Federal Register / Vol. 87, No. 87 / Thursday, May 5, 2022 / Proposed Rules 26699 

■ e. Removing the parenthetical 

authority at the end of the section. 

The revisions and addition read as 

follows: 

§ 201.200 Sale of livestock on credit. 

* * * * * 

(b) No dealer whose average annual 

purchases of livestock exceed $100,000 

shall purchase livestock on credit 

unless: 

(1) Before purchasing livestock on 

credit, the dealer obtains from the seller 

a written acknowledgement that 

includes the information described in 

this paragraph (b)(1). 

(i) The following statement: 

On this date I am entering into a 

written agreement for the sale of 

livestock on credit toll, a dealer, and 

I understand that in doing so I will have 

no rights under the trust provisions of 

section 318 of the Packers and 

Stockyards Act, 1921, as amended (7 

U.S.C. 217b), with respect to any such 

credit sale. 

(ii) A statement about whether the 

credit sales agreement covers a single 

sale; covers multiple sales and remains 

in effect through a certain date and 

states the date; or remains in effect until 

canceled in writing by either party. 

(iii) The date the seller signed the 

agreement. 

(iv) The seller’s signature. 

(2) The dealer retains the written 

acknowledgment, together with all other 

documents, if any, setting forth the 

terms of credit sales on which the 

purchaser and seller have agreed, and 

the dealer retains a copy thereof, in their 

records for such time as is required by 

any law, or by written notice served on 

the dealer by the Administrator, but not 

less than two calendar years from the 

date of expiration of the written 

agreement referred to in the 

acknowledgment. 

(3) The dealer provides a copy of the 

acknowledgment to the seller. 

(c) Purchasing livestock for which 

payment is to be made by a draft which 

is not a check shall constitute 

purchasing such livestock on credit 

within the meaning of paragraphs (a) 

and (b) of this section. (See also 

§ 201.43(b)(1).) 

* * * * * 

PART 203—STATEMENTS OF 

GENERAL POLICY UNDER THE 

PACKERS AND STOCKYARDS ACT 

■ 3. The authority for 9 CFR part 203 

continues to read as follows: 

Authority: 7 CFR 2.22 and 2.81. 

■ 4. Revise § 203.15 to read as follows: 

§ 203.15 Trust benefits under sections 206, 

207, and 318 of the Packers and Stockyards 

Act. 

(a) Within the times specified under 

sections 206(b), 207(d), and 318(b) of 

the Act, any livestock seller, live poultry 

seller or grower, to preserve their 

interest in the statutory trust, must give 

written notice to the appropriate packer, 

live poultry dealer, or livestock dealer 

and file such notice with the Secretary 

within the prescribed time by letter, fax, 

email, or other electronic transmission. 

The written notice should provide: 

(1) Notification to preserve trust 

benefits: 

(2) Identification of packer, live 

poultry dealer, or livestock dealer; 

(3) Identification of seller or poultry 

grower; 

(4) Date of the transaction; 

(5) Date of seller’s or poultry grower’s 

receipt of notice that payment 

instrument has been dishonored (if 

applicable); and 

(6) Amount of money due; and to 

make certain that a copy of such letter, 

fax, email, or other electronic 

transmission is filed with a PSD 

regional office or with the PSD 

headquarters office within the 

prescribed time. 

(b) While the information in 

paragraphs (a)(1) through (6) of this 

section is desirable, any written notice 

which informs the packer, live poultry 

dealer, or livestock dealer, and the 

Secretary that the packer, live poultry 

dealer, or livestock dealer has failed to 

pay is sufficient to meet the statutory 

requirement in paragraph (a) of this 

section if it is given within the 

prescribed time. 

(c) For purposes of administering 

statutory trusts under the Act, a cash 

sale means a sale in which the seller 

does not expressly extend credit to the 

buyer. 

(Approved by the Office of Management 

and Budget under control number 0581– 

0308) 

Erin Morris, 

Associate Administrator, Agricultural 

Marketing Service. 

[FR Doc. 2022–09485 Filed 5–4–22; 8:45 am] 

BILLING CODE P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0469; Project 

Identifier MCAI–2021–00124–Q] 

RIN 2120–AA64 

Airworthiness Directives; Cameron 

Balloons Ltd. Burner Assemblies 

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 Cameron Balloons Ltd. 

(Cameron) Stratus double burner 

assemblies installed on hot air balloons. 

