36266 Federal Register / Vol. 87, No. 116 / Thursday, June 16, 2022 / Proposed Rules 

(C) Percentage goals for loans made to 

new borrowers qualifying as YBS 

farmers and ranchers in the territory; or 

(D) Goals for capital committed to 

loans made YBS farmers and ranchers in 

the territory. 

(ii) Board of directors approval and 

review. Goals must be approved by the 

direct lender association’s board of 

directors and reviewed quarterly with 

adjustments made as needed. 

PART 620—DISCLOSURE TO 

SHAREHOLDERS 

■ 3. The authority citation for part 620 

continues to read as follows: 

Authority: Secs. 4.3, 4.3A, 4.19, 5.9, 5.17, 

5.19 of the Farm Credit Act (12 U.S.C. 2154, 

2154a, 2207, 2243, 2252, 2254); sec. 424 of 

Pub. L. 100–233, 101 Stat. 1568, 1656; sec. 

514 of Pub. L. 102–552, 106 Stat. 4102. 

■ 4. Revise § 620.5(k)(2) to read as 

follows: 

§ 620.5 Contents of the annual report to 

shareholders. 

* * * * * 

(k) * * * 

(2) Each direct lender association 

must provide a description of its young, 

beginning, and small (YBS) farmers and 

ranchers program, including a status 

report on each program component as 

set forth in § 614.4165(d) of this chapter 

and the definitions of ‘‘young,’’ 

‘‘beginning,’’ and ‘‘small’’ farmers and 

ranchers. The discussion must provide 

such other information necessary for a 

comprehensive understanding of the 

direct lender association’s YBS program 

and its results. 

* * * * * 

Dated: June 9, 2022. 

Ashley Waldron, 

Secretary, Farm Credit Administration Board. 

[FR Doc. 2022–12803 Filed 6–15–22; 8:45 am] 

BILLING CODE 6705–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0680; Project 

Identifier MCAI–2021–01415–T] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2020–22–03, which applies to all Airbus 

SAS Model A330–200, –200 Freighter, 

and –300 series airplanes. AD 2020–22– 

03 requires revising the existing 

airplane flight manual (AFM) to 

incorporate procedures to be applied if 

an engine bleed over-temperature occurs 

when the associated engine bleed valve 

is jammed open, and provides for the 

optional embodiment of updated flight 

warning computer (FWC) software, 

which terminates the AFM revision. 

Since the FAA issued AD 2020–22–03, 

new maintenance actions and software 

related to over-temperature failure 

conditions were developed. This 

proposed AD would continue to require 

the actions specified in AD 2020–22–03, 

would require accomplishing the new 

maintenance tasks and corrective 

actions, and would mandate 

embodiment of the updated FWC 

software for certain airplanes, as 

specified in a European Union Aviation 

Safety Agency (EASA), which is 

proposed for incorporation by reference. 

This proposed AD would also prohibit 

the installation of affected FWC 

software. 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 August 1, 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 material that will be incorporated 

by reference (IBR) in this AD, 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 material on the EASA website 

at https://ad.easa.europa.eu. 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–2022–0680. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0680; 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, the mandatory continuing 

airworthiness information (MCAI), any 

comments received, and other 

information. The street address for 

Docket Operations is listed above. 

FOR FURTHER INFORMATION CONTACT: 

Vladimir Ulyanov, Aerospace Engineer, 

Large Aircraft Section, International 

Validation Branch, FAA, 2200 South 

216th St., Des Moines, WA 98198; 

telephone and fax: 206–231–3229; 

email: vladimir.ulyanov@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–2022–0680; Project Identifier 

MCAI–2021–01415–T’’ at the beginning 

of your comments. The most helpful 

comments reference a specific portion of 

the proposal, explain the reason for any 

recommended change, and include 

supporting data. The FAA will consider 

all comments received by the closing 

date and may amend this 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 


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under the FOIA, and they will not be 

placed in the public docket of this 

NPRM. Submissions containing CBI 

should be sent to Vladimir Ulyanov, 

Aerospace Engineer, Large Aircraft 

Section, International Validation 

Branch, FAA, 2200 South 216th St., Des 

Moines, WA 98198; telephone and fax: 

206–231–3229; email: 

vladimir.ulyanov@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 

The FAA issued AD 2020–22–03, 

Amendment 39–21299 (85 FR 66873, 

October 21, 2020) (AD 2020–22–03), 

which applies to all Airbus SAS Model 

A330–200, –200 Freighter, and –300 

series airplanes. AD 2020–22–03 

requires revising the existing AFM to 

incorporate procedures to be applied if 

an engine bleed over-temperature occurs 

when the associated engine bleed valve 

is jammed open. AD 2020–22–03 also 

provides for the optional embodiment of 

updated FWC software, which would 

terminate the AFM revision, as specified 

in EASA AD 2020–0205. 

