Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 32295 

(i) European Union Aviation Safety Agency 

(EASA) AD 2021–0190, dated August 17, 

2021. 

(ii) [Reserved] 

(3) For EASA AD 2021–0190, contact 

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 

EASA AD on the EASA website at https://

ad.easa.europa.eu. 

(4) 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. 

(5) You may view this material 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/ibrlocations.html. 

Issued on May 13, 2022. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2022–11538 Filed 5–27–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0787; Project 

Identifier MCAI–2021–00252–T; Amendment 

39–22048; AD 2022–10–10] 

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 CL–600–1A11 

(600), CL–600–2A12 (601), and CL–600– 

2B16 (601–3A, 601–3R, and 604 

Variants) airplanes. This AD was 

prompted by a report of a wing stall 

(wing drop/un-commanded roll) during 

a landing flare. This AD requires 

revising the existing airplane flight 

manual (AFM) to incorporate a 

limitation and procedure for the wing 

anti-ice (WAI) system in order to 

mitigate the risk of ice accumulation on 

the wing leading edges. The FAA is 

issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective July 5, 2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of July 5, 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 https:// 

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 

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–2021–0787. 

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–2021– 

0787; 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. 

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: 

Background 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued TCCA AD CF– 

2021–06, dated February 26, 2021 

(TCCA AD CF–2021–06) (also referred 

to after this as the Mandatory 

Continuing Airworthiness Information, 

or the MCAI), to correct an unsafe 

condition for certain Bombardier, Inc., 

Model CL–600–1A11 (600), CL–600– 

2A12 (601), and CL–600–2B16 (601–3A, 

601–3R, and 604 Variants) airplanes. 

You may examine the MCAI in the AD 

docket at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2021–0787. 

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 

CL–600–1A11 (600), CL–600–2A12 

(601), and CL–600–2B16 (601–3A, 601– 

3R, and 604 Variants) airplanes. The 

NPRM published in the Federal 

Register on September 15, 2021 (86 FR 

51279). The NPRM was prompted by a 

report of a wing stall (wing drop/uncommanded roll) during a landing flare. 

The NPRM proposed to require revising 

the existing AFM to incorporate a 

limitation and procedure for the WAI 

system in order to mitigate the risk of 

ice accumulation on the wing leading 

edges. The FAA is issuing this AD to 

address ice accumulation on the wing 

leading edges, which could result in a 

wing stall during landing and 

consequent reduced controllability of 

the airplane. 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 the following 

service information, which specifies a 

revised AFM limitation and procedure 

for the WAI system in order to mitigate 

the risk of ice accumulation on the wing 

leading edge. These documents are 

distinct since they apply to different 

airplane configurations. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section of the Canadair 

Challenger AFM, Product Publication 

No. 600, Revision A114, dated April 16, 

2020. 

• Sub-section C., Icing Conditions 

During Flight, of Chapter 3., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

Canadair Challenger AFM, Product 

Publication No. 600, Revision A114, 

dated April 16, 2020. 


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32296 Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 

• Sub-section I., Before Landing, of 

Chapter 42., CONSOLIDATED CHECK 

LIST, of the NORMAL PROCEDURES 

section, of the Canadair Challenger 

AFM, Product Publication No. 600, 

Revision A114, dated April 16, 2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 4., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the Canadair 

Challenger AFM, Product Support 

Publication (PSP) No. 600–1, Revision 

106, dated April 16, 2020. 

• Sub-section C., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

Canadair Challenger AFM, Product 

Support Publication (PSP) No. 600–1, 

Revision 106, dated April 16, 2020. 

• Sub-section I., Before Landing, of 

Chapter 23., CONSOLIDATED CHECK 

LIST, of the NORMAL PROCEDURES 

section, of the Canadair Challenger 

AFM, Product Support Publication 

(PSP) No. 600–1, Revision 106, dated 

April 16, 2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the Canadair 

Challenger AFM, PSP No. 601–1A, 

Revision 123, dated April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Canadair Challenger AFM, PSP No. 

601–1A, Revision 123, dated April 16, 

2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601–1A–1, Revision 82, dated 

April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601–1A–1, Revision 82, dated 

April 16, 2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the Canadair 

Challenger AFM, PSP No. 601–1B, 

Revision 86, dated April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Canadair Challenger AFM, PSP No. 

