This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents.

Rules and Regulations Federal Register

29025 

Vol. 87, No. 92 

Thursday, May 12, 2022 

OFFICE OF MANAGEMENT AND 

BUDGET 

2 CFR Part 200 

Uniform Administrative Requirements, 

Cost Principles, and Audit 

Requirements 

AGENCY: Office of Management and 

Budget. 

ACTION: Guidance. 

SUMMARY: This document announces the 

availability of the 2022 Compliance 

Supplement (2022 Supplement) for the 

Office of Management and Budget’s 

uniform administrative requirements, 

cost principles, and audit requirements 

regulations. This document also offers 

interested parties an opportunity to 

comment on the 2022 Supplement. 

DATES: The 2022 Supplement replaces 

the 2021 Supplement (issued in August 

2020), its Addenda 1 & 2 (issued in 

December 2021 and January 2022), and 

the technical update (issued April 

2022). The Supplement applies to fiscal 

year audits that cover any period 

beginning after June 30, 2021. 

All comments to the 2022 

Supplement must be in writing and 

received by July 11, 2022. Late 

comments will be considered to the 

extent practicable. 

ADDRESSES: Comments will be reviewed 

and addressed, when appropriate, in the 

2023 Compliance Supplement. 

Electronic mail comments may be 

submitted to: http://

www.regulations.gov. Please include ‘‘2 

CFR part 200 Subpart F—Audit 

Requirements, Appendix XI— 

Compliance Supplement—2022’’ in the 

subject line and the full body of your 

comments in the text of the electronic 

message and as an attachment. Please 

include your name, title, organization, 

postal address, telephone number, and 

email address in the text of the message. 

Comments may also be sent to: 

GrantsTeam@omb.eop.gov. 

Please note that all public comments 

received are subject to the Freedom of 

Information Act and will be posted in 

their entirety, including any personal 

and/or business confidential 

information provided. Do not include 

any information you would not like to 

be made publically available. 

The 2022 Supplement is available 

online on the OMB home page at 

https://www.whitehouse.gov/omb/ 

office-federal-financial-management/. 

FOR FURTHER INFORMATION CONTACT: 

Recipients and auditors should contact 

their cognizant or oversight agency for 

audit, or Federal awarding agency, as 

appropriate. The Federal agency 

contacts are listed in appendix III of the 

Supplement. Subrecipients should 

contact their pass-through entity. 

Federal agencies should contact Gil 

Tran at Hai_M._Tran@omb.eop.gov or 

(202) 881–7830 or the OMB Grants team 

at GrantsTeam@omb.eop.gov. 

SUPPLEMENTARY INFORMATION: The 2022 

Supplement (2 CFR part 200, subpart F, 

and appendix XI to Part 200) adds five 

new programs (that are funded by the 

American Rescue Plan Act) and 

provides updates on many other 

programs, where necessary. In total, the 

2022 Supplement contains audit 

guidance for 235 individual programs 

and 48 clusters of programs from 22 

Federal agencies. The 2022 Supplement 

is a continuation of efforts to maximize 

the value of grant funding by applying 

a risk-based, data-driven framework that 

balances compliance requirements with 

demonstrating successful results. It 

requires a review for performance 

reporting for 63 programs. 

As part of the development of the 

audit guidance contained in the 

Supplement, OMB shared the draft 

language developed by the agencies 

with recipient and audit stakeholders, 

including the American Institute of 

Certified Public Accountants (AICPA), 

the National Association of State 

Auditors, Controllers and Treasurers 

(NASACT), the U.S. Government 

Accountability Office (GAO), and 

agency Inspector General offices for 

comments. The comments were 

reviewed, adjudicated, and addressed 

by the relevant agencies and OMB. All 

necessary changes are reflected in the 

final published version. 

Deidre A. Harrison, 

Acting Controller. 