The FAA issued AD 2020–22–03 to 

address the possibility of a jammed 

engine bleed valve, which could lead to 

damage of the bleed manifold and the 

ducts downstream of the engine bleed 

system, exposure of the surrounding 

structure to heat stress, and possible 

reduced structural integrity of the 

airplane. 

Actions Since AD 2020–22–03 Was 

Issued 

Since the FAA issued AD 2020–22– 

03, it has been determined that new 

maintenance tasks for failures related to 

over-temperature conditions must be 

accomplished, and embodiment of 

updated FWC software must be 

mandated for certain airplanes. 

EASA, which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2021–0281, 

dated December 17, 2021 (EASA AD 

2021–0281) (also referred to as the 

MCAI), to correct an unsafe condition 

for Airbus SAS Model A330–201, –202, 

–203, –223, –223F, –243, and –243F 

airplanes, Model A330–301, –302, –303, 

–321, –322, –323, –341, –342, –343, and 

–743L airplanes. 

Model A330–743L airplanes are not 

certificated by the FAA and are not 

included on the U.S. type certificate 

data sheet; this AD therefore does not 

include those airplanes in the 

applicability. 

EASA AD 2021–0281 specifies that 

after the software update (modification) 

required by this proposed AD is done on 

an airplane, that airplane remains 

compliant with the requirements of 

paragraph (2) of EASA AD 2020–0077 

(which corresponds to FAA AD 2020– 

17–16, Amendment 39–21221 (85 FR 

54900, September 3, 2020)). AD 2020– 

17–16 requires, among other actions, 

installing FWC standard T9 on Airbus 

SAS Model A330–200 and –300 series 

airplanes. This proposed AD would 

require installing FWC standard T9–3, 

which replaces FWC standard T9. 

This proposed AD was prompted by 

the development of new maintenance 

actions and software related to overtemperature failure conditions. The 

FAA is proposing this AD to address the 

possibility of a jammed engine bleed 

valve, which could lead to damage of 

the bleed manifold and the ducts 

downstream of the engine bleed system, 

exposure of the surrounding structure to 

heat stress, and possible reduced 

structural integrity of the airplane. See 

the MCAI for additional background 

information. 

Explanation of Retained Requirements 

Although this proposed AD does not 

explicitly restate the requirements of AD 

2020–22–03, this proposed AD would 

retain the requirements of AD 2020–22– 

03. Those requirements are referenced 

in EASA AD 2021–0281, which, in turn, 

are referenced in paragraph (g) of this 

proposed AD. 

Related Service Information Under 1 

CFR Part 51 

EASA AD 2021–0281 specifies 

procedures for amending the applicable 

AFM to incorporate procedures to be 

applied if an engine bleed overtemperature occurs when the associated 

engine bleed valve is jammed open. 

EASA AD 2020–0281 also specifies that 

embodiment of updated FWC software 

standard T9 would eliminate the need 

for the AFM amendment. EASA AD 

2021–0281 also describes maintenance 

tasks for failures related to overtemperature conditions and corrective 

actions (repair). EASA AD 2021–0281 

also specifies procedures for the 

embodiment of updated FWC software 

standard T9–3, and, for certain airplanes 

concurrent embodiment of system data 

acquisition concentrator (SDAC) 

software standard C13 or FWC software 

standard K3–2 and SDAC software 

standard C3–0A. Finally, EASA AD 

2021–0281 prohibit the installation of 

affected FWC software (FWC software 

standard T9–2 or earlier). This material 

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, it has notified the 

FAA of the unsafe condition described 

in the MCAI referenced above. The FAA 

is issuing this NPRM after determining 

that the unsafe condition described 

previously is likely to exist or develop 

in other products of the same type 

design. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would require 

accomplishing the actions specified in 

EASA AD 2021–0281 described 

previously, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD. 

This proposed AD would also prohibit 

the installation of affected FWC 

software. 

EASA AD 2021–0281 requires 

operators to ‘‘inform all flight crews’’ of 

revisions to the AFM, and thereafter to 

‘‘operate the aeroplane accordingly.’’ 

