1) The Board of Governors of the 

Federal Reserve System, the Federal 

Deposit Insurance Corporation, the 

Office of the Comptroller of the 

Currency, or the National Credit Union 

Administration that has the effect of 

prohibiting a person from participating 

in the affairs of any institution for 

which the Federal agency has 

supervisory authority; 

(2) The Consumer Financial 

Protection Bureau that has the effect of 

prohibiting a person from participating 

in mortgage- or real estate-related 

activities; or 

(3) The Securities and Exchange 

Commission or the Commodity Futures 

Trading Commission, or a judicial 

authority, that has the effect of 

prohibiting a person from participating 

in the relevant regulated market 

overseen by the Federal agency. 

* * * * * 

Sandra L. Thompson, 

Director, Federal Housing Finance Agency. 

[FR Doc. 2024–22393 Filed 9–30–24; 8:45 am] 

BILLING CODE 8070–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2323; Project 

Identifier MCAI–2024–00171–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 

supersede Airworthiness Directive (AD) 

2022–22–10, which applies to certain 

Airbus SAS Model A318, A319, A320, 

and A321 series airplanes. AD 2022–22– 

10 requires revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive airworthiness limitations. 

Since the FAA issued AD 2022–22–10, 

the FAA has determined that new or 

more restrictive airworthiness 

limitations are necessary. This proposed 

AD would continue to require certain 

actions in AD 2022–22–10 and would 

require revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive airworthiness limitations, 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. 

DATES: The FAA must receive comments 

on this proposed AD by November 15, 

2024. 

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–2024–2323; 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– 

2024–2323. 

• 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: 

Timothy Dowling, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; phone 

206–231–3367; email: 

timothy.p.dowling@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–2024–2323; Project 

Identifier MCAI–2024–00171–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 


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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 Timothy Dowling, 

Aviation Safety Engineer, FAA, 1600 

Stewart Avenue, Suite 410, Westbury, 

NY 11590; phone: 206–231–3367; email: 

timothy.p.dowling@faa.gov. Any 

commentary that the FAA receives that 

is not specifically designated as CBI will 

be placed in the public docket for this 

rulemaking. 

Background 

The FAA issued AD 2022–22–10, 

Amendment 39–22225 (87 FR 72374, 

November 25, 2022) (AD 2022–22–10), 

for certain Airbus SAS Model A318, 

A319, A320, and A321 series airplanes. 

AD 2022–22–10 was prompted by an 

MCAI originated by EASA, which is the 

Technical Agent for the Member States 

of the European Union. EASA issued 

AD 2022–0082, dated May 10, 2022 

(EASA AD 2022–0082) (which 

corresponds to FAA AD 2022–22–10), to 

correct an unsafe condition. 

AD 2022–22–10 requires revising the 

existing maintenance or inspection 

program, as applicable, to incorporate 

additional new or more restrictive 

airworthiness limitations. The FAA 

issued AD 2022–22–10 to address 

failure of certain life-limited parts, 

which could result in reduced structural 

integrity of the airplane. 

Actions Since AD 2022–22–10 Was 

Issued 

Since the FAA issued AD 2022–22– 

10, EASA superseded AD 2022–0082 

and issued EASA AD 2024–0066, dated 

March 8, 2024 (EASA AD 2024–0066) 

(referred to after this as the MCAI), for 

all Airbus SAS Model A318, A319, and 

A321 series airplanes; and Model A320– 

211, –212, –214, –215, –216, –231, –232, 

–233, –251N, –252N, –253N, –271N, 

–272N, and –273N airplanes. Model 

A320–215 airplanes are not certificated 

by the FAA and are not included on the 

U.S. type certificate data sheet; this 

proposed AD therefore does not include 

those airplanes in the applicability. The 

MCAI states that new or more restrictive 

airworthiness limitations have been 

developed. 

Airplanes with an original 

airworthiness certificate or original 

export certificate of airworthiness 

issued after November 6, 2023, must 

comply with the airworthiness 

limitations specified as part of the 

approved type design and referenced on 

the type certificate data sheet; this 

proposed AD therefore does not include 

those airplanes in the applicability. 

