Federal Register / Vol. 85, No. 235 / Monday, December 7, 2020 / Proposed Rules 78805 

■ c. Adding footnote 2 after ‘‘Market 

Risk Measure for Highly Complex 

Institutions’’. 

The revisions and additions read as 

follows: 

TABLE E.2—EXCLUSIONS FROM CERTAIN RISK MEASURES USED TO CALCULATE THE ASSESSMENT RATE FOR LARGE OR

HIGHLY COMPLEX INSTITUTIONS

Scorecard measures 1 Description Exclusions 

*******

Credit Quality Measure 2 ................ The credit quality score is the higher of the following two scores: 

* * * * * * * 

Market Risk Measure for Highly 

Complex Institutions 2.

The market risk score is a weighted average of the following three 

scores: 

* * * * * * * 

1The applicable portions of the current expected credit loss methodology (CECL) transitional amounts attributable to the allowance for credit 

losses on loans and leases held for investment and added to retained earnings for regulatory capital purposes pursuant to the regulatory capital 

regulations, as they may be amended from time to time (12 CFR part 3, 12 CFR part 217, 12 CFR part 324, 85 FR 61577 (Sept. 30, 2020), and 

84 FR 4222 (Feb. 14, 2019)), will be removed from the sum of Tier 1 capital and reserves throughout the large and highly complex bank scorecards, including in the ratio of Higher-Risk Assets to Tier 1 Capital and Reserves, the Growth-Adjusted Portfolio Concentrations Measure, the 

ratio of Top 20 Counterparty Exposure to Tier 1 Capital and Reserves, the Ratio of Largest Counterparty Exposure to Tier 1 Capital and Reserves, the ratio of Criticized and Classified Items to Tier 1 Capital and Reserves, and the ratio of Underperforming Assets to Tier 1 Capital and 

Reserves. All of these ratios are described in appendix A of this subpart. 2The credit quality score is the greater of the criticized and classified items to Tier 1 capital and reserves score or the underperforming assets 

to Tier 1 capital and reserves score. The market risk score is the weighted average of three scores—the trading revenue volatility to Tier 1 capital score, the market risk capital to Tier 1 capital score, and the level 3 trading assets to Tier 1 capital score. All of these ratios are described in 

appendix A of this subpart and the method of calculating the scores is described in appendix B of this subpart. Each score is multiplied by its respective weight, and the resulting weighted score is summed to compute the score for the market risk measure. An overall weight of 35 percent 

is allocated between the scores for the credit quality measure and market risk measure. The allocation depends on the ratio of average trading 

assets to the sum of average securities, loans and trading assets (trading asset ratio) as follows: (1) Weight for credit quality score = 35 percent 

* (1—trading asset ratio); and, (2) Weight for market risk score = 35 percent * trading asset ratio. In calculating the trading asset ratio, exclude 

from the balance of loans the outstanding balance of loans provided under the Paycheck Protection Program. 

(a) Description of the loss severity measure. The loss severity measure applies a standardized set of assumptions to an institution’s balance 

sheet to measure possible losses to the FDIC in the event of an institution’s failure. To determine an institution’s loss severity rate, the FDIC first 

applies assumptions about uninsured deposit and other liability runoff, and growth in insured deposits, to adjust the size and composition of the 

institution’s liabilities. Exclude total outstanding borrowings from Federal Reserve Banks under the Paycheck Protection Program Liquidity Facility 

from short-and long-term secured borrowings, as appropriate. Assets are then reduced to match any reduction in liabilities. Exclude from an institution’s balance of commercial and industrial loans the outstanding balance of loans provided under the Paycheck Protection Program. In the 

event that the outstanding balance of loans provided under the Paycheck Protection Program exceeds the balance of commercial and industrial 

loans, exclude any remaining balance of loans provided under the Paycheck Protection Program first from the balance of all other loans, up to 

the total amount of all other loans, followed by the balance of agricultural loans, up to the total amount of agricultural loans. Increase cash balances by outstanding loans provided under the Paycheck Protection Program that exceed total outstanding borrowings from Federal Reserve 