However, this proposed AD would not 

specifically require those actions as 

those actions are already required by 

FAA regulations. FAA regulations 

require operators furnish to pilots any 

changes to the AFM (for example, 14 

CFR 121.137), and to ensure the pilots 

are familiar with the AFM (for example, 

14 CFR 91.505). As with any other 

flightcrew training requirement, training 

on the updated AFM content is tracked 

by the operators and recorded in each 

pilot’s training record, which is 

available for the FAA to review. FAA 

regulations also require pilots to follow 

the procedures in the existing AFM 

including all updates. 14 CFR 91.9 

requires that any person operating a 

civil aircraft must comply with the 

operating limitations specified in the 

AFM. Therefore, including a 

requirement in this proposed AD to 

operate the airplane according to the 

revised AFM would be redundant and 

unnecessary. 

Explanation of Required Compliance 

Information 

In the FAA’s ongoing efforts to 

improve the efficiency of the AD 

process, the FAA developed a process to 

use some civil aviation authority (CAA) 

ADs as the primary source of 

information for compliance with 

requirements for corresponding FAA 

ADs. The FAA has been coordinating 


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this process with manufacturers and 

CAAs. As a result, the FAA proposes to 

incorporate EASA AD 2021–0281 by 

reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2021–0281 

in its entirety through that 

incorporation, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD. 

Using common terms that are the same 

as the heading of a particular section in 

EASA AD 2021–0281 does not mean 

that operators need comply only with 

that section. For example, where the AD 

requirement refers to ‘‘all required 

actions and compliance times,’’ 

compliance with this AD requirement is 

not limited to the section titled 

‘‘Required Action(s) and Compliance 

Time(s)’’ in EASA AD 2021–0281. 

Service information required by EASA 

AD 2021–0281 for compliance will be 

available at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2022–0680 after the FAA final 

rule is published. 

Costs of Compliance 

The FAA estimates that this AD 

affects 115 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 

AFM revision: 1 work-hour × $85 per hour = $85 ........................................................... $0 $85 ...................... $9,775. 

Software Update: 3 work-hours × 85 per hour = $255 .................................................... 0 $255 .................... Up to $29,325. 

Maintenance Tasks: 7 work-hours × $85 per hour = $595 ............................................. 720 $595 .................... $151,225. 

Concurrent Actions: Up to 4 work-hours × $85 per hour = Up to $340 .......................... 0 Up to $340 .......... Up to $39,100. 

ESTIMATED COSTS FOR OPTIONAL ACTIONS

Labor cost Parts cost Cost per 

product 

2 work-hours × $85 per hour = $170 ...................................................................................................................... $0 $170 

The FAA has received no definitive 

data that would enable the agency to 

provide cost estimates for the oncondition actions specified in this 

proposed AD. 

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. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 14 CFR part 

39 as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by: 

■ a. Removing Airworthiness Directive 

(AD) 2020–22–03, Amendment 39– 

21299 (85 FR 66873, October 21, 2020); 

and 

■ b. Adding the following new AD: 

Airbus SAS: Docket No. FAA–2022–0680; 

Project Identifier MCAI–2021–01415–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by August 1, 

2022. 

(b) Affected ADs 

This AD replaces AD 2020–22–03, 

Amendment 39–21299 (85 FR 66873, October 

21, 2020) (AD 2020–22–03). 

(c) Applicability 

This AD applies to all Airbus SAS Model 

airplanes, certificated in any category, as 

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

this AD. 

(1) Model A330–201, –202, –203, –223, and 

–243 airplanes. 

(2) Model A330–223F and –243F airplanes. 

(3) Model A330–301, –302, –303, –321, 

–322, –323, –341, –342, and –343 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 75, Air; Code 36, Pnuematic. 

(e) Unsafe Condition 

This AD was prompted by a report that 

during a certification exercise, it was 

identified that there was a risk of an engine 

bleed system over-temperature, without the 

engine bleed valve closing; the associated 

engine bleed valve should automatically 

close. This AD was also prompted by the 

development of new maintenance actions 

and software related to over-temperature 

failure conditions. The FAA is issuing this 

AD to address the possibility of a jammed 

engine bleed valve, which could lead to 

damage of the bleed manifold and the ducts 

downstream of the engine bleed system, 

exposure of the surrounding structure to heat 


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Federal Register / Vol. 87, No. 116 / Thursday, June 16, 2022 / Proposed Rules 36269 

stress, and possible reduced structural 

integrity of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Requirements 

Except as specified in paragraph (h) of this 

AD: Comply with all required actions and 

compliance times specified in, and in 

accordance with, European Union Aviation 

Safety Agency (EASA) AD 2021–0281, dated 

December 17, 2021 (EASA AD 2021–0281). 

(h) Exceptions to EASA AD 2021–0281 

(1) Where EASA AD 2021–0281 refers to 

October 1, 2020 (the effective date of EASA 

AD 2020–0205), this AD requires using 

November 5, 2020 (the effective date of AD 

2020–22–03). 