The FAA is proposing this AD to 

address failure of certain life-limited 

parts, which could result in reduced 

structural integrity of the airplane. You 

may examine the MCAI in the AD 

docket at regulations.gov under Docket 

No. FAA–2024–2323. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

EASA AD 2024–0066 specifies new or 

more restrictive airworthiness tasks and 

limitations for airplane structures and 

safe life limits. 

This proposed AD would also require 

EASA AD 2022–0082, which the 

Director of the Federal Register 

approved for incorporation by reference 

as of December 30, 2022 (87 FR 72374, 

November 25, 2022). 

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 MCAIs 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. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would retain 

certain requirements of AD 2022–22–10. 

This proposed AD would also require 

revising the existing maintenance or 

inspection program, as applicable, to 

incorporate additional new or more 

restrictive airworthiness limitations, 

which are specified in EASA AD 2024– 

0066 already described, as proposed for 

incorporation by reference. Any 

differences with EASA AD 2024–0066 

are identified as exceptions in the 

regulatory text of this proposed AD. 

This proposed AD would require 

revisions to certain operator 

maintenance documents to include new 

actions (e.g., inspections). Compliance 

with these actions is required by 14 CFR 

91.403(c). For airplanes that have been 

previously modified, altered, or repaired 

in the areas addressed by this proposed 

AD, the operator may not be able to 

accomplish the actions described in the 

revisions. In this situation, to comply 

with 14 CFR 91.403(c), the operator 

must request approval for an alternative 

method of compliance (AMOC) 

according to paragraph (m)(1) 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 

retain the IBR of EASA AD 2022–0082 

and incorporate EASA AD 2024–0066 

by reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2022–0082 

and EASA AD 2024–0066 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 2022–0082 or EASA AD 

2024–0066 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 

2022–0082 or EASA AD 2024–0066. 

Material required by EASA AD 2022– 

0082 and EASA AD 2024–0066 for 

compliance will be available at 

regulations.gov by searching for and 

locating Docket No. FAA–2024–2323 

after the FAA final rule is published. 

Airworthiness Limitation ADs Using 

the New Process 

The FAA’s process of incorporating 

by reference MCAI ADs as the primary 


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source of information for compliance 

with corresponding FAA ADs has been 

limited to certain MCAI ADs (primarily 

those with service bulletins as the 

primary source of information for 

accomplishing the actions required by 

the FAA AD). However, the FAA is now 

expanding the process to include MCAI 

ADs that require a change to 

airworthiness limitation documents, 

such as airworthiness limitation 

sections. 

For these ADs that incorporate by 

reference an MCAI AD that changes 

airworthiness limitations, the FAA 

requirements are unchanged. Operators 

must revise the existing maintenance or 

inspection program, as applicable, to 

incorporate the information specified in 

the new airworthiness limitation 

document. The airworthiness 

limitations must be followed according 

to 14 CFR 91.403(c) and 91.409(e). 

The previous format of the 

airworthiness limitation ADs included a 

paragraph that specified that no 

alternative actions (e.g., inspections) or 

intervals may be used unless the actions 

and intervals are approved as an AMOC 

in accordance with the procedures 

specified in the AMOCs paragraph 

under ‘‘Additional AD Provisions.’’ This 

new format includes a ‘‘New Provisions 

for Alternative Actions and Intervals’’ 

paragraph that does not specifically 

refer to AMOCs, but operators may still 

request an AMOC to use an alternative 

action or interval. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 1,857 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this proposed AD: 

The FAA estimates the total cost per 

operator for the retained actions from 

AD 2022–22–10 to be $7,650 (90 workhours × $85 per work-hour). 

The FAA has determined that revising 

the existing maintenance or inspection 

program takes an average of 90 workhours per operator, although the agency 

recognizes that this number may vary 

from operator to operator. Since 

operators incorporate maintenance or 

inspection program changes for their 

affected fleet(s), the FAA has 

determined that a per-operator estimate 

is more accurate than a per-airplane 

estimate. 

The FAA estimates the total cost per 

operator for the new proposed actions to 

be $7,650 (90 work-hours × $85 per 

work-hour). 