601–1B, Revision 86, dated April 16, 

2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601–1B–1, Revision 84, dated 

April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601–1B–1, Revision 84, dated 

April 16, 2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the Canadair 

Challenger AFM, PSP No. 601A–1, 

Revision 106, dated April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Canadair Challenger AFM, PSP No. 

601A–1, Revision 106, dated April 16, 

2020. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601A–1–1, Revision 95, dated 

April 16, 2020. 

• Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

NORMAL PROCEDURES section, of the 

Bombardier Canadair Challenger AFM, 

PSP No. 601A–1–1, Revision 95, dated 

April 16, 2020. 

• Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in 

Icing Conditions, of Section 02–04, 

Operating Limitations, of Chapter 2— 

LIMITATIONS, of the Bombardier 

Challenger 604 AFM, Publication No. 

PSP 604–1, Revision 116, dated 

December 18, 2019. (For obtaining the 

limitation and procedure for the 

Bombardier Challenger 604 AFM, 

Publication No. PSP 604–1, use 

Document Identification No. CH 604 

AFM.) 

• Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and 

Rain Protection, of Chapter 4— 

NORMAL PROCEDURES, of the 

Bombardier Challenger 604 AFM, 

Publication No. PSP 604–1, Revision 

116, dated December 18, 2019. (For 

obtaining the limitation and procedure 

for the Bombardier Challenger 604 

AFM, Publication No. PSP 604–1, use 

Document Identification No. CH 604 

AFM.) 

• Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in 

Icing Conditions, of Section 02–04, 

Operating Limitations, of Chapter 2— 

LIMITATIONS, of the Bombardier 

Challenger 605 AFM, Publication No. 

PSP 605–1, Revision 54, dated 

December 18, 2019. (For obtaining the 

limitation and procedure for the 

Bombardier Challenger 605 AFM, 

Publication No. PSP 605–1, use 

Document Identification No. CH 605 

AFM.) 

• Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and 

Rain Protection, of Chapter 4— 

NORMAL PROCEDURES, of the 

Bombardier Challenger 605 AFM, 

Publication No. PSP 605–1, Revision 54, 

dated December 18, 2019. (For obtaining 

the limitation and procedure for the 

Bombardier Challenger 605 AFM, 

Publication No. PSP 605–1, use 

Document Identification No. CH 605 

AFM.) 

• Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in 

Icing Conditions, of Section 02–04, 

Operating Limitations, of Chapter 2— 

LIMITATIONS, of the Bombardier 

Challenger 650 AFM, Publication No. 

PSP 650–1, Revision 19, dated 

December 18, 2019. (For obtaining the 

limitation and procedure for the 

Bombardier Challenger 650 AFM, 

Publication No. PSP 650–1, use 

Document Identification No. CH 650 

AFM.) 

• Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and 

Rain Protection, of Chapter 4— 

NORMAL PROCEDURES, of the 

Bombardier Challenger 650 AFM, 

Publication No. PSP 650–1, Revision 19, 

dated December 18, 2019. (For obtaining 

the limitation and procedure for the 

Bombardier Challenger 650 AFM, 

Publication No. PSP 650–1, use 

Document Identification No. CH 650 

AFM.) 

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 619 airplanes of U.S. registry. 

The FAA estimates the following costs 

to comply with this AD: 


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ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

1 work-hour × $85 per hour = $85 .............................................................................................. $0 $85 $52,615 

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. 

Adoption of 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: 

2022–10–10 Bombardier, Inc.: Amendment 

39–22048; Docket No. FAA–2021–0787; 

Project Identifier MCAI–2021–00252–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective July 5, 2022. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Bombardier, Inc., 

airplanes, certificated in any category, as 

identified in paragraphs (c)(1) through (3) of 

this AD. 

(1) Model CL–600–1A11 (600) airplanes 

having serial numbers (S/Ns) 1001 through 

1085 inclusive. 

(2) Model CL–600–2A12 (601) airplanes 

having S/Ns 3001 through 3066 inclusive. 

(3) Model CL–600–2B16 (601–3A, 601–3R, 

and 604 Variants) airplanes having S/Ns 5001 

through 5194 inclusive; 5301 through 5665 

inclusive; 5701 through 5988 inclusive; and 

6050 through 6153 inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 30, Ice and Rain Protection. 

