Federal Register / Vol. 85, No. 238 / Thursday, December 10, 2020 / Proposed Rules 79435 

‘‘Implementation of Quality Assurance 

Criteria and 10 CFR 50.59 for Nuclear 

Power Plant Components Produced 

Using Advanced Manufacturing 

Technologies’’ (ADAMS Accession No. 

ML20317A007). 

III. Background 

The NRC considers AMTs to consist 

of material processing and component 

fabrication methods that have not been 

traditionally used in the U.S. nuclear 

industry and have not yet received NRC 

approval through NRC-endorsed codes 

and standards or the approval of an 

industry submittal. There are several 

regulatory paths available to a licensee 

for utilizing an AMT in a nuclear 

application, including: (1) Development 

of a Code or Standard that can be 

incorporated by reference in section 

50.55a of chapter I of title 10 of the Code 

of Federal Regulations (10 CFR); (2) 

selection of an unregulated in-service 

application; (3) submission of generic 

technical reports or plant-specific 

submittals for NRC approval; or (4) 

implementation of the 10 CFR 50.59, 

‘‘Changes, tests and experiments,’’ 10 

CFR 70.72, ‘‘Facility changes and 

change process,’’ or 10 CFR 72.48, 

‘‘Changes, tests, and experiments’’ 

processes. Industry indicated that plans 

for the initial installation of AMTfabricated components would involve 

the 10 CFR 50.59 process. Therefore, the 

NRC staff documented in the draft 

document a description of the 

processes, consistent with the QA 

requirements in Appendix B to 10 CFR 

part 50 and in accordance with 10 CFR 

50.59 in order to support the staff’s 

performance of potential inspections of 

a licensee’s implementation of these 

requirements for AMT-fabricated 

components. 

IV. Specific Considerations 

This report documents completion of 

the staff’s initial review of QA criteria 

and 10 CFR 50.59 requirements for AMT 

applications at U.S. nuclear power 

plants. This report does not represent a 

complete and final analysis of all 

aspects of QA criteria and 10 CFR 50.59 

requirements and guidance that might 

be applicable to the use of AMT 

components at U.S. nuclear power 

plants. This report does not create new 

regulatory requirements or establish 

new regulatory positions with respect to 

the use or manufacture of AMT 

components for nuclear power plants. 

The scope of this report is limited to the 

review of existing requirements and 

guidance to address AMT components 

and the consideration of potential 

regulatory and technical challenges. 

This report may be subject to future 

revision, as additional insights and 

operating experience for use of AMT 

components are gained. 

In its effort to be open and transparent 

regarding potential processes for the 

installation of AMT-fabricated 

components, the NRC is requesting 

general comments on this document. 

V. Public Meeting 

The NRC plans to hold a public 

meeting during the public comment 

period for this action. A public meeting 

is planned for January 2021, via online 

webinar. The public webinar will 

provide a forum for the NRC staff to 

discuss the document and for members 

of the public to provide comments on 

the document. The NRC does not intend 

to provide any responses to comments 

submitted during the public webinar. 

The public webinar will be noticed on 

the NRC’s public meeting website at 

least 10 calendar days before the 

meeting. Members of the public should 

monitor the NRC’s public meeting 

website for additional information about 

the public webinar at https:// 

www.nrc.gov/public-involve/publicmeetings/index.cfm. The NRC will post 

the notice for the public webinar and 

may post additional material related to 

this action to the Federal Rulemaking 

website at https://www.regulations.gov/ 

under Docket ID NRC–2020–0253. The 

Federal Rulemaking website allows you 

to receive alerts when changes or 

additions occur in a docket folder. To 

subscribe: (1) Navigate to the docket 

folder (NRC–2020–0253); (2) click the 

‘‘Sign up for Email Alerts’’ link; and (3) 

enter your email address and select how 

frequently you would like to receive 

emails (daily, weekly, or monthly). 

Dated: December 2, 2020. 

For the Nuclear Regulatory Commission. 

Anna H. Bradford, 

Director, Division of New and Renewed 

Licenses, Office of Nuclear Reactor 

Regulation. 

[FR Doc. 2020–26845 Filed 12–9–20; 8:45 am] 

BILLING CODE 7590–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1114; Project 

Identifier 2019–SW–058–AD] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Helicopters 

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 Airbus Helicopters Model 

EC120B helicopters. This proposed AD 

was prompted by a report of broken and 

bent attachment bolts of the main rotor 

(MR) hub scissors assembly. This 

proposed AD would require an 

inspection of the attachment bolts of the 

MR hub scissors assembly for 

discrepancies and repair if necessary; 

part marking of the attachment bolts of 

the MR hub scissors assembly; and 

repetitive inspections of the part 

marking of the attachment bolts, and 

repair if necessary; as specified in a 

European Union Aviation Safety Agency 

(EASA) AD, which will be incorporated 

by reference. 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 January 25, 

2021. 

