Federal Register / Vol. 87, No. 29 / Friday, February 11, 2022 / Rules and Regulations 7931 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0725; Project 

Identifier MCAI–2020–01402–T; Amendment 

39–21882; AD 2021–26–23] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc., Airplanes; Correction 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that was 

published in the Federal Register. That 

AD applies to certain Bombardier, Inc., 

Model CL–600–2B16 (601–3A, 601–3R, 

and 604 Variants) airplanes. As 

published, the AD number specified in 

the regulatory text is incorrect. This 

document corrects that error and one 

other minor error. In all other respects, 

the original document remains the 

same. 

DATES: This correction is effective 

February 25, 2022. The effective date of 

AD 2021–26–23 remains February 25, 

2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of February 25, 2022 (87 FR 3184, 

January 21, 2022). 

The Director of the Federal Register 

approved the incorporation by reference 

of certain other publications listed in 

this AD as of November 30, 2017 (82 FR 

49498, October 26, 2017). 

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 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 at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2021– 

0725. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0725; 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: 

Steven Dzierzynski, Aerospace 

Engineer, Avionics and Electrical 

Systems Section, FAA, New York ACO 

Branch, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; telephone 

516–228–7367; fax 516–794–5531; email 

9-avs-nyaco-cos@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

AD 2021–26–23, Amendment 39– 

21882 (87 FR 3184, January 21, 2022) 

(AD 2021–26–23), requires repetitive 

inspections for fuel leakage at the 

engine and auxiliary power unit (APU) 

fuel pumps, related investigative and 

corrective actions if necessary, an 

inspection of the APU for damage and 

deformation, repair if necessary, and 

modification of the engine electrical fuel 

pump (EFP) installation. The AD 

applies to certain Bombardier, Inc., 

Model CL–600–2B16 (601–3A, 601–3R, 

and 604 Variants) airplanes. 

Need for the Correction 

As published, the regulatory text of 

AD 2021–26–23 included the following 

errors: 

• The AD number was incorrectly 

identified as ‘‘2021–21–23.’’ The correct 

AD number is 2021–26–23. 

• The last sentence of paragraph (g) 

requires use of certain service 

information ‘‘as the effective date of this 

AD.’’ The correct compliance time for 

that requirement is ‘‘as of the effective 

date of this AD.’’ 

Related Service Information Under 1 

CFR Part 51 

Bombardier has issued the following 

service information, which describes 

procedures for repetitive general visual 

inspections and rectifications for any 

fuel leak from the engine and APU EFP 

electrical wiring conduit outlets. These 

documents are distinct since they apply 

to different airplane serial numbers. 

• Bombardier Service Bulletin 604– 

28–022, Revision 3, dated August 31, 

2018. 

• Bombardier Service Bulletin 605– 

28–010, Revision 3, dated August 31, 

2018. 

• Bombardier Service Bulletin 650– 

28–001, Revision 3, dated January 3, 

2019. 

Bombardier has also issued the 

following service information, which 

describes procedures for a detailed 

visual inspection of the APU for any 

damage or deformations (e.g., cut wires 

and a broken harness assembly of the 

fuel boost pump connector), 

modification of the engine EFP 

installation, and repair if necessary. 

These documents are distinct since they 

apply to different airplane serial 

numbers. 

• Bombardier Service Bulletin 604– 

28–024, Revision 01, dated May 28, 

2021. 

• Bombardier Service Bulletin 605– 

28–012, dated June 16, 2020. 

• Bombardier Service Bulletin 650– 

28–002, dated June 16, 2020. 

This AD also requires Bombardier 

Service Bulletin 604–28–022, dated 

October 19, 2015, and Bombardier 

Service Bulletin 605–28–010, dated 

October 19, 2015, which the Director of 

the Federal Register approved for 

incorporation by reference as of 

November 30, 2017 (82 FR 49498, 

October 26, 2017). 

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. 