(e) Unsafe Condition 

This AD was prompted by a report of a 

wing stall during a landing flare. Photographs 

after landing showed that the airplane had 

mixed ice on the leading edges of the wings; 

therefore, it was determined that during 

descent the wing anti-ice (WAI) system had 

been OFF because the ice detector did not 

detect ice. The FAA is issuing this AD to 

address ice accumulation on the wing 

leading edges, which could result in a wing 

stall during landing and consequent reduced 

controllability of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Airplane Flight Manual (AFM) Revision 

Within 60 days after the effective date of 

this AD: Revise the existing AFM to 

incorporate the specified sections of the 

Bombardier or Canadair Challenger AFM 

revision limitations and procedures for the 

WAI system specified in figure 1 to 

paragraph (g) of this AD. 

BILLING CODE 4910–13–P 


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Figure 1 to paragraph (g) -AFM Revisions 

Bombardier 

Airplane New Limitation/Procedure AFM AFM Revision 

Model/Serial and Issue Date 

Number 

CL-600-lAl 1 Sub-sub section (2), Wing Canadair Revision Al 14, 

(Variant 600), Anti-ice System, of sub- Challenger AFM, dated April 16, 

1001 through 1085 section I., Operation in Icing Product 2020 

inclusive for Conditions, of Chapter 3., Publication No. 

non-winglets OPERATING 600 

LIMITATIONS, of the 

LIMITATIONS section; and 

sub-section C., Icing 

Conditions During Flight, of 

Chapter 3., SYSTEMS 

OPERATIONS-ANTI-ICE, 

and sub-section I., Before 

Landing, of Chapter 42., 

CONSOLIDATED CHECK 

LIST, of the NORMAL 

PROCEDURES section 

CL-600-lAl 1 Sub-sub section (2), Wing Canadair Revision 106, 

(Variant 600), Anti-ice System, of sub- Challenger AFM, dated April 16, 

1001 through 1085 section I., Operation in Icing Product Support 2020 

inclusive for Conditions, of Chapter 4., Publication (PSP) 

winglets OPERATING No. 600-1 

LIMITATIONS, of the 

LIMITATIONS section; subsection C., Icing Conditions 

During Flight, of Chapter 4., 

SYSTEMS OPERATIONS -

ANTI-ICE, and sub-section 

I., Before Landing, of 

Chapter 23., 

CONSOLIDATED CHECK 

LIST, of the NORMAL 

PROCEDURES section 
Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 32299 


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Bombardier 

Airplane New Limitation/Procedure AFM AFM Revision 

Model/Serial and Issue Date 

Number 

CL-600-2A12 Sub-sub section (2), Wing Canadair Revision 123, 

(Variant 601), Anti-ice System, of sub- Challenger AFM, dated April 16, 

3001 through section I., Operation in Icing PSP No. 601-lA 2020 

3066, and 43,100 Conditions, of Chapter 3., 

lb. maximum take- OPERATING 

off weight LIMITATIONS, of the 

(MTOW) LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 

CL-600-2A12 Sub-sub section (2), Wing Bombardier Revision 82, 

(Variant 601 ), Anti-ice System, of sub- Canadair dated April 16, 

3001 through section I., Operation in Icing Challenger AFM, 2020 

3066, and 44,600 Conditions, of Chapter 3., PSP No. 601-lA-1 

lb./45,100 lb. OPERATING 

MTOW LIMITATIONS, of the 

LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 

CL-600-2A12 Sub-sub section (2), Wing Canadair Revision 86, 

(Variant 601), Anti-ice System, of sub- Challenger AFM, dated April 16, 

3001 through 3066 section I., Operation in Icing PSP No. 601-lB 2020 

with -3A engine, Conditions, of Chapter 3., 

and 43,100 lb. OPERATING 

MTOW LIMITATIONS, of the 

LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 
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Bombardier 