Banks under the Paycheck Protection Program Liquidity Facility, if any. The institution’s asset values are then further reduced so that the Leverage Ratio reaches 2 percent. In both cases, assets are adjusted pro rata to preserve the institution’s asset composition. Assumptions regarding 

loss rates at failure for a given asset category and the extent of secured liabilities are then applied to estimated assets and liabilities at failure to 

determine whether the institution has enough unencumbered assets to cover domestic deposits. Any projected shortfall is divided by current domestic deposits to obtain an end-of-period loss severity ratio. The loss severity measure is an average loss severity ratio for the three most recent quarters of data available. The applicable portions of the current expected credit loss methodology (CECL) transitional amounts attributable 

to the allowance for credit losses on loans and leases held for investment and added to retained earnings for regulatory capital purposes pursuant to the regulatory capital regulations, as they may be amended from time to time (12 CFR part 3, 12 CFR part 217, 12 CFR part 324, 85 FR 

61577 (Sept. 30, 2020), and 84 FR 4222 (Feb. 14, 2019)), will be removed from the calculation of the loss severity measure. 

* * * * * 

Federal Deposit Insurance Corporation. 

By order of the Board of Directors. 

Dated at Washington, DC, on November 17, 

2020. 

James P. Sheesley, 

Assistant Executive Secretary. 

[FR Doc. 2020–25830 Filed 12–4–20; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1110; Project 

Identifier MCAI–2020–01003–T] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Canada Limited Partnership (Type 

Certificate Previously Held by C Series 

Aircraft Limited Partnership (CSALP); 

Bombardier, Inc.) Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2019–23–15, which applies to certain 

Airbus Canada Limited Partnership 

Model BD–500–1A10 and BD–500– 

1A11 airplanes. AD 2019–23–15 

requires revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive airworthiness limitations. 

Since the FAA issued AD 2019–23–15, 

the FAA has determined that new or 

more restrictive airworthiness 

limitations are necessary. This proposed 

AD would require revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive airworthiness limitations. 

The FAA is proposing this AD to 


khammond on DSKJM1Z7X2PROD with PROPOSALS
78806 Federal Register / Vol. 85, No. 235 / Monday, December 7, 2020 / Proposed Rules 

address the unsafe condition on these 

products. 

DATES: The FAA must receive comments 

on this proposed AD by January 21, 

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 Airbus Canada 

Limited Partnership, 13100 Henri-Fabre 

Boulevard, Mirabel, Que ́bec, J7N 3C6, 

Canada; telephone 450–476–7676; email 

a220_crc@abc.airbus; internet http://

a220world.airbus.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. 

Examining the AD Docket 

You may examine the AD docket on 

the internet at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

1110; 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. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Andrea Jimenez, Aerospace Engineer, 

Airframe and Propulsion Section, FAA, 

New York ACO Branch, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 

11590; telephone: 516–228–7330; fax: 

516–794–5531; email: 9-avs-nyaco-cos@

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–2020–1110; Project 

Identifier MCAI–2020–01003–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 Andrea Jimenez, 

Aerospace Engineer, Airframe and 

Propulsion Section, FAA, New York 

ACO Branch, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; 

telephone: 516–228–7330; fax: 516– 

794–5531; email: 9-avs-nyaco-cos@

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. 

Discussion 

The FAA issued AD 2019–23–15, 

Amendment 39–19809 (84 FR 67830, 

December 12, 2019) (AD 2019–23–15), 

for certain Airbus Canada Limited 

Partnership Model BD–500–1A10 and 

BD–500–1A11 airplanes. AD 2019–23– 

15 requires revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive airworthiness limitations. AD 

2019–23–15 resulted from a 

determination that new or more 

restrictive airworthiness limitations are 

necessary. The FAA issued AD 2019– 

23–15 to address reduced structural 

integrity of the airplane or reduced 

controllability of the airplane. 

