33574 Federal Register / Vol. 86, No. 120 / Friday, June 25, 2021 / Proposed Rules 

4For the purposes of these Guidelines, for state 

non-member banks and state savings associations, 

‘‘total capital’’ refers to the FDIC-supervised 

institution’s tier 1 capital, as defined in § 324.2 of 

this chapter, plus the allowance for loan and leases 

losses or the allowance for credit losses attributable 

to loans and leases, as applicable. The allowance for 

credit losses attributable to loans and leases is 

applicable for institutions that have adopted the 

Current Expected Credit Losses methodology. 

their aggregate amount reported at least 

quarterly to the institution’s board of 

directors. (See additional reporting 

requirements described under ‘‘Exceptions to 

the General Policy.’’) 

The aggregate amount of all loans in excess 

of the supervisory loan-to-value limits should 

not exceed 100 percent of total capital.4

Moreover, within the aggregate limit, total 

loans for all commercial, agricultural, 

multifamily or other non-1-to-4 family 

residential properties should not exceed 30 

percent of total capital. An institution will 

come under increased supervisory scrutiny 

as the total of such loans approaches these 

levels. 

In determining the aggregate amount of 

such loans, institutions should: (a) Include 

all loans secured by the same property if any 

one of those loans exceeds the supervisory 

loan-to-value limits; and (b) include the 

recourse obligation of any such loan sold 

with recourse. Conversely, a loan should no 

longer be reported to the directors as part of 

aggregate totals when reduction in principal 

or senior liens, or additional contribution of 

collateral or equity (e.g., improvements to the 

real property securing the loan), bring the 

loan-to-value ratio into compliance with 

supervisory limits. 

* * * * * 

Federal Deposit Insurance Corporation. 

By order of the Board of Directors. 

Dated at Washington, DC, on June 15, 2021. 

James P. Sheesley, 

Assistant Executive Secretary. 

[FR Doc. 2021–12973 Filed 6–24–21; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0451; Project 

Identifier AD–2021–00007–T] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2019–01–08, which applies to certain 

The Boeing Company Model 777–200, 

–200LR, –300, and –300ER series 

airplanes. AD 2019–01–08 requires 

modifications for galley mounted 

attendant seat fittings. Since the FAA 

issued AD 2019–01–08, the FAA 

determined that additional airplanes are 

subject to the unsafe condition. This 

proposed AD would retain the 

requirements of AD 2019–01–18 and 

expand the applicability to include 

additional airplanes. The FAA is 

proposing this AD to address the unsafe 

condition on these products. 

DATES: The FAA must receive comments 

on this proposed AD August 9, 2021. 

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 

https://www.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. 

For service information identified in 

this NPRM, 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; 

internet https://

www.myboeingfleet.com. You may view 

this service information 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 https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2021– 

0451. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0451; 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, any comments received, and 

other information. The street address for 

Docket Operations is listed above. 

FOR FURTHER INFORMATION CONTACT: 

Brandon Lucero, Aerospace Engineer, 

Cabin Safety and Environmental 

Systems Section, FAA, Seattle ACO 

Branch, 2200 South 216th St., Des 

Moines, WA 98198; phone and fax: 206– 

231–3569; email: brandon.lucero@

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 ADDRESSES. Include ‘‘Docket No. 

FAA–2021–0451; Project Identifier AD– 

2021–00007–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 the 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 https://

www.regulations.gov, including any 

personal information you provide. The 

agency will also post a report 

summarizing each substantive verbal 

contact received about this proposed 

AD. 

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 Brandon Lucero, 

Aerospace Engineer, Cabin Safety and 

Environmental Systems Section, FAA, 

Seattle ACO Branch, 2200 South 216th 

St., Des Moines, WA 98198; phone and 

fax: 206–231–3569; email: 

brandon.lucero@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 

The FAA issued AD 2019–01–08, 

Amendment 39–19547 (84 FR 4318, 


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Federal Register / Vol. 86, No. 120 / Friday, June 25, 2021 / Proposed Rules 33575 

February 15, 2019) (AD 2019–01–08), 

for certain The Boeing Company Model 

777–200, –200LR, –300, and –300ER 

series airplanes. AD 2019–01–08 was 

prompted by a report that showed noncompliance exists on some in-service 

galley mounted attendant seat fitting 

installations. AD 2019–01–08 requires 

modifications for galley mounted 

attendant seat fittings. The agency 

issued AD 2019–01–08 to address noncompliant flight attendant seats, which 

could fail in a high-G crash and result 

in potential injury to flight attendants 

and consequent inability of the flight 

attendants to assist with passenger 

evacuation in a timely manner. 