Airplane New Limitation/Procedure AFM AFM Revision 

Model/Serial and Issue Date 

Number 

CL-600-2A12 Sub-sub section (2), Wing Bombardier Revision 84, 

(Variant 601), Anti-ice System, of sub- Canadair dated April 16, 

3001 through 3066 section I., Operation in Icing Challenger AFM, 2020 

with -3A engine, Conditions, of Chapter 3., PSP No. 601-lB-1 

and 44,600 OPERATING 

lb./45,100 lb. LIMITATIONS, of the 

MTOW LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 

CL-600-2B16 Sub-sub section (2), Wing Canadair Revision 106, 

(Variant 601-3A/3 Anti-ice System, of sub- Challenger AFM, dated April 16, 

R) 5001 through section I., Operation in Icing PSP No. 601A-1 2020 

5134 inclusive, Conditions, of Chapter 3., 

and 43,100 lb. OPERATING 

MTOW LIMITATIONS, of the 

LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 

CL-600-2B16 Sub-sub section (2), Wing Bombardier Revision 95, 

(Variant 601- Anti-ice System, of sub- Canadair dated April 16, 

3A/3R) 5001 section I., Operation in Icing Challenger AFM, 2020 

through 5194 Conditions, of Chapter 3., PSP No. 601A-1-1 

inclusive, and OPERATING 

44,600 lb./45,100 LIMITATIONS, of the 

lb.MTOW LIMITATIONS section; and 

sub-section E., Icing 

Conditions During Flight, of 

Chapter 4., SYSTEMS 

OPERATIONS-ANTI-ICE, 

of the NORMAL 

PROCEDURES section 
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BILLING CODE 4910–13–C (h) 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 


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Bombardier 

Airplane New Limitation/Procedure AFM AFM Revision 

Model/Serial and Issue Date 

Number 

CL-600-2B16 Sub-sub section B., Wing Bombardier Revision 116, 

(Variant 604) Anti-ice System, of sub- Challenger 604 dated 

5301 through 5665 section 4., Operation in Icing AFM,PSPNo. December 18, 

inclusive Conditions, of Section 02-04, 604-1 1 2019 

Operating Limitations, of 

Chapter 2-LIMITATIONS; 

and sub-section M., Icing 

Conditions During Flight, of 

Section 04-14, Ice and Rain 

Protection, of Chapter 4 -

NORMAL PROCEDURES 

CL-600-2B16 Sub-sub section B., Wing Bombardier Revision 54, 

(Variant 604) Anti-ice System, of sub- Challenger 605 dated 

5701 through 5988 section 4., Operation in Icing AFM,PSPNo. December 18, 

inclusive Conditions, of Section 02-04, 605-12 2019 

Operating Limitations, of 

Chapter 2-LIMITATIONS; 

and sub-section M., Icing 

Conditions During Flight, of 

Section 04-14, Ice and Rain 

Protection, of Chapter 4 -

NORMAL PROCEDURES 

CL-600-2B16 Sub-sub section B., Wing Bombardier Revision 19, 

(Variant 604) Anti-ice System, of sub- Challenger 650 dated 

6050 through 6153 section 4., Operation in Icing AFM,PSPNo. December 18, 

inclusive Conditions, of Section 02-04, 650-1 3 2019 

Operating Limitations, of 

Chapter 2-LIMITATIONS; 

and sub-section M., Icing 

Conditions During Flight, of 

Section 04-14, Ice and Rain 

Protection, of Chapter 4 -

NORMAL PROCEDURES 

1 For obtaining the limitation and procedure for the Bombardier Challenger 604 AFM, 

Publication No. PSP 604-1, use Document Identification No. CH 604 AFM. 

2 For obtaining the limitation and procedure for the Bombardier Challenger 605 AFM, 

Publication No. PSP 605-1, use Document Identification No. CH 605 AFM. 

3 For obtaining the limitation and procedure for the Bombardier Challenger 650 AFM, 

Publication No. PSP 650-1, use Document Identification No. CH 650 AFM. 
32302 Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 

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; 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 Bombardier, Inc.’s TCCA Design 

Approval Organization (DAO). If approved by 

the DAO, the approval must include the 

DAO-authorized signature. 

(i) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) TCCA AD 

CF–2021–06, dated February 26, 2021, for 

related information. This MCAI may be 

found in the AD docket at https:// 

www.regulations.gov by searching for and 

locating Docket No. FAA–2021–07871. 

(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. 