This proposed AD was prompted by 

reports from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI identifies the unsafe 

condition as fatigue cracking of the weld 

on Stratus double burner hangers. This 

proposed AD would require repetitively 

inspecting certain Stratus double burner 

hangers and replacing certain Stratus 

double burners, and would prohibit 

installing certain parts. 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 June 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 proposed AD, contact Cameron 

Balloons Ltd., St Johns Street, 

Bedminster, Bristol, BS3 4NH, United 

Kingdom; phone: +44 0 117 9637216; 

email: technical@

cameronballoons.co.uk; website: 

https://www.cameronballoons.co.uk. 

You may view this service information 

at the FAA, Airworthiness Products 

Section, Operational Safety Branch, 901 


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26700 Federal Register / Vol. 87, No. 87 / Thursday, May 5, 2022 / Proposed Rules 

Locust, Kansas City, MO 64106. For 

information on the availability of this 

material at the FAA, call (817) 222– 

5110. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0469; 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 MCAI, any comments 

received, and other information. The 

street address for Docket Operations is 

listed above. 

FOR FURTHER INFORMATION CONTACT: 

Mike Kiesov, Aviation Safety Engineer, 

General Aviation & Rotorcraft Section, 

International Validation Branch, FAA, 

901 Locust, Room 301, Kansas City, MO 

64106; phone: (816) 329–4144; email: 

mike.kiesov@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 the ADDRESSES section. Include 

‘‘Docket No. FAA–2022–0469; Project 

Identifier MCAI–2021–00124–Q’’ 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 

under the FOIA, and they will not be 

placed in the public docket of this 

NPRM. Submissions containing CBI 

should be sent to Mike Kiesov, Aviation 

Safety Engineer, FAA, General Aviation 

& Rotorcraft Section, International 

Validation Branch, 901 Locust, Room 

301, Kansas City, MO 64106. 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 European Union Aviation Safety 

Agency (EASA), which is the Technical 

Agent for the Member States of the 

European Union, has issued EASA AD 

2021–0042, dated January 29, 2021 

(referred to after this as ‘‘the MCAI’’), to 

address an unsafe condition on all hot 

air balloons. The MCAI states: 

An occurrence was been reported of a 

Stratus burner hanger, [part number] P/N 

CB8504, failing after landing, leaving one 

burner unit detached from the load frame. 

Investigation revealed a limited number of 

similar failures. Comparable issues have been 

experienced with other parts of the Stratus 

product line (see Australian [Civil Aviation 

Safety Authority] CASA AWB 14–001 

[Airworthiness Bulletin AWB 14–001, Issue 

3, dated February 5, 2021]). The suspected 

cause is fatigue cracking of the weld, caused 

mainly during ground transportation with the 

burner erect, combined with an overload 

event. 

This condition, if not detected and 

corrected, could lead to burner falling on the 

balloon occupant’s head, resulting in injury 

to balloon occupants. It could also lead to an 

uncontrolled cold descent and hard landing, 

possibly resulting in injury to balloon 

occupants and persons on the ground. 

To address this potential unsafe condition, 

Cameron Balloons issued the SB [Service 

Bulletin No. 28, Revision 3, dated February 

3, 2021], providing inspection and 

replacement instructions. It was determined 

that some burner hangers cannot be 

inspected as they are covered with a doubler 

plate to reinforce the central part of the 

hanger bracket. 

For the reasons described above, this 

[EASA] AD requires repetitive detailed 

inspections (DET) of the affected parts A and, 

depending on findings, replacement with a 

serviceable part. This [EASA] AD also 

requires direct replacement of the burner 

hanger installed on affected parts B. 

You may view the MCAI in the AD 

docket at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2022–0469. 

Related Service Information Under 1 

CFR Part 51 

The FAA reviewed Cameron Balloons 

Service Bulletin 28, Revision 3, dated 

February 3, 2021. The service 

information specifies identifying the 

Stratus double burner hanger, 

inspecting it in accordance with 

Cameron Balloons SB28: 

Accomplishment Instructions CBL/TN/ 

DCB/3191, Issue B, dated February 4, 

2020 (CBL/TN/DCB/3191 Issue B), and 

replacing it if there are any cracks. 

The FAA also reviewed CBL/TN/ 

DCB/3191 Issue B, which contains 

procedures for identifying and 

inspecting affected Stratus double 

burner hangers. 