Actions Since AD 2019–23–15 Was 

Issued 

Since the FAA issued AD 2019–23– 

15, the FAA has determined that new or 

more restrictive airworthiness 

limitations are necessary. 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued Canadian AD 

CF–2020–25, dated July 16, 2020 (also 

referred to after this as the Mandatory 

Continuing Airworthiness Information, 

or the MCAI), to correct an unsafe 

condition for certain Airbus Canada 

Limited Partnership Model BD–500– 

1A10 and BD–500–1A11 airplanes. You 

may examine the MCAI in the AD 

docket on the internet at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

1110. 

This proposed AD was prompted by 

a determination that new or more 

restrictive airworthiness limitations are 

necessary. The FAA is proposing this 

AD to address reduced structural 

integrity of the airplane or reduced 

controllability of the airplane. See the 

MCAI for additional background 

information. 

Related Service Information Under 1 

CFR Part 51 

Airbus Canada Limited Partnership 

has issued A220 Airworthiness 

Limitations BD500–3AB48–11400–02, 

Issue 011.00, dated June 18, 2020. This 

service information describes 

airworthiness limitations for fuel tank 

systems, safe life limits, and 

certification maintenance requirements. 

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. 

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 the State 

of Design Authority, the FAA has been 

notified of the unsafe condition 

described in the MCAI and service 

information referenced above. The FAA 

is proposing this AD because the FAA 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop on other products of the same 

type design. 


khammond on DSKJM1Z7X2PROD with PROPOSALS
Federal Register / Vol. 85, No. 235 / Monday, December 7, 2020 / Proposed Rules 78807 

Proposed Requirements of This NPRM 

This proposed AD would retain none 

of the requirements of AD 2019–23–15. 

This proposed AD would require 

revising the existing maintenance or 

inspection program, as applicable, to 

incorporate new or more restrictive 

airworthiness limitations. 

This proposed AD would require 

revisions to certain operator 

maintenance documents to include new 

actions (e.g., inspections) and Critical 

Design Configuration Control 

Limitations (CDCCLs). Compliance with 

these actions and CDCCLs 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 according to paragraph (i)(1) 

of this proposed AD. 

Costs of Compliance 

The FAA estimates that this proposed 

AD affects 11 airplanes of U.S. registry. 

The FAA estimates the following costs 

to comply with this proposed AD: 

The FAA has determined that revising 

the maintenance or inspection program 

takes an average of 90 work-hours 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. Therefore, the agency 

estimates the average total cost per 

operator 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) 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 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) 2019–23–15, Amendment 39– 

19809 (84 FR 67830, December 12, 

2019), and 

■ b. Adding the following new AD: 

Airbus Canada Limited Partnership (Type 

Certificate Previously Held by C Series 

Aircraft Limited Partnership (CSALP); 

Bombardier, Inc.): Docket No. FAA– 

2020–1110; Project Identifier MCAI– 

2020–01003–T. 

(a) Comments Due Date 

The FAA must receive comments by 

January 21, 2021. 

(b) Affected ADs 

This AD replaces AD 2019–23–15, 

Amendment 39–19809 (84 FR 67830, 

December 12, 2019). 

(c) Applicability 

This AD applies to the Airbus Canada 

Limited Partnership Model BD–500–1A10 

and BD–500–1A11 airplanes, certificated in 

any category, identified in paragraphs (c)(1) 

and (2) of this AD. 

(1) Model BD–500–1A10 airplanes, serial 

numbers 50001 and subsequent with an 

original airworthiness certificate or original 

export certificate of airworthiness issued on 

or before June 18, 2020. 

(2) Model BD–500–1A11 airplanes, serial 

numbers 55001 and subsequent with an 

original airworthiness certificate or original 

export certificate of airworthiness issued on 

or before June 18, 2020. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 05, Time Limits/Maintenance 

Checks. 

(e) Reason 

This AD was prompted by a determination 

that new or more restrictive airworthiness 

limitations are necessary. The FAA is issuing 

this AD to address reduced structural 

integrity of the airplane or reduced 

controllability of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) New Maintenance or Inspection Program 

Revision 

Within 90 days after the effective date of 

this AD, revise the existing maintenance or 

inspection program, as applicable, to 

incorporate the information specified in 

Airbus Canada Limited Partnership A220 

Airworthiness Limitations, BD500–3AB48– 

11400–02, Issue 011.00, dated June 18, 2020. 