(j) 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) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Canadair Challenger Airplane Flight 

Manual (AFM), Product Publication No. 600, 

Revision A114, dated April 16, 2020. 

(ii) Sub-section C., Icing Conditions During 

Flight, of Chapter 3., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Canadair 

Challenger AFM, Product Publication No. 

600, Revision A114, dated April 16, 2020. 

(iii) Sub-section I., Before Landing, of 

Chapter 42., CONSOLIDATED CHECK LIST, 

of the NORMAL PROCEDURES section, of 

the Canadair Challenger AFM, Product 

Publication No. 600, Revision A114, dated 

April 16, 2020. 

(iv) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 4., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Canadair Challenger AFM, Product 

Support Publication (PSP) No. 600–1, 

Revision 106, dated April 16, 2020. 

(v) Sub-section C., Icing Conditions During 

Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Canadair 

Challenger AFM, PSP No. 600–1, Revision 

106, dated April 16, 2020. 

(vi) Sub-section I., Before Landing, of 

Chapter 23., CONSOLIDATED CHECK LIST, 

of the NORMAL PROCEDURES section, of 

the Canadair Challenger AFM, PSP No. 600– 

1, Revision 106, dated April 16, 2020. 

(vii) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Canadair Challenger AFM, PSP No. 

601–1A, Revision 123, dated April 16, 2020. 

(viii) Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Canadair 

Challenger AFM, PSP No. 601–1A, Revision 

123, dated April 16, 2020. 

(ix) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Bombardier Canadair Challenger AFM, 

PSP No. 601–1A–1, Revision 82, dated April 

16, 2020. 

Note 1 to paragraph (j)(2)(ix): The List of 

Effective Pages contains a page date error for 

page i of the LIMITATIONS Contents. The 

page date identified is in the List of Effective 

Pages is October 26, 2009; the date specified 

on page i is April 16, 2020. 

(x) Sub-section E., Icing Conditions During 

Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Bombardier 

Canadair Challenger AFM, PSP No. 601–1A– 

1, Revision 82, dated April 16, 2020. 

(xi) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Canadair Challenger AFM, PSP No. 

601–1B, Revision 86, dated April 16, 2020. 

(xii) Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Canadair 

Challenger AFM, PSP No. 601–1B, Revision 

86, dated April 16, 2020. 

(xiii) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Bombardier Canadair Challenger AFM, 

PSP No. 601–1B–1, Revision 84, dated April 

16, 2020. 

(xiv) Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Bombardier 

Canadair Challenger AFM, PSP No. 601–1B– 

1, Revision 84, dated April 16, 2020. 

(xv) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Canadair Challenger AFM, PSP No. 

601A–1, Revision 106, dated April 16, 2020. 

(xvi) Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Canadair 

Challenger AFM, PSP No. 601A–1, Revision 

106, dated April 16, 2020. 

(xvii) Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in Icing 

Conditions, of Chapter 3., OPERATING 

LIMITATIONS, of the LIMITATIONS section, 

of the Bombardier Canadair Challenger AFM, 

PSP No. 601A–1–1, Revision 95, dated April 

16, 2020. 

(xviii) Sub-section E., Icing Conditions 

During Flight, of Chapter 4., SYSTEMS 

OPERATIONS—ANTI-ICE, of the NORMAL 

PROCEDURES section, of the Bombardier 

Canadair Challenger AFM, PSP No. 601A–1– 

1, Revision 95, dated April 16, 2020. 

(xix) Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in Icing 

Conditions, of Section 02–04, Operating 

Limitations, of Chapter 2—LIMITATIONS, of 

the Bombardier Challenger 604 AFM, 

Publication No. PSP 604–1, Revision 116, 

dated December 18, 2019. 

Note 2 to paragraph (j)(2)(xix): For 

obtaining the limitation and procedure 

specified in paragraphs (j)(2)(xix) and (xx) of 

this AD for the Bombardier Challenger 604 

AFM, Publication No. PSP 604–1, use 

Document Identification No. CH 604 AFM. 

(xx) Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and Rain 

Protection, of Chapter 4—NORMAL 

PROCEDURES, of the Bombardier Challenger 

604 AFM, Publication No. PSP 604–1, 

Revision 116, dated December 18, 2019. 