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 this 

State of Design Authority, it has notified 

the agency of the unsafe condition 

described in the MCAI and service 

information referenced above. The FAA 

is issuing this NPRM after determining 

that the unsafe condition described 

previously is likely to exist or develop 

on other products of the same type 

design. 

Proposed AD Requirements 

This proposed AD would require 

accomplishing the actions specified in 

the service information already 

described, except as discussed under 

‘‘Differences Between this Proposed AD 

and the MCAI.’’ 

Differences Between This Proposed AD 

and the MCAI 

The MCAI requires reporting 

information to Cameron Balloons, and 

this proposed AD would not. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 220 

burner assemblies that have been 

produced worldwide. The FAA has no 

way of knowing how many of these 

burner assemblies are installed on hot 

air balloons of U.S. Registry. Therefore, 

for the purposes of this proposed AD, 

the FAA is basing the fleet cost estimate 

on the maximum number of 220 burner 

assemblies. 

The FAA estimates the following 

costs to comply with this proposed AD: 


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Federal Register / Vol. 87, No. 87 / Thursday, May 5, 2022 / Proposed Rules 26701 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per hot air balloon Cost on U.S. 

operators 

Inspect burner hangers ......... 1 work-hour × $85 per hour 

= $85.

Not applicable ...... $85 per inspection cycle ...... $18,700 per inspection 

cycle. 

The FAA estimates the following 

costs to replace a cracked burner hanger 

or a burner that has a doubler plate. The 

FAA has no way of determining the 

number of hot air balloons that would 

need this action. 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per hot 

air balloon 

Replace with a serviceable part ................................... 1 work-hour × $85 per hour = $85 ............................... $250 $335 

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) Would not be 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 adding 

the following new airworthiness 

directive: 

Cameron Balloons Ltd.: Docket No. FAA– 

2022–0469; Project Identifier MCAI– 

2021–00124–Q. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by June 21, 

2022. 

(b) Affected ADs 

None. 

(c) Applicability 

(1) This AD applies to hot air balloons, 

certificated in any category, with a Cameron 

Balloons Ltd. Stratus double burner assembly 

part number (P/N) CB8720 or P/N CB8721 

installed. 

(2) The affected burner assemblies may be 

installed on hot air balloon models 

including, but not limited to, those of the 

following design approval holders: 

(i) Aerostar International, Inc.; 

(ii) Ballonbau Worner GmbH; 

(iii) Balo ́ny Kubı ́cˇek spol. s.r.o.; 

(iv) Cameron Balloons Ltd.; 

(v) Eagle Balloons Corp.; 

(vi) JR Aerosports, Ltd (type certificate 

previously held by Sundance Balloons (US)); 

(vii) Lindstrand Balloons Ltd.; and 

(viii) Michael D. McGrath (type certificate 

subsequently transferred to Andrew Philip 

Richardson, Adams Aerostats LLC). 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 7100, Powerplant System. 

(e) Unsafe Condition 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

originated by an aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as suspected 

fatigue cracking of the weld on affected 

burner hangers. The FAA is issuing this AD 

to prevent burners from separating from the 

balloon. The unsafe condition, if not 

addressed, could result in an uncontrolled 

cold descent and hard landing of the balloon. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Definitions 

(1) For purposes of this AD, an ‘‘affected 

part A’’ is a Stratus double burner hanger P/ 

N CB8504, Issue A, Issue B, or Issue C, except 

those installed on a Stratus double burner P/ 

N CB8720 or P/N CB8721 with a doubler 

plate reinforcing the central part of the 

hanger bracket, as shown in figure 2 of 

Cameron Balloons Service Bulletin 28, 

Revision 3, dated February 3, 2021 (Cameron 

Balloons SB28 R3). 

(2) For purposes of this AD, an ‘‘affected 

part B’’ is a Stratus double burner P/N 

CB8720 or P/N CB8721 with a doubler plate 

reinforcing the central part of the hanger 

bracket, as shown in figure 2 of Cameron 

Balloons SB28 R3. 

(3) For purposes of this AD, a ‘‘serviceable 

part’’ is a Stratus double burner hanger P/N 

CB8504, Issue D or later. 

(h) Actions 

(1) Within 10 hours time-in-service (TIS) or 

30 days, whichever occurs first after the 

effective date of this AD, inspect the weld of 

each affected part A for cracks in accordance 

with paragraphs 3.1.2 through 3.1.4 and 

Figure 6 of Cameron Balloons SB28: 


lotter on DSK11XQN23PROD with PROPOSALS1
26702 Federal Register / Vol. 87, No. 87 / Thursday, May 5, 2022 / Proposed Rules 

Accomplishment Instructions CBL/TN/DCB/ 

3191, Issue B, dated February 4, 2020. 