Actions Since AD 2019–01–08 Was 

Issued 

Since the FAA issued AD 2019–01– 

08, an operator reported that line 

numbers (L/Ns) 413, 421, 424, 425, 426, 

and 439, which are equipped with 

galley part number (P/N) 

1013G42A00000 (one of the affected 

part numbers identified in Boeing 

Special Attention Service Bulletin 777– 

25–0649, Revision 1, dated October 6, 

2017) were not included in AD 2019– 

01–08. A subsequent investigation by 

Boeing determined that L/Ns 1111, 

1115, and 1137 were also missing from 

the effectivity of Boeing Special 

Attention Service Bulletin 777–25– 

0649, Revision 1, dated October 6, 2017, 

and therefore not included in the 

applicability of AD 2019–01–08. 

FAA’s Determination 

The FAA is issuing this NPRM after 

determining that the unsafe condition 

described previously is likely to exist or 

develop on other products of the same 

type design. 

Related Service Information Under 1 

CFR Part 51 

The FAA reviewed Boeing Special 

Attention Service Bulletin 777–25– 

0649, Revision 2, dated October 8, 2020. 

This service information specifies 

procedures for modifying galley 

mounted attendant seat fittings. This 

service information 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. 

Proposed AD Requirements in This 

NPRM 

Although this proposed AD does not 

explicitly restate the requirements of AD 

2019–01–08, this proposed AD would 

retain all of the requirements of AD 

2019–01–08. Those requirements are 

referenced in the service information 

identified previously, which, in turn, is 

referenced in paragraph (g) of this 

proposed AD. This proposed AD would 

add airplanes to the applicability. This 

proposed AD would also require 

accomplishment of the actions 

identified as ‘‘RC’’ (required for 

compliance) in the Accomplishment 

Instructions of Boeing Special Attention 

Service Bulletin 777–25–0649, Revision 

2, dated October 8, 2020, described 

previously. 

For information on the procedures 

and compliance times, see this service 

information at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2021– 

0451. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 50 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this proposed AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Modification ............................ 7 work-hours × $85 per hour = $595 ..................................... $0 $595 $29,750 

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 that the 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 

2019–01–08, Amendment 39–19547 (84 

FR 4318, February 15, 2019), and 

■ b. Adding the following new 

airworthiness directive: 

The Boeing Company: Docket No. FAA– 

2021–0451; Project Identifier AD–2021– 

00007–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) action by 

August 9, 2021. 

(b) Affected ADs 

This AD replaces AD 2019–01–08, 

Amendment 39–19547 (84 FR 4318, February 

15, 2019) (AD 2019–01–08). 


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(c) Applicability 

This AD applies to The Boeing Company 

Model 777–200, –200LR, –300, and –300ER 

series airplanes, certificated in any category, 

as identified in Boeing Special Attention 

Service Bulletin 777–25–0649, Revision 2, 

dated October 8, 2020. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25, Equipment/furnishings. 

(e) Unsafe Condition 

This AD was prompted by a report that 

showed a non-compliance exists on some inservice galley attendant seat fitting 

installations, and a determination that 

additional airplanes are subject to the unsafe 

condition. The FAA is issuing this AD to 

address non-compliant flight attendant seats, 

which could fail in a high-G crash and result 

in potential injury to flight attendants and 

consequent inability of the flight attendants 

to assist with passenger evacuation in a 

timely manner. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

Except as specified by paragraph (h) of this 

AD: At the applicable times specified in 

paragraph 1.E., ‘‘Compliance,’’ of Boeing 

Special Attention Service Bulletin 777–25– 

0649, Revision 2, dated October 8, 2020, do 

all applicable actions identified as ‘‘RC’’ 

(required for compliance) in, and in 

accordance with, the Accomplishment 

Instructions of Boeing Special Attention 

Service Bulletin 777–25–0649, Revision 2, 

dated October 8, 2020. 