[FR Doc. 2022–10182 Filed 5–11–22; 8:45 am] 

BILLING CODE 3110–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0016; Project 

Identifier MCAI–2021–00945–T; Amendment 

39–22022; AD 2022–09–02] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc., Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Bombardier, Inc., Model BD–100–1A10 

airplanes. This AD was prompted by a 

report that the nose wheel steering 

selector valve (SSV) can be slow to 

deactivate under low temperature 

conditions. This AD requires replacing 

the affected nose wheel SSV with a 

redesigned nose wheel SSV, and 

performing an operational test of the 

nose wheel SSV and nose wheel 

steering control system. This AD also 

prohibits the installation of a certain 

nose wheel SSV. The FAA is issuing 

this AD to address the unsafe condition 

on these products. 

DATES: This AD is effective June 16, 

2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 16, 2022. 

ADDRESSES: For service information 

identified in this final rule, 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; internet http://

www.bombardier.com. You may view 

this service information at the FAA, 

Airworthiness Products Section, 

Operational Safety Branch, 2200 South 

216th St., Des Moines, WA. For 


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29026 Federal Register / Vol. 87, No. 92 / Thursday, May 12, 2022 / Rules and Regulations 

information on the availability of this 

material at the FAA, call 206–231–3195. 

It is also available on the internet at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0016. 

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–2022– 

0016; 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. 

FOR FURTHER INFORMATION CONTACT: 

Chirayu Gupta, Aerospace Engineer, 

Mechanical Systems and Administrative 

Services Section, FAA, New York ACO 

Branch, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; telephone 

516–228–7300; email 9-avs-nyaco-cos@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued TCCA AD CF– 

2021–29, dated August 18, 2021 (TCCA 

AD CF–2021–29) (also referred to as the 

MCAI), to correct an unsafe condition 

for certain Bombardier, Inc., Model BD– 

100–1A10 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–2022–0016. 

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–100–1A10 airplanes. The NPRM 

published in the Federal Register on 

January 27, 2022 (87 FR 4170). The 

NPRM was prompted by a report that 

the nose wheel SSV can be slow to 

deactivate under low temperature 

conditions. The NPRM proposed to 

require replacing the affected nose 

wheel SSV with a redesigned nose 

wheel SSV, and performing an 

operational test of the nose wheel SSV 

and nose wheel steering control system. 

The NPRM also proposed to prohibit the 

installation of a certain nose wheel SSV. 

The FAA is issuing this AD to address 

a slow nose wheel SSV deactivation, 

which, in combination with an uncommanded steering input, could lead 

to a delayed transition to free castor 

mode and result in an aircraft runway 

excursion. See the MCAI for additional 

background information. 

Comments 

The FAA gave the public the 

opportunity to participate in developing 

this final rule. The FAA received no 

comments on the NPRM or on the 

determination of the cost to the public. 

Conclusion 

The FAA reviewed the relevant data 

and determined that air safety and the 

public interest require adopting this 

final rule as proposed, except for minor 

editorial changes. The FAA has 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

addressing the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Related Service Information Under 1 

CFR Part 51 

Bombardier has issued Service 

Bulletin 100–32–35, dated March 30, 

2021; and Service Bulletin 350–32–011, 

dated March 30, 2021. This service 

information describes procedures for 

replacing the existing nose wheel SSV 

(part number 41130–107) with a 

redesigned nose wheel SSV (part 

number 41130–111), and performing an 

operational test of the nose wheel SSV 

and nose wheel steering control system. 

These documents are distinct since they 

apply to different airplane 

configurations. 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. 

Costs of Compliance 

The FAA estimates that this AD 

affects 660 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 

4 work-hours × $85 per hour = $340 .......................................................................................... $5,793 $6,133 $4,047,780 

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. 


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Federal Register / Vol. 87, No. 92 / Thursday, May 12, 2022 / Rules and Regulations 29027 

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: 

2022–09–02 Bombardier, Inc.: Amendment 

39–22022; Docket No. FAA–2022–0016; 

Project Identifier MCAI–2021–00945–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective June 16, 2022. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Bombardier, Inc., 

Model BD–100–1A10 airplanes, certificated 

in any category, serial numbers 20003 

through 20892 inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 32, Landing gear. 