(xxi) Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in Icing 

Conditions, of Section 02–04, Operating 

Limitations, of Chapter 2—LIMITATIONS, of 

the Bombardier Challenger 605 AFM, 

Publication No. PSP 605–1, Revision 54, 

dated December 18, 2019. 

Note 3 to paragraph (j)(2)(xxi): For 

obtaining the limitation and procedure 

specified in paragraphs (j)(2)(xxi) and (xxii) 

of this AD for the Bombardier Challenger 605 

AFM, Publication No. PSP 605–1, use 

Document Identification No. CH 605 AFM. 

(xxii) Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and Rain 

Protection, of Chapter 4—NORMAL 

PROCEDURES, of the Bombardier Challenger 

605 AFM, Publication No. PSP 605–1, 

Revision 54, dated December 18, 2019. 

(xxiii) Sub-sub section B., Wing Anti-ice 

System, of sub-section 4., Operation in Icing 

Conditions, of Section 02–04, Operating 

Limitations, of Chapter 2—LIMITATIONS, of 

the Bombardier Challenger 650 AFM, 

Publication No. PSP 650–1, Revision 19, 

dated December 18, 2019. 

Note 4 to paragraph (j)(2)(xxiii): For 

obtaining the limitation and procedure 

specified in paragraphs (j)(2)(xxiii) and (xxiv) 

of this AD for the Bombardier Challenger 650 

AFM, Publication No. PSP 650–1, use 

Document Identification No. CH 650 AFM. 

(xxiv) Sub-section M., Icing Conditions 

During Flight, of Section 04–14, Ice and Rain 

Protection, of Chapter 4—NORMAL 

PROCEDURES, of the Bombardier Challenger 

650 AFM, Publication No. PSP 650–1, 

Revision 19, dated December 18, 2019. 

(3) For service information identified in 

this AD, contact Bombardier Business 

Aircraft Customer Response Center, 400 CoˆteVerDate Sep<11>2014 16:00 May 27, 2022 Jkt 256001 PO 00000 Frm 00014 Fmt 4700 Sfmt 4700 E:\FR\FM\31MYR1.SGM 31MYR1

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Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 32303 

Vertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–2999; email 

ac.yul@aero.bombardier.com; internet 

https://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 May 6, 2022. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2022–11531 Filed 5–27–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE TREASURY 

Office of Foreign Assets Control 

31 CFR Part 587 

Publication of Financial Services 

Sectoral Determination and Directives 

1A, 2, 3, and 4 Under Executive Order 

14024 of April 15, 2021 

AGENCY: Office of Foreign Assets 

Control, Treasury. 

ACTION: Publication of one 

determination and four directives. 

SUMMARY: The Department of the 

Treasury’s Office of Foreign Assets 

Control (OFAC) is publishing a sectoral 

determination by the Secretary of the 

Treasury, in consultation with the 

Secretary of State, and four Russian 

Harmful Foreign Activities Sanctions 

directives in the Federal Register. The 

determination and four directives, all 

issued pursuant to an April 15, 2021 

Executive Order, were previously issued 

on OFAC’s website. 

DATES: The Determination Pursuant to 

Section 1(a)(i) of Executive Order 14024 

was issued on February 22, 2022 and 

took effect immediately. Directive 1A 

under Executive Order (E.O.) 14024, 

‘‘Prohibitions Related to Certain 

Sovereign Debt of the Russian 

Federation,’’ was issued on February 22, 

2022, and the prohibitions therein took 

effect on March 1, 2022. Directive 2 

under E.O. 14024, ‘‘Prohibitions Related 

to Correspondent or Payable-Through 

Accounts and Processing of 

Transactions Involving Certain Foreign 

Financial Institutions,’’ was issued on 

February 24, 2022, and the prohibitions 

therein took effect on March 26, 2022. 

Directive 3 under E.O. 14024, 

‘‘Prohibitions Related to New Debt and 

Equity of Certain Russia-related 

Entities,’’ was issued on February 24, 

2022 and the prohibitions therein took 

effect on March 26, 2022. Directive 4, 

‘‘Prohibitions Related to Transactions 

Involving the Central Bank of the 

Russian Federation, the National Wealth 

Fund of the Russian Federation, and the 

Ministry of Finance of the Russian 

Federation,’’ was issued on February 28, 

2022 and took effect immediately. 

