6082 Federal Register / Vol. 87, No. 23 / Thursday, February 3, 2022 / Proposed Rules 

familiarity with, and to ask, as 

appropriate, substantive questions of 

management and the internal and 

external auditors of: 

(i) Basic finance and accounting 

practices, including the ability to read 

and understand the Federal credit 

union’s balance sheet and income 

statement; and 

(ii) The Federal credit union’s 

succession plan established pursuant to 

paragraph (e) of this section. 

* * * * * 

(e) Succession planning. (1) General. 

A Federal credit union board of 

directors must establish a process to 

ensure proper succession planning to 

include officers of the board, 

management officials, executive 

committee members, supervisory 

committee members, and (where 

provided for in the bylaws) the members 

of the credit committee, as described in 

Appendix A. 

(2) Board responsibilities. The board 

of directors or an appropriate committee 

of the board must: 

(i) Approve a written succession plan 

that covers the individuals described in 

paragraph (e)(1) of this section; and 

(ii) Review, and update as deemed 

necessary, the succession plan and 

policy in accordance with a schedule 

established by the board of directors, 

but no less than annually. 

(3) Succession plan contents. The 

succession plan must, at a minimum, 

identify key positions covered by the 

plan, necessary general competencies 

and skills for those positions, and 

strategies to identify alternatives to fill 

vacancies. 

[FR Doc. 2022–02038 Filed 2–2–22; 8:45 am] 

BILLING CODE 7535–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0085; Project 

Identifier MCAI–2021–00498–T] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc., Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to adopt a 

new airworthiness directive (AD) for 

certain Bombardier, Inc., Model BD– 

700–1A10 and BD–700–1A11 airplanes. 

This proposed AD was prompted by 

reports of oxygen leaks caused by 

cracked, brittle, or broken oxygen hoses 

that were found during scheduled 

maintenance tests of the airplane 

oxygen system. This proposed AD 

would require an inspection of the 

oxygen hose assembly to determine if an 

affected part number is installed, and 

replacement of affected oxygen hoses. 

For certain airplanes, this proposed AD 

would allow repetitive testing of the 

oxygen system until affected hoses are 

replaced. This proposed AD would also 

prohibit installation of an affected 

oxygen hose. 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 March 21, 2022. 

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 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. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0085; or in person at Docket 

Operations between 9 a.m. and 5 p.m., 

Monday through Friday, except Federal 

holidays. The AD docket contains this 

NPRM, any comments received, and 

other information. The street address for 

Docket Operations is listed above. 

FOR FURTHER INFORMATION CONTACT: 

Elizabeth Dowling, 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; 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 ADDRESSES. Include ‘‘Docket No. 

FAA–2022–0085; Project Identifier 

MCAI–2021–00498–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 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 

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 Elizabeth Dowling, 

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; 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. 

Background 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 


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for Canada, has issued TCCA AD CF– 

2021–17, dated April 28, 2021 (also 

referred to after this as the Mandatory 

Continuing Airworthiness Information, 

or the MCAI), to correct an unsafe 

condition for certain Bombardier, Inc., 

Model BD–700–1A10 and BD–700– 

1A11 airplanes. You may examine the 

MCAI in the AD docket at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2022– 

0085. 

This proposed AD was prompted by 

reports of oxygen leaks caused by 

cracked, brittle, or broken oxygen hoses 

that were found during scheduled 

maintenance tests of the airplane 

oxygen system. The FAA is proposing 

this AD to prevent a leak in the oxygen 

line, which may result in failure to 

provide oxygen to passengers and crew 

and result in an oxygen-enriched 

atmosphere creating a fire risk on the 

airplane. See the MCAI for additional 

background information. 

Related Service Information Under 1 

CFR Part 51 

Bombardier has issued the following 

service information. 

• Bombardier Service Bulletin 700– 

1A11–35–014, Revision 01, dated 

February 12, 2021. 

• Bombardier Service Bulletin 700– 

35–015, Revision 01, dated February 12, 

2021. 

• Bombardier Service Bulletin 700– 

35–5005, Revision 01, dated February 

12, 2021. 

• Bombardier Service Bulletin 700– 

35–6005, Revision 01, dated February 

12, 2021. 

• Bombardier Service Bulletin 700– 

35–6501, Revision 01, dated February 

12, 2021. 

This service information describes 

procedures for doing an inspection of 

the oxygen hose assembly installations 

to determine if a part number within the 

series O2C20T1 is installed, and 

replacing the oxygen hose if necessary. 