Correction of Publication 

This document corrects two errors in 

the regulatory text and correctly adds 

the AD as an amendment to 14 CFR 

39.13. Although no other part of the 

preamble or regulatory information has 

been corrected, the FAA is publishing 

the entire rule in the Federal Register. 

The effective date of this AD remains 

February 25, 2022. 

Since this action only corrects the AD 

number and a minor grammatical error 

in the regulatory text, it has no adverse 

economic impact and imposes no 

additional burden on any person. 

Therefore, the FAA has determined that 

notice and public procedures are 

unnecessary. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, the Federal Aviation 

Administration amends part 39 of the 

Federal Aviation Regulations (14 CFR 

part 39) as follows: 


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7932 Federal Register / Vol. 87, No. 29 / Friday, February 11, 2022 / Rules and Regulations 

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 [Corrected] 

■ 2. The FAA amends § 39.13 by: 

■ a. Removing Airworthiness Directive 

(AD) 2017–22–06, Amendment 39– 

19086 (82 FR 49498, October 26, 2017); 

and 

■ b. Adding the following new AD: 

2021–26–23 Bombardier, Inc.: Amendment 

39–21882; Docket No. FAA–2021–0725; 

Project Identifier MCAI–2020–01402–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective February 25, 2022. 

(b) Affected ADs 

This AD replaces AD 2017–22–06, 

Amendment 39–19086 (82 FR 49498, October 

26, 2017) (AD 2017–22–06). 

(c) Applicability 

This AD applies to Bombardier, Inc., 

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

604 Variants) airplanes, certificated in any 

category, serial numbers 5301 through 5665 

inclusive, 5701 through 5990 inclusive, and 

6050 through 6163 inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 28, Fuel. 

(e) Reason 

This AD was prompted by reports of fuel 

leaks from the electrical connectors and 

conduits of the engine and auxiliary power 

unit (APU) electrical fuel pump (EFP) 

cartridge/canister, and the development of 

additional actions to address the root cause 

of the fuel leaks. The FAA is issuing this AD 

to address the potential for a fire hazard as 

a result of fuel leak from the APU EFP 

electrical conduit in the hot landing light 

compartment. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Actions for Certain Airplanes, 

With Revised Service Information and 

Method of Compliance Provisions 

This paragraph restates the requirements of 

paragraph (g) of AD 2017–22–06, with 

revised service information and method of 

compliance provisions. For Model CL–600– 

2B16 airplanes having serial numbers 5301 

through 5665 inclusive: Within 600 flight 

hours or 12 months, whichever occurs first 

after November 30, 2017 (the effective date of 

AD 2017–22–06), do the inspections 

specified in paragraphs (g)(1) through (3) of 

this AD, and do all applicable corrective 

actions, in accordance with the 

Accomplishment Instructions of Bombardier 

Service Bulletin 604–28–022, dated October 

19, 2015, or Bombardier Service Bulletin 

604–28–022, Revision 3, dated August 31, 

2018. Do all applicable corrective actions 

before further flight. Repeat the inspections 

at intervals not to exceed 600 flight hours or 

12 months, whichever occurs first. As of the 

effective date of this AD, use Bombardier 

Service Bulletin 604–28–022, Revision 3, 

dated August 31, 2018, only. 

(1) Do a general visual inspection for traces 

of fuel coming from the right-hand engine 

boost pump at the location of the belly fairing 

screw (FS412, BL 0.0). 

(2) Do a general visual inspection for traces 

of fuel coming from the left-hand engine 

boost pump at the location of the belly fairing 

screw (FS412, BL 0.0). 

(3) Do a general visual inspection for traces 

of fuel coming from the EFP electrical wiring 

conduit outlet at the lower body fairing area 

for engine EFPs and at the right-hand landing 

light compartment for the APU EFP. 