(i) If there are no cracks, repeat the 

inspection in paragraph (h)(1) of this AD at 

intervals not to exceed 12 months. 

(ii) If there is a crack, before further flight, 

remove the affected part A from service and 

install a serviceable part. Installation of a 

serviceable part on a Stratus double burner 

assembly constitutes terminating action for 

the repetitive inspections required by 

paragraph (h)(1) of this AD for that Stratus 

double burner assembly. 

(2) Within 30 days or 10 hours TIS, 

whichever occurs first after the effective date 

of this AD, remove each affected part B from 

service and install a serviceable part. 

(3) As of the effective date of this AD, do 

not install on any hot air balloon an affected 

part A. 

(4) As of the effective date of this AD, do 

not install on any hot air balloon an affected 

part B, unless it is equipped with a 

serviceable part. 

(i) Credit for Previous Actions 

You may take credit for the initial 

inspection required by paragraph (h)(1) of 

this AD if you performed the inspection 

before the effective date of this AD using 

Cameron Balloons Service Bulletin 28, 

Revision 2, dated March 4, 2020; or Revision 

3, dated February 3, 2021. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, 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 local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the certification office, 

send it to the attention of the person 

identified in paragraph (k)(1) of this AD and 

email to: 9-AVS-AIR-730-AMOC@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/ 

certificate holding district office. 

(k) Related Information 

(1) For more information about this AD, 

contact Mike Kiesov, Aviation Safety 

Engineer, General Aviation & Rotorcraft 

Section, International Validation Branch, 

FAA, 901 Locust, Room 301, Kansas City, 

MO 64106; phone: (816) 329–4144; email: 

mike.kiesov@faa.gov. 

(2) Refer to European Union Aviation 

Safety Agency (EASA) AD 2021–0042, dated 

January 29, 2021, for more information. You 

may view the EASA AD at https://

www.regulations.gov in Docket No. FAA– 

2022–0469. 

(3) For service information identified in 

this AD, contact Cameron Balloons Ltd., St. 

Johns Street, Bedminster, Bristol, BS3 4NH, 

United Kingdom; phone: +44 0 117 9637216; 

email: technical@cameronballoons.co.uk; 

website: https://www.cameronballoons.co.uk. 

You may view this service information at the 

FAA, Airworthiness Products Section, 

Operational Safety Branch, 901 Locust, 

Kansas City, MO 64106. For information on 

the availability of this material at the FAA, 

call (817) 222–5110. 

Issued on April 22, 2022. 

Derek Morgan, 

Acting Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–09077 Filed 5–4–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0471; Project 

Identifier MCAI–2021–01219–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) 

2021–22–04, which applies to all Airbus 

SAS Model A318–111, –112, –121, and 

–122 airplanes, Model A319–111, –112, 

–113, –114, –115, –131, –132, and –133 

airplanes, Model A320–211, –212, –214, 

–216, –231, –232, and –233 airplanes, 

and Model A321–111, –112, –131, –211, 

–212, –213, –231, and –232 airplanes. 

AD 2021–22–04 requires a one-time 

eddy current conductivity measurement 

of certain structural parts of the outer 

flaps to determine if the incorrect alloy 

was used, and replacement if necessary; 

and also requires a one-time eddy 

current conductivity measurement of 

certain other structural parts of the outer 

flaps to determine if the parts were 

properly heat treated, and replacement 

if necessary. Since the FAA issued AD 

2021–22–04, typographical errors have 

been identified regarding serial numbers 

of certain suspected parts, and it was 

determined that inconsistent serial 

numbers formats have been used to 

identify certain suspected parts. This 

proposed AD would continue to require 

the actions in AD 2021–22–04, and 

would require using an updated list of 

suspected parts, as specified in a 

European Union Aviation Safety Agency 

(EASA) AD, which is proposed for 

incorporation by reference. This 

proposed AD would also limit the 

installation of affected parts. 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 June 20, 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–2022–0471. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0471; 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; 

phone 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–2022–0471; Project Identifier 

MCAI–2021–01219–T’’ at the beginning 

of your comments. The most helpful 

comments reference a specific portion of 


lotter on DSK11XQN23PROD with PROPOSALS1