For certain airplanes, the service 

information specifies optional repetitive 

testing of the oxygen system that would 

allow for delay of the replacement. 

These documents are distinct since they 

apply to different airplane serial 

numbers. 

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. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would require 

accomplishing the actions specified in 

the service information already 

described. This proposed AD would 

also prohibit installation of an affected 

oxygen hose. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 409 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this proposed AD: 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per product Cost on U.S. 

operators 

Up to 36 work-hours × $85 per hour = Up to $3,060 $0 Up to $3,060 .................................. Up to $1,251,540. 

ESTIMATED COSTS FOR OPTIONAL ACTIONS

Labor cost Parts cost Cost per product 

Up to 25 work-hours × $85 per hour = Up to $2,125 ............. Up to $125 ............................................. Up to $2,250. 

The FAA has included all known 

costs in its cost estimate. According to 

the manufacturer, however, some or all 

of the costs of this proposed AD may be 

covered under warranty, thereby 

reducing the cost impact on affected 

operators. 

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) Would not affect intrastate 

aviation in Alaska, and 

(3) Would not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 


khammond on DSKJM1Z7X2PROD with PROPOSALS
6084 Federal Register / Vol. 87, No. 23 / Thursday, February 3, 2022 / Proposed Rules 

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 adding 

the following new airworthiness 

directive: 

Bombardier, Inc.: Docket No. FAA–2022– 

0085; Project Identifier MCAI–2021– 

00498–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by March 21, 

2022. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Bombardier, Inc., 

Model BD–700–1A10 and BD–700–1A11 

airplanes, certificated in any category, serial 

numbers 9002 through 9879 inclusive and 

9998. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 35, Oxygen. 

(e) Unsafe Condition 

This AD was prompted by reports of 

oxygen leaks caused by cracked, brittle or 

broken oxygen hoses that were found during 

scheduled maintenance tests of the airplane 

oxygen system. The FAA is issuing this AD 

to address a leak in the oxygen line, which 

may result in failure to provide oxygen to 

passengers and crew and result in an oxygen 

enriched atmosphere creating a fire risk on 

the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection and Replacement 

Within 6 months after the effective date of 

this AD: Do an inspection of the oxygen hose 

assembly to determine if any hose having a 

part number (P/N) in the O2C20T1 series is 

installed, in accordance with the 

Accomplishment Instructions of the 

applicable service information specified in 

figure 1 to paragraph (g) of this AD. If P/N 

O2C20T1 series is installed, or if any test 

fails as specified in paragraph (h) of this AD: 

Before further flight, replace all the oxygen 

hoses, in accordance with the 

Accomplishment Instructions of the 

applicable service information specified in 

figure 1 to paragraph (g) of this AD. 

BILLING CODE 4910–13–P 


khammond on DSKJM1Z7X2PROD with PROPOSALS
Federal Register / Vol. 87, No. 23 / Thursday, February 3, 2022 / Proposed Rules 6085 

(h) Optional Interim Testing for Certain 

Airplanes 

For airplanes identified in figure 2 of 

paragraph (h) of this AD: The oxygen hose 

replacement, if required by paragraph (g) of 

this AD, may be delayed if all conditions 

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

this AD are met. 

(1) The oxygen system is tested at the 

applicable times specified in paragraph 

(h)(1)(i) or (ii) of this AD, in accordance with 

the Accomplishment Instructions of the 

applicable service information specified in 

figure 2 to paragraph (h) of this AD. 

(i) If the Aircraft Completion Center 

Supplemental Type Certificate (STC) for the 

passenger cabin interior was issued within 5 

years before the effective date of this AD: The 

oxygen system is tested within 6 months after 

the effective date of this AD, and thereafter 

at intervals not to exceed 30 months. 

(ii) If the Aircraft Completion Center STC 

for the passenger cabin interior was issued 5 

years or more before the effective date of this 

AD: The oxygen system is tested within 6 

months after the effective date of this AD, 

and thereafter at intervals not to exceed 15 

months. 

