84262 Federal Register / Vol. 89, No. 204 / Tuesday, October 22, 2024 / Rules and Regulations 

2https://www.fdic.gov/deposit-insurance/ 

questions-and-answers-related-fdics-part-328-finalrule. 

and other banking industry participants, 

the FDIC understands that some IDIs 

would find it beneficial to have 

additional time beyond the January 1, 

2025, compliance date to implement the 

new regulatory requirements under 

subpart A of 12 CFR part 328. In 

particular, some IDIs have reported they 

continue to update online systems and 

platforms, and have requested 

additional time to meet the new 

requirements under subpart A. To 

provide additional opportunity for IDIs 

to put in place processes and systems, 

and make technological updates, the 

FDIC is delaying the compliance date 

for amendments to subpart A of 12 CFR 

part 328 from January 1, 2025, to May 

1, 2025. The compliance date for the 

final rule amendments to subpart B of 

12 CFR part 328 remains January 1, 

2025. 

The FDIC has also received a number 

of questions from industry participants 

regarding the application of the new 

requirements. In response, the FDIC has 

published two sets of ‘‘Questions and 

Answers’’ 2 addressing certain issues 

raised by industry participants. The 

FDIC has continued to receive requests 

for additional clarity. The FDIC will 

continue to evaluate questions that have 

been received and will endeavor to 

make any additional potential 

‘‘Questions and Answers’’ publicly 

available by November 30, 2024, to 

facilitate effective compliance by the 

May 1, 2025, compliance date. 

Federal Deposit Insurance Corporation. 

By order of the Board of Directors. 

Dated at Washington, DC, on October 17, 

2024. 

James P. Sheesley, 

Assistant Executive Secretary. 

[FR Doc. 2024–24433 Filed 10–21–24; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–1889; Project 

Identifier MCAI–2024–00134–T; Amendment 

39–22858; AD 2024–19–16] 

RIN 2120–AA64 

Airworthiness Directives; Deutsche 

Aircraft GmbH (Type Certificate 

Previously Held by 328 Support 

Services GmbH; AvCraft Aerospace 

GmbH; Fairchild Dornier GmbH; 

Dornier Luftfahrt GmbH) Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for all 

Deutsche Aircraft GmbH Model 328–100 

and 328–300 airplanes. This AD was 

prompted by reports of a broken 

attachment eyebolt in a Collins 

Aerospace JB6 Commuter Class 

passenger seat. This AD requires a onetime detailed inspection of each affected 

part, and applicable corrective actions, 

and limits the installation of affected 

parts, as specified in a European Union 

Aviation Safety Agency (EASA) AD, 

which is proposed for incorporation by 

reference (IBR). The FAA is issuing this 

AD to address the unsafe condition on 

these products. 

DATES: This AD is effective November 

26, 2024. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of November 26, 2024. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–1889; 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 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. 

• 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–2024–1889. 

FOR FURTHER INFORMATION CONTACT: 

Todd Thompson, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; 

telephone 206–231–3228; email 

todd.thompson@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 Deutsche Aircraft GmbH 

Model 328–100 and 328–300 airplanes. 

The NPRM published in the Federal 

Register on July 17, 2024 (89 FR 58089). 

The NPRM was prompted by AD 2024– 

0051, dated February 23, 2024, issued 

by EASA, which is the Technical Agent 

for the Member States of the European 

Union (EASA AD 2024–0051) (also 

referred to as the MCAI). The MCAI 

states there have been reports of a 

broken attachment eyebolt in a Collins 

Aerospace JB6 Commuter Class 

passenger seat. The eyebolt is the 

connection between the reclining 

mechanism and the seat structure and 

connects the seat belt to the seat 

structure. Broken attachment eyebolts, if 

not detected and corrected, could 

prevent the correct operation of the 

safety belts, possibly resulting in 

injuries to seat occupants. 

In the NPRM, the FAA proposed to 

require a one-time detailed inspection of 

each affected part, and applicable 

corrective actions, and to limit the 

installation of affected parts, as 

specified in EASA AD 2024–0051. 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–2024–1889. 

Discussion of Final Airworthiness 

Directive 

Comments 

The FAA received no comments on 

the NPRM or on the determination of 

the cost to the public. 

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 


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Federal Register / Vol. 89, No. 204 / Tuesday, October 22, 2024 / Rules and Regulations 84263 

FAA of the unsafe condition described 

in the MCAI referenced above. The FAA 

reviewed the relevant data 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 

EASA AD 2024–0051 specifies a onetime detailed inspection of affected 

eyebolt and spreader for correct 

installation and discrepancies (i.e., 

cracks, traces of aluminum flakes or 

remainders of ripped-out threads in the 

tip threads, and damaged thread runs), 

and applicable corrective actions 

(obtaining and following repair 

instructions and replacing the affected 

parts). EASA AD 2024–0051 also 

specifies an affected part may be 

installed provided, before installation, 

that part passed an inspection (no 

damage detected). 