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: 

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: 

■ a. Removing Airworthiness Directive 

(AD) 2022–22–10, Amendment 39– 

22225 (87 FR 72374, November 25, 

2022); and 

■ b. Adding the following new AD: 

Airbus SAS: Docket No. FAA–2024–2323; 

Project Identifier MCAI–2024–00171–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

AD by November 15, 2024. 

(b) Affected ADs 

This AD replaces AD 2022–22–10, 

Amendment 39–22225 (87 FR 72374, 

November 25, 2022) (AD 2022–22–10). 

(c) Applicability 

This AD applies to Airbus SAS Model 

airplanes identified in paragraphs (c)(1) 

through (4) of this AD, certificated in any 

category, with an original airworthiness 

certificate or original export certificate of 

airworthiness issued on or before November 

6, 2023. 

(1) A318–111, –112, –121, and –122 

airplanes. 

(2) A319–111, –112, –113, –114, –115, 

–131, –132, –133, –151N, –153N, and –171N 

airplanes. 

(3) A320–211, –212, –214, –216, –231, 

–232, –233, –251N, –252N, –253N, –271N, 

–272N, and –273N airplanes. 

(4) A321–111, –112, –131, –211, –212, 

–213, –231, –232, –251N, –252N, –253N, 

–271N, –272N, –251NX, –252NX, –253NX, 

–271NX, and –272NX airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 05, Time Limits/Maintenance 

Checks. 

(e) Unsafe Condition 

This AD was prompted by a determination 

that new or more restrictive airworthiness 

limitations are necessary. The FAA is issuing 

this AD to address failure of certain lifelimited parts. The unsafe condition, if not 

addressed, could result in reduced structural 

integrity of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Revision of the Existing 

Maintenance or Inspection Program, With a 

New Terminating Action 

This paragraph restates the requirements of 

paragraph (j) of AD 2022–22–10, with a new 

terminating action. For airplanes with an 

original airworthiness certificate or original 

export certificate of airworthiness issued on 

or before February 2, 2022, except as 

specified in paragraph (h) of this AD: Comply 

with all required actions and compliance 

times specified in, and in accordance with, 

European Union Aviation Safety Agency 

(EASA) AD 2022–0082, dated May 10, 2022 

(EASA AD 2022–0082). Accomplishing the 

revision of the existing maintenance or 

inspection program required by paragraph (j) 

of this AD terminates the requirements of this 

paragraph. 


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(h) Retained Exceptions to EASA AD 2022– 

0082, With No Changes 

This paragraph restates the exceptions 

specified in paragraph (k) of AD 2022–22–10, 

with no changes. 

(1) Where EASA AD 2022–0082 refers to its 

effective date, this AD requires using 

December 30, 2022 (the effective date of AD 

2022–22–10). 

(2) The requirements specified in 

paragraph (1) of EASA AD 2022–0082 do not 

apply to this AD. 

(3) Paragraph (2) of EASA AD 2022–0082 

specifies revising ‘‘the approved AMP’’ 

within 12 months after its effective date, but 

this AD requires revising the existing 

maintenance or inspection program, as 

applicable, within 90 days after December 30, 

2022 (the effective date of AD 2022–22–10). 

(4) The initial compliance time for doing 

the tasks specified in paragraph (2) of EASA 

AD 2022–0082 is at the applicable 

‘‘limitations’’ as incorporated by the 

requirements of paragraph (2) of EASA AD 

2022–0082, or within 90 days after December 

30, 2022 (the effective date of AD 2022–22– 

10), whichever occurs later. 

(5) The provisions specified in paragraphs 

(3) and (4) of EASA AD 2022–0082 do not 

apply to this AD. 

(6) The ‘‘Remarks’’ section of EASA AD 

2022–0082 does not apply to this AD. 

(i) Retained Restrictions on Alternative 

Actions and Intervals, With a New Exception 

This paragraph restates the requirements of 

paragraph (l) of AD 2022–22–10, with a new 

exception. Except as required by paragraph 

(j) of this AD, after the existing maintenance 

or inspection program has been revised as 

required by paragraph (g) of this AD, no 

alternative actions (e.g., inspections) and 

intervals are allowed unless they are 

approved as specified in the provisions of the 

‘‘Ref. Publications’’ section of EASA AD 

2022–0082. 