(h) Retained Actions for Certain Other 

Airplanes, With Revised Service Information 

and Compliance Method Provisions 

This paragraph restates the requirements of 

paragraph (h) of AD 2017–22–06, with 

revised service information and compliance 

method provisions. For Model CL–600–2B16 

airplanes having serial numbers 5701 

through 5955 inclusive, 5957, 5960 through 

5966 inclusive, 5968 through 5971 inclusive, 

and 5981: Within 600 flight hours or 12 

months, whichever occurs first after 

November 30, 2017 (the effective date of AD 

2017–22–06), do the inspections specified in 

paragraphs (h)(1) through (3) of this AD, and 

do all applicable related investigative and 

corrective actions, in accordance with the 

Accomplishment Instructions in Bombardier 

Service Bulletin 605–28–010, dated October 

19, 2015, or Bombardier Service Bulletin 

605–28–010, Revision 3, dated August 31, 

2018. Do all applicable related investigative 

and corrective actions before further flight. 

Repeat the inspections at intervals not to 

exceed 600 flight hours or 12 months, 

whichever occurs first. As of the effective 

date of this AD, use Bombardier Service 

Bulletin 605–28–010, Revision 3, dated 

August 31, 2018, only. 

(1) Do a general visual inspection for traces 

of fuel coming from the right-hand engine 

boost pump at the location of the belly fairing 

screw (FS412, BL 0.0). 

(2) Do a general visual inspection for traces 

of fuel coming from the left-hand engine 

boost pump at the location of the belly fairing 

screw (FS412, BL 0.0). 

(3) Do a general visual inspection of the 

right-hand landing light compartment for 

traces of fuel coming from the APU EFP. 

(i) New Requirements of This AD: 

Inspections and Rectifications 

For the airplanes identified in figure 1 to 

paragraph (i) of this AD: At the applicable 

compliance time specified in figure 1 to 

paragraph (i) of this AD, do a general visual 

inspection for any fuel leak from the engine 

and APU EFP electrical wiring conduit 

outlets, in accordance with the 

Accomplishment Instructions of the 

applicable service information specified in 

figure 1 to paragraph (i) of this AD. If any fuel 

leak is found during the general visual 

inspection, before further flight, correct the 

fuel leak in accordance with the 

Accomplishment Instructions of the 

applicable service information specified in 

figure 1 to paragraph (i) of this AD. 

Thereafter, repeat the general visual 

inspection at intervals not to exceed 600 

flight hours or 12 months, whichever occurs 

first. 


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Federal Register / Vol. 87, No. 29 / Friday, February 11, 2022 / Rules and Regulations 7933 

(j) New Requirements of This AD: Inspection 

and Modification 

Within 60 months after the effective date 

of this AD: Do a detailed visual inspection of 

the APU for any damage or deformations, and 

modify the engine EFP installation, in 

accordance with the Accomplishment 

Instructions of the applicable service 

information specified in figure 2 to paragraph 

(j) of this AD. If any damage or deformations 

are found during the detailed visual 

inspection, before further flight, do the repair 

in accordance with the Accomplishment 

Instructions of the applicable service 

information specified in figure 2 to paragraph 

(j) of this AD. 

(k) No Reporting Requirement 

Where service information identified in 

this AD specifies to submit certain 

information to the manufacturer, this AD 

does not include that requirement. 

(l) Terminating Actions 

Accomplishing the actions required by 

paragraph (j) of this AD terminates all 

requirements of this AD. 

(m) Credit for Previous Actions 

(1) This paragraph provides credit for 

actions required by paragraph (g) of this AD, 

if those actions were performed before the 

effective date of this AD using Bombardier 

Service Bulletin 604–28–022, dated October 

19, 2015, provided that within 4 months or 

150 flight hours from the effective date of this 

AD or within 1 year from the last inspection, 

whichever occurs first, the actions specified 

in paragraph (g) are done using Bombardier 

Service Bulletin 604–28–022, Revision 3, 

dated August 31, 2018. Bombardier Service 

Bulletin 604–28–022, dated October 19, 2015, 

was incorporated by reference in AD 2017– 

22–06. 