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 30 

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 

12 work-hours × $85 per hour = $1,020 ..................................................................................... $0 $1,020 $30,600 

The FAA estimates the following 

costs to do any necessary 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 

on-condition action: 

ESTIMATED COSTS OF ON-CONDITION ACTIONS

Labor cost Parts cost Cost per 

product 

1 work-hour × $85 per hour = $85 .......................................................................................................................... $1,126 $1,211 

The FAA has received no definitive 

data on which to base the cost estimates 

for the on-condition repairs specified in 

this AD. 

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: 

2024–19–16 Deutsche Aircraft GmbH (Type 

Certificate Previously Held by 328 

Support Services GmbH; AvCraft 

Aerospace GmbH; Fairchild Dornier 

GmbH; Dornier Luftfahrt GmbH): 

Amendment 39–22858; Docket No. 

FAA–2024–1889; Project Identifier 

MCAI–2024–00134–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective November 26, 2024. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Deutsche Aircraft 

GmbH Model 328–100 and 328–300 

airplanes, certificated in any category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25, Equipment/furnishings. 

(e) Unsafe Condition 

This AD was prompted by reports of a 

broken attachment eyebolt in a Collins 

Aerospace JB6 Commuter Class passenger 

seat. The FAA is issuing this AD to address 

broken attachment eyebolts. The unsafe 

condition, if not addressed, could prevent the 


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84264 Federal Register / Vol. 89, No. 204 / Tuesday, October 22, 2024 / Rules and Regulations 

correct operation of the safety belts, possibly 

resulting in injuries to seat occupants. 

(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 2024–0051, dated 

February 23, 2024 (EASA AD 2024–0051). 

(h) Exceptions to EASA AD 2024–0051 

(1) Where EASA AD 2024–0051 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

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

0051 specifies ‘‘if, during the inspection 

required by paragraph (1) of this AD, 

discrepancies are detected, as defined in the 

ASB, before next flight, contact Deutsche 

Aircraft GmbH and Collins Aerospace for 

approved instructions and accomplish those 

instructions accordingly,’’ this AD requires 

replacing that text with ‘‘if, during the 

inspection as required by paragraph (1) of 

this AD, any discrepancy is detected, the 

discrepancy must be repaired before further 

flight using a method approved by the 

Manager, International Validation Branch, 

FAA; or EASA; or Deutsche Aircraft GmbH’s 

EASA Design Organization Approval (DOA). 

If approved by the DOA, the approval must 

include the DOA-authorized signature.’’ 

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

section of EASA AD 2024–0051. 

(i) No Reporting or Return of Parts 

Requirement 

Although the service information 

referenced in EASA AD 2024–0051 specifies 

to submit certain information and send 

removed parts to the manufacturer, this AD 

does not include that requirement. 

(j) 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, mail it to the address identified in 

paragraph (k) 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 EASA; or Deutsche Aircraft 

GmbH’s EASA DOA. If approved by the 

DOA, the approval must include the DOAauthorized signature. 

(k) Additional Information 

For more information about this AD, 

contact Todd Thompson, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; telephone 206– 

231–3228; email todd.thompson@faa.gov. 

(l) 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) European Union Aviation Safety Agency 

(EASA) AD 2024–0051, dated February 23, 

2024. 

(ii) [Reserved] 

(3) For EASA AD 2024–0051, 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 EASA AD 

on the EASA website ad.easa.europa.eu. 

(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 September 23, 2024. 

Victor Wicklund, 

Deputy Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2024–24386 Filed 10–21–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–0229; Project 

Identifier AD–2023–00485–T; Amendment 

39–22848; AD 2024–19–06] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 737–8 and 

Model 737–9 airplanes. This AD was 

prompted by a Boeing review of the 

standby power system control unit 

(SPCU) design where a single point of 

failure exists internal to the SPCU. This 

AD requires installing four diodes and 

changing wire bundles in the P5 panel, 

as well as performing installation and 

power tests and applicable on-condition 

actions. The FAA is issuing this AD to 

address the unsafe condition on these 

products. 

DATES: This AD is effective November 

26, 2024 . 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of November 26, 2024. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–0229; 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, 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 Boeing material identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Contractual & Data 

Services (C&DS), 2600 Westminster 

Blvd., MC 110–SK57, Seal Beach, CA 

90740–5600; telephone 562–797–1717; 

website myboeingfleet.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–2024–0229. 

FOR FURTHER INFORMATION CONTACT: Raja 

Vengadasalam, Aviation Safety 

Engineer, FAA, 2200 South 216th St., 

Des Moines, WA 98198; telephone 206– 

231–3537; email Raja.Vengadasalam@

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 The Boeing Company 

Model 737–8 and Model 737–9 

airplanes. The NPRM published in the 

Federal Register on February 14, 2024 

(89 FR 11231). The NPRM was 

prompted by a Boeing review of the 

SPCU design where a single point of 

failure exists internal to the SPCU. In 

the NPRM, the FAA proposed to require 

installing four diodes and changing wire 

bundles in the P5 panel, as well as 


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