The initial compliance time for doing the 

tasks is at the time specified in Airbus 

Canada Limited Partnership A220 

Airworthiness Limitations, BD500–3AB48– 

11400–02, Issue 011.00, dated June 18, 2020, 

or within 90 days after the effective date of 

this AD, whichever occurs later. 

(h) New No Alternative Actions, Intervals, or 

Critical Design Configuration Control 

Limitations (CDCCLs) 

After the existing maintenance or 

inspection program has been revised as 

required by paragraph (g) of this AD, no 

alternative actions (e.g., inspections), 

intervals, or CDCCLs may be used unless the 

actions, intervals, and CDCCLs are approved 

as an alternative method of compliance 

(AMOC) in accordance with the procedures 

specified in paragraph (i)(1) of this AD. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York 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 ATTN: Program Manager, 

Continuing Operational Safety, FAA, New 


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78808 Federal Register / Vol. 85, No. 235 / Monday, December 7, 2020 / Proposed Rules 

York ACO Branch, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; telephone 

516–228–7300; fax 516–794–5531. 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, New York ACO Branch, 

FAA; or Transport Canada Civil Aviation 

(TCCA); or Airbus Canada Limited 

Partnership’s TCCA Design Approval 

Organization (DAO). If approved by the DAO, 

the approval must include the DAOauthorized signature. 

(j) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

AD CF–2020–25, dated July 16, 2020, for 

related information. This MCAI may be 

found in the AD docket on the internet at 

https://www.regulations.gov by searching for 

and locating Docket No. FAA–2020–1110. 

(2) For more information about this AD, 

contact Andrea Jimenez, Aerospace Engineer, 

Airframe and Propulsion Section, FAA, New 

York ACO Branch, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; telephone: 

516–228–7330; fax: 516–794–5531; email: 9- 

avs-nyaco-cos@faa.gov. 

(3) For service information identified in 

this AD, contact Airbus Canada Limited 

Partnership, 13100 Henri-Fabre Boulevard, 

Mirabel, Que ́bec, J7N 3C6, Canada; telephone 

450–476–7676; email a220_crc@abc.airbus; 

internet http://a220world.airbus.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. 

Issued on December 1, 2020. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2020–26764 Filed 12–4–20; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1111; Product 

Identifier MCAI–2020–01374–T] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2018–24–03 which applies to all 

Dassault Aviation Model Falcon 10 

airplanes. AD 2018–24–03 requires 

revising the existing maintenance or 

inspection program, as applicable, to 

incorporate new or more restrictive 

maintenance requirements and 

airworthiness limitations. Since the 

FAA issued AD 2018–24–03, the FAA 

has determined that new or more 

restrictive airworthiness limitations are 

necessary. This proposed AD 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. 

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 January 21, 

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 EASA material identified in this 

proposed AD that will be incorporated 

by reference (IBR), contact the EASA, 

Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; telephone +49 221 

8999 000; email ADs@easa.europa.eu; 

internet www.easa.europa.eu. You may 

find this IBR material on the EASA 

website at https://ad.easa.europa.eu. 

For Dassault Aviation service 

information identified in this proposed 

AD, contact Dassault Falcon Jet 

Corporation, Teterboro Airport, P.O. 

Box 2000, South Hackensack, NJ 07606; 

telephone 201–440–6700; internet 

https://www.dassaultfalcon.com. You 

may view this IBR 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 in the AD docket on 

the internet at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

1111. 

Examining the AD Docket 

You may examine the AD docket on 

the internet at https://

www.regulations.gov by searching for 

and locating FAA–2020–1111; 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. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, Large 

Aircraft Section, International 

Validation Branch, FAA, 2200 South 

216th St., Des Moines, WA 98198; 

telephone and fax 206–231–3226; email 

tom.rodriguez@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–2020–1111; Product 

Identifier MCAI–2020–01374–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 

NPRM based on 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 

that are received, without change, to 

https://www.regulations.gov, including 

any personal information you provide. 

The FAA will also post a report 

summarizing each substantive verbal 

contact the FAA receives 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 


khammond on DSKJM1Z7X2PROD with PROPOSALS