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 incorporated by reference 

(IBR) in this AD, contact the EASA, 

Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; telephone +49 221 

89990 000; email ADs@easa.europa.eu; 

internet www.easa.europa.eu. You may 

find this IBR material on the EASA 

website at https://ad.easa.europa.eu. 

You may view this IBR material at the 

FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood 

Pkwy., Room 6N–321, Fort Worth, TX 

76177. For information on the 

availability of this material at the FAA, 

call 817–222–5110. It is also available in 

the AD docket on the internet at https:// 

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

1114. 

Examining the AD Docket 

You may examine the AD docket on 

the internet at https://

www.regulations.gov by searching for 


jbell on DSKJLSW7X2PROD with PROPOSALS
79436 Federal Register / Vol. 85, No. 238 / Thursday, December 10, 2020 / Proposed Rules 

and locating Docket No. FAA–2020– 

1114; 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. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: Hal 

Jensen, Aerospace Engineer, Operational 

Safety Branch, FAA, 470 L’Enfant Plaza 

SW, Washington, DC 20024; telephone 

202–267–9167; email hal.jensen@

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–2020–1114; Project Identifier 

2019–SW–058–AD’’ 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 proposal. 

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 Hal Jensen, Aerospace 

Engineer, Operational Safety Branch, 

FAA, 470 L’Enfant Plaza SW, 

Washington, DC 20024; telephone 202– 

267–9167; email hal.jensen@faa.gov. 

Any commentary that the FAA receives 

that is not specifically designated as CBI 

will be placed in the public docket for 

this rulemaking. 

Discussion 

The EASA, which is the Technical 

Agent for the Member States of the 

European Union, has issued EASA AD 

2019–0139, dated June 12, 2019 (EASA 

AD 2019–0139) (also referred to as the 

Mandatory Continuing Airworthiness 

Information, or the MCAI), to correct an 

unsafe condition for all Airbus 

Helicopters Model EC120B helicopters. 

This proposed AD was prompted by 

a report of broken and bent attachment 

bolts of the MR hub scissors assembly. 

The FAA is proposing this AD to 

address broken and bent attachment 

bolts of the MR hub scissors assembly, 

which could lead to detachment of a MR 

hub scissors attachment bolt, possibly 

resulting in complete loss of control of 

the helicopter. See the MCAI for 

additional background information. 

Related Service Information Under 1 

CFR Part 51 

EASA AD 2019–0139 describes 

procedures for an inspection of the 

attachment bolts of the MR hub scissors 

assembly for discrepancies 

(discrepancies include corrosion, 

fretting, wear, cracking, bolt play, and 

bolt tightening torque); and repair if 

necessary; part marking of the 

attachment bolts of the MR hub scissors 

assembly; and repetitive inspections, 

after part marking, of the attachment 

bolts for discrepancies, and repair if 

necessary. The inspections of the 

attachment bolts of the MR hub 

assembly include checking the play and 

torque of the scissors attachment bolts 

and making sure that there are no hard 

spots in the scissors link hinge. 

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 and Requirements 

of This Proposed AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to the 

bilateral agreement with the State of 

Design Authority, the FAA has been 

notified of the unsafe condition 

described in the MCAI 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 

in other products of the same type 

design. 

Proposed AD Requirements 

This proposed AD would require 

accomplishing the actions specified in 

EASA AD 2019–0139, described 

previously, as incorporated by 

reference, except for any differences 

identified as exceptions in the 

regulatory text of this AD. 

Explanation of Required Compliance 

Information 

In the FAA’s ongoing efforts to 

improve the efficiency of the AD 

process, the FAA initially worked with 

Airbus and EASA to develop a process 

to use certain EASA ADs as the primary 

source of information for compliance 

with requirements for corresponding 

FAA ADs. The FAA has since 

coordinated with other manufacturers 

and civil aviation authorities (CAAs) to 

use this process. As a result, EASA AD 

2019–0139 will be incorporated by 

reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2019–0139 

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 

the EASA AD 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 the EASA AD. Service 

information specified in EASA AD 

2019–0139 that is required for 

compliance with EASA AD 2019–0139 

will be available on the internet at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2020–1114 after the FAA final 

rule is published. 

Costs of Compliance 

The FAA estimates that this proposed 

AD affects 160 helicopters of U.S. 

registry. The FAA estimates the 

following costs to comply with this 

proposed AD: 


jbell on DSKJLSW7X2PROD with PROPOSALS
Federal Register / Vol. 85, No. 238 / Thursday, December 10, 2020 / Proposed Rules 79437 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

5 work-hours × $85 per hour = $425 .......................................................................................... $0 $425 $68,000 

The FAA estimates that it would take 

about 1 hour per product to comply 

with the proposed reporting 

requirement in this proposed AD. The 

average labor rate is $85 per hour. Based 

on these figures, the FAA estimates the 

cost of reporting on U.S. operators to be 

$13,600, or $85 per product. 