(2) All P/N O2C20T1 series hoses are 

replaced before further flight as specified in 

paragraph (g) of this AD after any hose fails 

any test. 


khammond on DSKJM1Z7X2PROD with PROPOSALSEP03FE22.025</GPH>

Figure 1 to paragraph (g) - Service Information 

Model- Serial Numbers- Bombardier 

Service Bulletin9002 through 9005 inclusive, 9007 through 

9014 inclusive, 9016 through 9020 

inclusive, 9022 through 9026 inclusive, 

9028 through 9033 inclusive, 9035, 9036, 

9038 through 9051 inclusive, 9053 through 

BD-700-lAlO 9055 inclusive, 9058 through 9080 700-35-015, 

airplanes inclusive, 9082 through 9106 inclusive, Revision 01, dated 

9108 through 9122 inclusive, 9124 through February 12, 2021 

9129 inclusive, 9133, 9134, 9136 through 

9171 inclusive, 9175, 9179 through 9286 

inclusive, 9290 through 9312 inclusive, 

9314 through 9354 inclusive, 9357, and 

9360 through 9429 inclusive 

9381, 9432 through 9491 inclusive, 9496 

through 9505 inclusive, 9507 through 9515 

inclusive, 9518 through 9525 inclusive, 

9527 through 9619 inclusive, 9622 through 

BD-700-lAlO 9654 inclusive, 9657 through 9673 700-35-6005, 

airplanes inclusive, 9677, 9680 through 9684 Revision 01, dated 

inclusive, 9686 through 9712 inclusive, February 12, 2021 

9716 through 9742 inclusive, 9744 through 

9785 inclusive, 9788 through 9853 

inclusive, 9856 through 9867 inclusive, 

9870, 9873 through 9878 inclusive 

BD-700-lAlO 9861 and 9872 700-35-6501 

airplanes Revision 01, dated 

February 12, 2021 

9130 through 9209 inclusive, 9212 through 700-lAl 1-35-014, BD-700-lAll 9305 inclusive, 9311 through 9359 Revision 01, dated airplanes inclusive, 9366 through 9430 inclusive, and February 12, 2021 9998 

BD-700-lAll 9386, 9401 through 9613 inclusive, and 700-35-5005, 

Revision 01, dated airplanes 9618 through 9879 inclusive February 12, 2021 
6086 Federal Register / Vol. 87, No. 23 / Thursday, February 3, 2022 / Proposed Rules 

(3) Except as specified by paragraph (h)(2) 

of this AD, all P/N O2C20T1 series hoses are 

replaced within 10 years after issuance of the 

Aircraft Completion Center STC for the 

passenger cabin interior as specified in 

paragraph (g) of this AD provided that all 

P/N O2C20T1 series hoses in the flight 

compartment and the third crew (left-hand 

side enclosure) are replaced within 6 months 

after the effective date of this AD. 

(i) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install an oxygen hose assembly 

having a P/N in the O2C20T1 series on any 

airplane. 

(j) Credit for Previous Actions 

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 the applicable service 

information specified in paragraphs (j)(1) 

through (5) of this AD. 

(1) Bombardier Service Bulletin 700– 

1A11–35–014, dated September 28, 2020. 

(2) Bombardier Service Bulletin 700–35– 

015, dated September 28, 2020. 

(3) Bombardier Service Bulletin 700–35– 

5005, dated September 28, 2020. 

(4) Bombardier Service Bulletin 700–35– 

6005, dated September 28, 2020. 

(5) Bombardier Service Bulletin 700–35– 

6501, dated September 28, 2020. 

(k) 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; 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. 

(l) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) TCCA AD 

CF–2021–17, dated April 28, 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–2022–0085. 

(2) For more information about this AD, 

contact Elizabeth Dowling, 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; fax 516–794–5531; email 

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

(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 

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. 

Issued on January 28, 2022. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–02141 Filed 2–2–22; 8:45 am] 

BILLING CODE 4910–13–C 


khammond on DSKJM1Z7X2PROD with PROPOSALSEP03FE22.026</GPH>

Figure 2 to paragraph (h)-Service Information for Optional Interim Testing 

Model- Serial Numbers- Bombardier 

Service Bulletin9381, 9432 through 9491 inclusive, 9496 

through 9505 inclusive, 9507 through 9515 

inclusive, 9518 through 9525 inclusive, 

9527 through 9619 inclusive, 9622 through 

BD-700-lAl0 9654 inclusive, 9657 through 9673 700-35-6005, 

airplanes inclusive, 9677, 9680 through 9684 Revision 01, dated 

inclusive, 9686 through 9712 inclusive, February 12, 2021 

9716 through 9742 inclusive, 9744 through 

9785 inclusive, 9788 through 9853, 9856 

through 9867 inclusive, 9870, 9873 through 

9878 inclusive. 

BD-700-lAlO 700-35-6501 

airplanes 9861 and 9872 Revision 01, dated 

February 12, 2021 

BD-700-lAll 9386, 9401 through 9613 inclusive, and 700-35-5005, 

Revision 01, dated airplanes 9618 through 9879 inclusive February 12, 2021