(2) Where EASA AD 2021–0281 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

(3) Where paragraph (1) of EASA AD 2021– 

0281 specifies to ‘‘inform all flight crews, 

and, thereafter, operate the aeroplane 

accordingly,’’ this AD does not require those 

actions as those actions are already required 

by existing FAA operating regulations. 

(4) Where paragraphs (6) and (7) of EASA 

AD 2021–0281 specifies actions if ‘‘any 

discrepancies are detected,’’ for this AD 

discrepancies include failures related to an 

over-temperature situation, hidden failures in 

equipment for a ‘‘not isolated overtemperature’’ failure condition, cracking on 

the exchanger outlet temperature sensor, or 

dual drift in the exchanger outlet temperature 

sensor. 

(5) Where paragraph (11) of EASA AD 

2021–0281 specifies that an airplane with 

certain modifications is compliant with ‘‘the 

requirements of paragraph (2) of EASA AD 

2020–0077,’’ for this AD use ‘‘for the 

corresponding requirements of paragraph (2) 

of EASA AD 2020–0077 that are required by 

paragraph (g) of AD 2020–17–16, 

Amendment 39–21221 (85 FR 54900, 

September 3, 2020).’’ 

(6) The ‘‘Remarks’’ section of EASA AD 

2021–0281 does not apply to this AD. 

(i) No Reporting Requirements 

Although the service information 

referenced in EASA AD 2021–0281 specifies 

to submit certain information to the 

manufacturer, this AD does not include that 

requirement. 

(j) Additional FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Large Aircraft 

Section, International Validation 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 Large Aircraft 

Section, International Validation Branch/ 

manager of the certification office, send it to 

the attention of the person identified in 

paragraph (k)(2) of this AD. Information may 

be emailed to: 9-AVS-AIR-730-AMOC@

faa.gov. 

(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, Large Aircraft Section, 

International Validation Branch, FAA; or 

EASA; or Airbus SAS’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(3) Required for Compliance (RC): Except 

as required by paragraph (j)(2) of this AD, if 

any service information referenced in EASA 

AD 2021–0281 contains paragraphs that are 

labeled as RC, the instructions in RC 

paragraphs, including subparagraphs under 

an RC paragraph, must be done to comply 

with this AD; any paragraphs, including 

subparagraphs under those paragraphs, that 

are not identified as RC are recommended. 

The instructions in paragraphs, including 

subparagraphs under those paragraphs, not 

identified as RC may be deviated from using 

accepted methods in accordance with the 

operator’s maintenance or inspection 

program without obtaining approval of an 

AMOC, provided the instructions identified 

as RC can be done and the airplane can be 

put back in an airworthy condition. Any 

substitutions or changes to instructions 

identified as RC require approval of an 

AMOC. 

(k) Related Information 

(1) For EASA AD 2021–0281, 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. 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. This 

material may be found in the AD docket at 

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

and locating Docket No. FAA–2022–0680. 

(2) For more information about this AD, 

contact Vladimir Ulyanov, Aerospace 

Engineer, Large Aircraft Section, 

International Validation Branch, FAA, 2200 

South 216th St., Des Moines, WA 98198; 

telephone and fax: 206–231–3229; email: 

Vladimir.Ulyanov@faa.gov. 

Issued on June 10, 2022. 

Christina Underwood, 

Acting Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–12936 Filed 6–15–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0679; Project 

Identifier MCAI–2021–01213–T] 

RIN 2120–AA64 

Airworthiness Directives; MHI RJ 

Aviation ULC (Type Certificate 

Previously Held by 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 all 

MHI RJ Aviation ULC Model CL–600– 

2C10 (Regional Jet Series 700, 701 & 

702) airplanes, Model CL–600–2C11 

(Regional Jet Series 550) airplanes, 

Model CL–600–2D15 (Regional Jet 

Series 705) airplanes, Model CL–600– 

2D24 (Regional Jet Series 900) airplanes, 

and Model CL–600–2E25 (Regional Jet 

Series 1000) airplanes. This proposed 

AD was prompted by a determination 

that new and more restrictive 

airworthiness limitations are necessary. 

This proposed AD would require 

revising the existing maintenance or 

inspection program, as applicable, to 

incorporate new and more restrictive 

airworthiness limitations. 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 August 1, 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 MHI RJ Aviation 

Group, Customer Response Center, 3655 

Ave. des Grandes-Tourelles, Suite 110, 

Boisbriand, Que ́bec J7H 0E2 Canada; 

North America toll-free telephone 833– 

990–7272 or direct-dial telephone 450– 

990–7272; fax 514–855–8501; email 

thd.crj@mhirj.com; internet https:// 


khammond on DSKJM1Z7X2PROD with PROPOSALS