(h) Exception to Service Information 

Specifications 

Where Boeing Special Attention Service 

Bulletin 777–25–0649, Revision 2, dated 

October 8, 2020, uses the phrase ‘‘the 

Revision 2 date of this service bulletin,’’ this 

AD requires using ‘‘the effective date of this 

AD.’’ 

(i) No Reporting Requirement 

Although the service information 

referenced in Boeing Special Attention 

Service Bulletin 777–25–0649, Revision 2, 

dated October 8, 2020, specifies to submit 

certain information to the manufacturer, this 

AD does not include that requirement. 

(j) Credit for Previous Actions 

This paragraph provides credit for the 

actions specified in paragraph (g) of this AD, 

if those actions were performed before the 

effective date of this AD using Boeing Special 

Attention Service Bulletin 777–25–0649, 

Revision 1, dated October 6, 2017 (which is 

incorporated by reference in AD 2019–01– 

08). 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle ACO 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 

certification office, send it to the attention of 

the person identified in Related Information. 

Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the responsible Flight Standards Office. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair, 

modification, or alteration required by this 

AD if it is approved by The Boeing Company 

Organization Designation Authorization 

(ODA) that has been authorized by the 

Manager, Seattle ACO Branch, FAA, to make 

those findings. To be approved, the repair 

method, modification deviation, or alteration 

deviation must meet the certification basis of 

the airplane, and the approval must 

specifically refer to this AD. 

(4) AMOCs approved for AD 2019–01–08 

are approved as AMOCs for the 

corresponding provisions of Boeing Special 

Attention Service Bulletin 777–25–0649, 

Revision 2, dated October 8, 2020, that are 

required by paragraph (g) of this AD. 

(5) For service information that contains 

steps that are labeled as Required for 

Compliance (RC), the provisions of 

paragraphs (k)(5)(i) and (ii) of this AD apply. 

(i) The steps labeled as RC, including 

substeps under an RC step and any figures 

identified in an RC step, must be done to 

comply with the AD. If a step or substep is 

labeled ‘‘RC Exempt,’’ then the RC 

requirement is removed from that step or 

substep. An AMOC is required for any 

deviations to RC steps, including substeps 

and identified figures. 

(ii) Steps not labeled 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 RC steps, 

including substeps and identified figures, can 

still be done as specified, and the airplane 

can be put back in an airworthy condition. 

(l) Related Information 

(1) For more information about this AD, 

contact Brandon Lucero, Aerospace Engineer, 

Cabin Safety and Environmental Systems 

Section, FAA, Seattle ACO Branch, 2200 

South 216th St., Des Moines, WA 98198; 

phone and fax: 206–231–3569; email: 

brandon.lucero@faa.gov. 

(2) For service information 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; internet https://

www.myboeingfleet.com. You may view this 

referenced service information 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. 

Issued on May 28, 2021. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2021–13407 Filed 6–24–21; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0502; Project 

Identifier 2018–CE–043–AD] 

RIN 2120–AA64 

Airworthiness Directives; B–N Group 

Ltd. 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 

certain B–N Group Ltd. Models BN–2, 

BN–2A, BN–2A–2, BN–2A–3, BN–2A–6, 

BN–2A–8, BN–2A–9, BN–2A–20, BN– 

2A–21, BN–2A–26, BN–2A–27, BN–2B– 

20, BN–2B–21, BN–2B–26, BN–2B–27, 

BN–2T, and BN–2T–4R airplanes. This 

proposed AD results from mandatory 

continuing airworthiness information 

(MCAI) originated by an aviation 

authority of another country to identify 

and correct an unsafe condition on an 

aviation product. The MCAI identifies 

the unsafe condition as failure of the 

rudder final drive rod because of cracks 

in the region of the taper pins. This 

proposed AD would require repetitively 

inspecting the rudder final drive rod 

assembly and replacing the rudder final 

drive assembly, if necessary. 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 August 9, 2021. 

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 

https://www.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. 


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