FOR FURTHER INFORMATION CONTACT: 

OFAC: Assistant Director for Licensing, 

202–622–2480; Assistant Director for 

Regulatory Affairs, 202–622–4855; or 

Assistant Director for Sanctions 

Compliance & Evaluation, 202–622– 

2490. 

SUPPLEMENTARY INFORMATION: 

Electronic Availability 

This document and additional 

information concerning OFAC are 

available on OFAC’s website: 

www.treas.gov/ofac. 

Background 

On April 15, 2021, the President, 

invoking the authority of, inter alia, the 

International Emergency Economic 

Powers Act (50 U.S.C. 1701 et seq.), 

issued Executive Order (E.O.) 14024 (86 

FR 20249, April 19, 2021). 

In E.O. 14024, the President found 

that specified harmful foreign activities 

of the Government of the Russian 

Federation—in particular, efforts to 

undermine the conduct of free and fair 

democratic elections and democratic 

institutions in the United States and its 

allies and partners; to engage in and 

facilitate malicious cyber-enabled 

activities against the United States and 

its allies and partners; to foster and use 

transnational corruption to influence 

foreign governments; to pursue 

extraterritorial activities targeting 

dissidents or journalists; to undermine 

security in countries and regions 

important to United States national 

security; and to violate well-established 

principles of international law, 

including respect for the territorial 

integrity of states—constitute an 

unusual and extraordinary threat to the 

national security, foreign policy, and 

economy of the United States and 

declared a national emergency to deal 

with that threat. 

Among other things, section 1 of E.O. 

14024 blocks all property and interests 

in property that are in the United States, 

that hereafter come within the United 

States, or that are or hereafter come 

within the possession or control of any 

United States person of any person 

determined by the Secretary of the 

Treasury, in consultation with the 

Secretary of State, to operate or have 

operated in the technology sector or the 

defense and related materiel sector of 

the Russian Federation economy, or any 

other sector of the Russian Federation 

economy as may be determined by the 

Secretary of the Treasury, in 

consultation with the Secretary of State. 

On February 22, 2022, the Secretary of 

the Treasury, in consultation with the 

Secretary of State, determined that 

section 1(a)(i) of E.O. 14024 shall apply 

to the financial services sector of the 

Russian Federation economy (‘‘February 

22, 2022 Determination Pursuant to 

Section 1(a)(i) of Executive Order 

14024’’). Pursuant to this determination, 

any person that the Secretary of 

Treasury, in consultation with the 

Secretary of State, or the Secretary of 

State, in consultation with the Secretary 

of the Treasury (or their respective 

designees), subsequently determines 

operates or has operated in the financial 

services sector of the Russian Federation 

economy shall be subject to the 

prohibitions described in section 1(a)(i) 

of E.O. 14024. 

On February 22, 2022, the Director of 

OFAC issued Directive 1A under E.O. 

14024, ‘‘Prohibitions Related to Certain 

Sovereign Debt of the Russian 

Federation’’ (Russia-related Sovereign 

Debt Directive), replacing and 

superseding Directive 1 under E.O. 

14024 of April 15, 2021 (86 FR 35867, 

July 7, 2021), to extend existing 

sovereign debt prohibitions to cover 

participation in the secondary market 

for bonds issued after March 1, 2022 by 

the Central Bank of the Russian 

Federation, the National Wealth Fund of 

the Russian Federation, or the Ministry 

of Finance of the Russian Federation, 

effective March 1, 2022. 

On February 24, 2022, the Director of 

OFAC issued Directive 2 under E.O. 

14024, ‘‘Prohibitions Related to 

Correspondent or Payable-Through 

Accounts and Processing of 

Transactions Involving Certain Foreign 

Financial Institutions’’ (Russia-related 

CAPTA Directive), which prohibits U.S. 

financial institutions from: (i) The 

opening or maintaining of a 

correspondent account or payablethrough account for or on behalf of 

foreign financial institutions determined 

to be subject to the prohibitions of the 

Russia-related CAPTA Directive; and (ii) 

the processing of transactions involving 

foreign financial institutions determined 

to be subject to the prohibitions of the 

Russia-related CAPTA Directive. The 

effective date of these prohibitions with 


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