Federal Register / Vol. 89, No. 244 / Thursday, December 19, 2024 / Rules and Regulations 103631 

Subpart C—Borrower Management and 

Operations Responsibilities 

■ 3. Amend § 3560.103 by revising and 

republishing paragraph (a)(3)(xx) to read 

as follows: 

§ 3560.103 Maintaining housing projects. 

(a) * * * 

(3) * * * 

(xx) Smoke alarms. The housing 

project must have Qualifying Smoke 

Alarms which are installed in 

accordance with applicable codes and 

standards as set forth in sections 514(k), 

515(m), and 516(c) of the Housing Act 

of 1949 (42 U.S.C. 1471 et seq.), in each 

level and in or near each sleeping area 

in such dwelling unit, including in 

basements but excepting crawl spaces 

and unfinished attics, and in each 

common area in a project containing 

such a dwelling unit. 

(A) Dwelling units built before 

December 29, 2022, and not 

substantially rehabilitated after 

December 29, 2022, smoke alarms must: 

(1) Be hardwired; or 

(2) Use 10-year non rechargeable, 

nonreplaceable primary batteries, 

(i) Be sealed, 

(ii) Tamper resistant, 

(iii) Contain silencing means; and 

(3) Provide notification for persons 

with hearing loss as required by 

applicable standards set forth in 

sections 514(k), 515(m), and 516(c) of 

the Housing Act of 1949 (42 U.S.C. 1471 

et seq.). 

(B) Dwelling units built or 

substantially rehabilitated after 

December 29, 2022; smoke alarms must 

be hardwired. 

* * * * * 

Joaquin Altoro, 

Administrator, Rural Housing Service. 

[FR Doc. 2024–30216 Filed 12–18–24; 8:45 am] 

BILLING CODE 3410–XV–P 

DEPARTMENT OF ENERGY 

10 CFR Part 431 

Energy Efficiency Program for Certain 

Commercial and Industrial Equipment 

CFR Correction 

This rule is being published by the 

Office of the Federal Register to correct 

an editorial or technical error that 

appeared in the most recent annual 

revision of the Code of Federal 

Regulations. 

In Title 10 of the Code of Federal 

Regulations, Parts 200 to 499, revised as 

of January 1, 2024, make the following 

corrections: 

■ 1. Amend Appendix C to subpart R of 

part 431 in section 3.2.7.1, in the table, 

by removing the words ‘‘Table 1’’ and 

adding in its place, the words ‘‘Table 

C.4’’. 

■ 2. Amend Appendix C1 to subpart R 

of part 431 by reinstating the heading 

and introductory text to section 3.2.5 

before Table 15 to read as follows: 

Appendix C1 to Subpart R of Part 431— 

Uniform Test Method for the 

Measurement of Net Capacity and 

AWEF2 of Walk-In Cooler and Walk-In 

Freezer Refrigeration Systems 

* * * * * 

3. * * * 

3.2 * * * 

3.2.5 Test Operating Conditions for TwoCapacity Indoor Matched-Pair or SinglePackaged Refrigeration Systems 

For two-capacity indoor mediumtemperature matched-pair or single-packaged 

refrigeration systems, conduct tests using the 

test conditions specified in table 15 of this 

appendix. For two-capacity indoor lowtemperature matched-pair or single-packaged 

refrigeration systems, conduct tests using the 

test conditions specified in table 16 of this 

appendix. 

* * * * * 

[FR Doc. 2024–30077 Filed 12–18–24; 8:45 am] 

BILLING CODE 0099–10–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–1468; Project 

Identifier MCAI–2023–00975–T; Amendment 

39–22840; AD 2024–18–06] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc., Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Bombardier, Inc., Model BD–700–2A12 

airplanes. This AD was prompted by 

reports that the pivot door pressure 

seals on the thrust reverser fixed 

structure were found disbonded or 

missing on several airplanes. This AD 

requires inspecting the pivot door 

pressure seals and accomplishing 

applicable corrective actions. This AD 

also requires a functional test of the 

thrust reversers. The FAA is issuing this 

AD to address the unsafe condition on 

these products. 

DATES: This AD is effective January 23, 

2025. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of January 23, 2025. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–1468; 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 Bombardier, Inc. material 

identified in this AD, contact 

Bombardier Business Aircraft Customer 

Response Center, 400 Coˆte-Vertu Road 

West, Dorval, Que ́bec H4S 1Y9, Canada; 

telephone 514–855–2999; email ac.yul@

aero.bombardier.com; website: 

bombardier.com. 

• 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–2024–1468. 

FOR FURTHER INFORMATION CONTACT: 

Joseph Catanzaro, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; 

telephone 516–228–7300; email 

joseph.catanzaro@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 certain Bombardier, Inc., Model 

BD–700–2A12 airplanes. The NPRM 

published in the Federal Register on 

May 22, 2024 (89 FR 44933). The NPRM 

was prompted by AD CF–2023–61, 

dated August 16, 2023, issued by 

Transport Canada, which is the aviation 

authority for Canada (Transport Canada 

AD CF–2023–61) (also referred to as the 

MCAI). The MCAI states that the pivot 

door pressure seals on the thrust 

reverser fixed structure were found 

disbonded or missing on several 

airplanes. 

In the NPRM, the FAA proposed to 

require inspecting the pivot door 

pressure seals and accomplishing 

applicable corrective actions. The FAA 

also proposed to require a functional 


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