(j) New Revision of the Existing Maintenance 

or Inspection Program 

Except as specified in paragraph (k) of this 

AD: Comply with all required actions and 

compliance times specified in, and in 

accordance with, EASA AD 2024–0066, 

dated March 8, 2024 (EASA AD 2024–0066). 

Accomplishing the revision of the existing 

maintenance or inspection program required 

by this paragraph terminates the 

requirements of paragraph (g) of this AD. 

(k) Exceptions to EASA AD 2024–0066 

(1) This AD does not adopt the 

requirements specified in paragraph (1) of 

EASA AD 2024–0066. 

(2) Paragraph (2) of EASA AD 2024–0066 

specifies revising ‘‘the approved AMP,’’ 

within 12 months after its effective date, but 

this AD requires revising the existing 

maintenance or inspection program, as 

applicable, within 90 days after the effective 

date of this AD. 

(3) The initial compliance time for doing 

the tasks specified in paragraph (2) of EASA 

AD 2024–0066 is at the applicable 

‘‘limitations’’ as incorporated by the 

requirements of paragraph (2) of EASA AD 

2024–0066, or within 90 days after the 

effective date of this AD, whichever occurs 

later. 

(4) This AD does not adopt the provisions 

specified in paragraphs (3) and (4) of EASA 

AD 2024–0066. 

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

section of EASA AD 2024–0066. 

(l) New Provisions for Alternative Actions 

and Intervals 

After the existing maintenance or 

inspection program has been revised as 

required by paragraph (j) of this AD, no 

alternative actions (e.g., inspections) and 

intervals are allowed unless they are 

approved as specified in the provisions of the 

‘‘Ref. Publications’’ section of EASA AD 

2024–0066. 

(m) Additional AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Validation Branch, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or 

responsible Flight Standards Office, as 

appropriate. If sending information directly 

to the manager of the International Validation 

Branch, send it to the attention of the person 

identified in paragraph (n) of this AD and 

email to: AMOC@faa.gov. 

(i) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the responsible Flight Standards Office. 

(ii) AMOCs approved previously for AD 

2022–22–10 are approved as AMOCs for the 

corresponding provisions of EASA AD 2024– 

0066 that are required by paragraph (g) of this 

AD. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain instructions 

from a manufacturer, the instructions must 

be accomplished using a method approved 

by the Manager, International Validation 

Branch, FAA; or EASA; or Airbus SAS’s 

EASA Design Organization Approval (DOA). 

If approved by the DOA, the approval must 

include the DOA-authorized signature. 

(n) Additional Information 

For more information about this AD, 

contact Timothy Dowling, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

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

3367; email: timothy.p.dowling@faa.gov. 

(o) 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. 

(3) The following material was approved 

for IBR on [DATE 35 DAYS AFTER 

PUBLICATION OF THE FINAL RULE]. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2024–0066, dated March 8, 2024. 

(ii) [Reserved] 

(4) The following material was approved 

for IBR on December 30, 2022 (87 FR 72374, 

November 25, 2022). 

(i) EASA AD 2022–0082, dated May 10, 

2022. 

(ii) [Reserved] 

(5) 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. 

(6) 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. 

(7) 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 September 25, 2024. 

Peter A. White, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–22444 Filed 9–30–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2024–2274 Airspace 

Docket No. 22–AAL–80] 

RIN 2120–AA66 

Amendment of Alaskan Very High 

Frequency Omnidirectional Range 

Federal Airway V–510 in Alaska 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: This action proposes to 

amend Alaskan Very High Frequency 

Omnidirectional Range (VOR) Federal 

Airway V–510 in Alaska. This proposed 

action is due to the decommissioning of 

the Anvik Nondirectional Radio Beacon 

(NDB) in Alaska. 

DATES: Comments must be received on 

or before November 15, 2024. 

ADDRESSES: Send comments identified 

by FAA Docket No. FAA–2024–2274 

and Airspace Docket No. 22–AAL–80 

using any of the following methods: 

* Federal eRulemaking Portal: Go to 

www.regulations.gov and follow the 

online instructions for sending your 

comments electronically. 

* Mail: Send comments to Docket 

Operations, M–30; U.S. Department of 


khammond on DSKJM1Z7X2PROD with PROPOSALS