(e) Unsafe Condition 

This AD was prompted by a report that the 

nose wheel steering selector valve (SSV) can 

be slow to deactivate under low temperature 

conditions. The FAA is issuing this AD to 

address a slow nose wheel SSV deactivation, 

which, in combination with an uncommanded steering input, could lead to a 

delayed transition to free castor mode and 

result in an aircraft runway excursion. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Replacement of Nose Wheel SSV 

Within 36 months after the effective date 

of this AD: Replace the nose wheel SSV part 

number 41130–107 with the redesigned nose 

wheel SSV part number 41130–111; and 

before further flight, perform an operational 

test of the nose wheel SSV and nose wheel 

steering control system; in accordance with 

paragraphs 2.B. and 2.C. of the 

Accomplishment Instructions of the 

applicable service information specified in 

paragraphs (g)(1) and (2) of this AD. If any 

test fails, do applicable corrective actions and 

repeat the test until the part passes the test. 

(1) Bombardier Service Bulletin 100–32– 

35, dated March 30, 2021. 

(2) Bombardier Service Bulletin 350–32– 

011, dated March 30, 2021. 

(h) Parts Installation Prohibition 

Do not install nose wheel SSV, part 

number 41130–107 on any airplane as of the 

applicable compliance time specified in 

paragraph (h)(1) or (2) of this AD. 

(1) For airplanes that have nose wheel SSV, 

part number 41130–107 installed as of the 

effective date of this AD: After replacement 

of nose wheel SSV as required by paragraph 

(g) of this AD. 

(2) For airplanes that, as of the effective 

date of this AD, do not have nose wheel SSV, 

part number 41130–107 installed: As of the 

effective date of this AD. 

(i) No Reporting Requirement 

Although the service information specified 

in paragraphs (g)(1) and (2) of this AD 

specifies to submit certain information to the 

manufacturer, this AD does not include that 

requirement. 

(j) 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 

York ACO Branch, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; telephone 

516–228–7300. 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 Bombardier, Inc.’s TCCA Design 

Approval Organization (DAO). If approved by 

the DAO, the approval must include the 

DAO-authorized signature. 

(k) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Transport 

Canada AD CF–2021–29, dated August 18, 

2021, 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– 

2022–0016. 

(2) For more information about this AD, 

contact Chirayu Gupta, Aerospace Engineer, 

Mechanical Systems and Administrative 

Services Section, FAA, New York ACO 

Branch, 1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; telephone 516–228– 

7300; email 9-avs-nyaco-cos@faa.gov. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) Bombardier Service Bulletin 100–32–35, 

dated March 30, 2021. 

(ii) Bombardier Service Bulletin 350–32– 

011, dated March 30, 2021. 

(3) For service information identified in 

this AD, contact Bombardier Business 

Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–2999; email 

ac.yul@aero.bombardier.com; internet http:// 

www.bombardier.com. 

(4) 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. 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

email fr.inspection@nara.gov, or go to: 

https://www.archives.gov/federal-register/cfr/ 

ibr-locations.html. 

Issued on April 11, 2022. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–10139 Filed 5–11–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0466; Project 

Identifier MCAI–2021–00572–T; Amendment 

39–22025; AD 2022–09–05] 

RIN 2120–AA64 

Airworthiness Directives; Embraer S.A. 

(Type Certificate Previously Held by 

Yabora ̃ Indu ́ stria Aerona ́utica S.A.) 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Embraer S.A. Model ERJ 190–300, and 

–400 airplanes. This AD was prompted 

by a report of premature failures of the 

alternating current motor pump (ACMP) 

3A at hydraulic system #3 due to 

excessive wear of the ACMP tail 

bearing. This AD requires repetitive 

replacement of the hydraulic system 

ACMP 3A having a certain part number 

with a serviceable part, as specified in 

an Ageˆncia Nacional de Aviac ̧a ̃o Civil 


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