(2) This paragraph provides credit for 

actions required by paragraph (h) of this AD, 

if those actions were performed before the 

effective date of this AD using Bombardier 

Service Bulletin 605–28–010, dated October 

19, 2015, provided that within 4 months or 

150 flight hours from the effective date of this 

AD or within 1 year from the last inspection, 

whichever occurs first, the actions specified 

in paragraph (h) of this AD are done using 

Bombardier Service Bulletin 605–28–010, 

Revision 3, dated August 31, 2018. 

Bombardier Service Bulletin 605–28–010, 

dated October 19, 2015, was incorporated by 

reference in AD 2017–22–06. 

(3) This paragraph provides credit for 

actions required by paragraph (i) of this AD, 

if those actions were performed before the 

effective date of this AD using the service 

information in paragraphs (m)(3)(i) through 

(iii) of this AD, provided that within 1 year 

from the last inspection, the actions 

accomplished in paragraph (i) of this AD are 

done using Bombardier Service Bulletin 650– 

28–001, Revision 3, dated January 3, 2019. 

This service information is not incorporated 

by reference in this AD. 

(i) Bombardier Service Bulletin 650–28– 

001, dated November 3, 2017. 

(ii) Bombardier Service Bulletin 650–28– 

001, Revision 1, dated May 14, 2018. 

(iii) Bombardier Service Bulletin 650–28– 

001, Revision 2, dated August 31, 2018. 

(4) This paragraph provides credit for 

actions required by paragraph (j) of this AD, 

if those actions were performed before the 

effective date of this AD using Bombardier 

Service Bulletin 604–28–024, dated June 16, 

2020. This service information is not 

incorporated by reference in this AD. 

(n) Other FAA AD Provisions 

(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 


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Figure 1 to paragraph (i) - Compliance Times and Service Information 

Serial numbers- Compliance Time- Bombardier Service 

Bulletin 

5956, 5958, 5959, Within 600 flight hours or 12 5967,5972through Bombardier Service Bulletin 

5980 inclusive, and months, whichever occurs first 

5982 through 5990 after the effective date of this 605-28-010, Revision 3, 

inclusive AD dated August 31, 2018 

6050 through 6163 

Within 600 flight hours or 12 Bombardier Service Bulletin months, whichever occurs first 

inclusive after the effective date of this 650-28-001, Revision 3, 

AD dated January 3, 2019 

Figure 2 to paragraph G) - Service Information 

Serial numbers5301 through 5665 inclusive 

5701 through 5990 inclusive 

6050 through 6163 inclusive 

Bombardier Service Bulletin 

Bombardier Service Bulletin 604-28-024 

Revision 01, dated May 28, 2021 ' 

Bombardier Service Bulletin 605-28-012 

dated June 16, 2020 ' 

Bombardier Service Bulletin 650-28-002 

dated June 16, 2020 ' 
7934 Federal Register / Vol. 87, No. 29 / Friday, February 11, 2022 / Rules and Regulations 

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. 

(o) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) TCCA AD 

CF–2016–32R4, dated October 13, 2020; and 

TCCA AD CF–2020–38, dated October 13, 

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– 

2021–0725. 

(2) For more information about this AD, 

contact Steven Dzierzynski, Aerospace 

Engineer, Avionics and Electrical Systems 

Section, FAA, New York ACO Branch, 1600 

Stewart Avenue, Suite 410, Westbury, NY 

11590; telephone 516–228–7367; fax 516– 

794–5531; email 9-avs-nyaco-cos@faa.gov. 

(3) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (p)(5) and (6) of this AD. 

(p) 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. 

(3) The following service information was 

approved for IBR on February 25, 2022 (87 

FR 3184, January 21, 2022). 

(i) Bombardier Service Bulletin 604–28– 

022, Revision 3, dated August 31, 2018. 

(ii) Bombardier Service Bulletin 604–28– 

024, Revision 01, dated May 28, 2021. 

(iii) Bombardier Service Bulletin 605–28– 

010, Revision 3, dated August 31, 2018. 

(iv) Bombardier Service Bulletin 605–28– 

012, dated June 16, 2020. 

(v) Bombardier Service Bulletin 650–28– 

001, Revision 3, dated January 3, 2019. 

(vi) Bombardier Service Bulletin 650–28– 

002, dated June 16, 2020. 

(4) The following service information was 

approved for IBR on November 30, 2017 (82 

FR 49498, October 26, 2017). 

(i) Bombardier Service Bulletin 604–28– 

022, dated October 19, 2015. 

(ii) Bombardier Service Bulletin 605–28– 

010, dated October 19, 2015. 

(5) 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 1–514–855–2999; email 

ac.yul@aero.bombardier.com; internet 

https://www.bombardier.com. 

(6) 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. 

(7) 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 February 7, 2022. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–02881 Filed 2–10–22; 8:45 am] 

BILLING CODE 4910–13–P 

SECURITIES AND EXCHANGE 

COMMISSION 

17 CFR Part 249 

[Release No. 34–87005D; File No. S7–05– 

14] 

RIN 3235–AL45 

Recordkeeping and Reporting 

Requirements for Security-Based 

Swap Dealers, Major Security-Based 

Swap Participants, and BrokerDealers; Correction 

AGENCY: Securities and Exchange 

Commission. 

ACTION: Correcting amendment. 

SUMMARY: On September 19, 2019, the 

Securities and Exchange Commission 

(the ‘‘Commission’’) adopted 

recordkeeping, reporting, and 

notification requirements applicable to 

security-based swap dealers and major 

security-based swap participants, 

securities count requirements applicable 

to certain security-based swap dealers, 

and additional recordkeeping 

requirements applicable to brokerdealers to account for their securitybased swap and swap activities. Release 

34–87005 (Sept. 19, 2019) was 

published in the Federal Register on 

Dec. 16, 2019. This document corrects 

technical inaccuracies in that release. 

DATES: Effective February 11, 2022. 

FOR FURTHER INFORMATION CONTACT: 

Valentina Minak Deng, Special Counsel, 

at (202) 551–5778; Division of Trading 

and Markets, Securities and Exchange 

Commission, 100 F Street NE, 

Washington, DC 20549–7010. 

SUPPLEMENTARY INFORMATION: We are 

making technical corrections to Part II 

and Part IIC of Form X–17A–5 

(referenced in 17 CFR 249.617). The 

release resulting in the technical 

inaccuracies was published in the 

Federal Register on December 16, 2019 

at 84 FR 68550, and adopted by the 

Commission in Exchange Act Release 

No. 87005 on September 19, 2019. 

List of Subjects in 17 CFR Part 249 

Brokers, Recordkeeping and reporting 

requirements, Securities. 

Accordingly, 17 CFR part 249 is 

corrected by making the following 

amendments: 

PART 249—FORMS, SECURITIES 

EXCHANGE ACT OF 1934 

■ 1. The authority citation for part 249 

continues to read, in part, as follows: 

Authority: 15 U.S.C. 78a et seq. and 7201 

et seq.; 12 U.S.C. 5461 et seq.; 18 U.S.C. 1350; 

Sec. 953(b), Pub. L. 111–203, 124 Stat. 1904; 

Sec. 102(a)(3), Pub. L. 112–106, 126 Stat. 309 

(2012); Sec. 107, Pub. L. 112–106, 126 Stat. 

313 (2012), and Sec. 72001, Pub. L. 114–94, 

129 Stat. 1312 (2015), unless otherwise 

noted. 

* * * * * 

Section 249.617 is also issued under Pub. 

L. 111–203, 939, 939A, 124. Stat. 1376 (2010) 

(15 U.S.C. 78c, 15 U.S.C. 78o–7 note). 

* * * * * 

■ 2. Amend Part II of Form X–17A–5 

(referenced in § 249.617 of this chapter) 

by: 

BILLING CODE 8011–01–P 


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