The FAA estimates the following 

costs to do any necessary on-condition 

actions that would be required based on 

the results of any required actions. The 

FAA has no way of determining the 

number of helicopters that might need 

these on-condition actions: 

ESTIMATED COSTS OF ON-CONDITION ACTIONS

Labor cost Parts cost Cost per 

product 

4 work-hours × $85 per hour = $340 ...................................................................................................................... $40 $380 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a current valid 

OMB control number. The control 

number for the collection of information 

required by this proposed AD is 2120– 

0056. The paperwork cost associated 

with this proposed AD has been 

detailed in the Costs of Compliance 

section of this document and includes 

time for reviewing instructions, as well 

as completing and reviewing the 

collection of information. Therefore, all 

reporting associated with this proposed 

AD is mandatory. Comments concerning 

the accuracy of this burden and 

suggestions for reducing the burden 

should be directed to Information 

Collection Clearance Officer, Federal 

Aviation Administration, 10101 

Hillwood Parkway, Fort Worth, TX 

76177–1524. 

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) Will not affect intrastate aviation 

in Alaska, and 

(3) Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

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: 

Airbus Helicopters: Docket No. FAA–2020– 

1114; Project Identifier 2019–SW–058– 

AD. 

(a) Comments Due Date 

The FAA must receive comments by 

January 25, 2021. 

(b) Affected Airworthiness Directives (ADs) 

None. 

(c) Applicability 

This AD applies to Airbus Helicopters 

Model EC120B helicopters, certificated in 

any category, having an affected part as 

defined in European Union Aviation Safety 

Agency (EASA) AD 2019–0139, dated June 

12, 2019 (EASA AD 2019–0139). 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 6200, Main Rotor System. 

(e) Reason 

This AD was prompted by a report of 

broken and bent attachment bolts of the main 

rotor (MR) hub scissors assembly. The FAA 

is issuing this AD to address broken and bent 

attachment bolts of the MR hub scissors 

assembly, which could lead to detachment of 

a MR hub scissors attachment bolt, possibly 

resulting in complete loss of control of the 

helicopter. 

(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, EASA AD 2019–0139. 


jbell on DSKJLSW7X2PROD with PROPOSALS
79438 Federal Register / Vol. 85, No. 238 / Thursday, December 10, 2020 / Proposed Rules 

(h) Exceptions to EASA AD 2019–0139 

(1) Where EASA AD 2019–0139 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

(2) Where EASA AD 2019–0139 refers to 

September 5, 2018 (the effective date of 

EASA AD 2018–0186, dated August 29, 

2018), this AD requires using the effective 

date of this AD. 

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

2019–0139 does not apply to this AD. 

(4) Where EASA AD 2019–0139 refers to 

flight hours (FH), this AD requires using 

hours time-in-service. 

(5) Paragraphs (3) and (4) of EASA AD 

2019–0139 refer to ‘‘discrepancies.’’ For this 

AD, discrepancies include corrosion, fretting, 

wear, cracking, bolt play, and bolt tightening 

torque. 

(6) Although the service information 

referenced in EASA AD 2019–0139 specifies 

to discard certain parts, this AD does not 

include that requirement. 

(7) Where EASA AD 2019–0139 specifies 

to contact the manufacturer for repair 

instructions, repair using a method approved 

by the Manager, Rotorcraft Standards Branch, 

FAA. For a repair method to be approved by 

the Manager, Rotorcraft Standards Branch, as 

required by this paragraph, the Manager’s 

approval letter must specifically refer to this 

AD. 

(8) Paragraph (5) of EASA AD 2019–0139 

specifies to report inspection results to 

Airbus Helicopters within a certain 

compliance time. For this AD, report 

inspection results at the applicable time 

specified in paragraph (h)(8)(i) or (ii) of this 

AD. 

(i) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 30 days after the inspection. 

(ii) If the inspection was done before the 

effective date of this AD: Submit the report 

within 30 days after the effective date of this 

AD. 

(i) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Rotorcraft Standards Branch, 

FAA, may approve AMOCs for this AD. Send 

your proposal to: Manager, Rotorcraft 

Standards Branch, FAA, 10101 Hillwood 

Pkwy, Fort Worth, TX 76177; phone: 817– 

222–5110; email: 9-ASW-FTW-AMOCRequests@faa.gov. 

(j) Paperwork Reduction Act Burden 

Statement 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject to 

a penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork Reduction 

Act unless that collection of information 

displays a current valid OMB Control 

Number. The OMB Control Number for this 

information collection is 2120–0056. Public 

reporting for this collection of information is 

estimated to be approximately 1 hour per 

response, including the time for reviewing 

instructions, searching existing data sources, 

gathering and maintaining the data needed, 

and completing and reviewing the collection 

of information. All responses to this 

collection of information are mandatory as 

required by this AD. Send comments 

regarding this burden estimate or any other 

aspect of this collection of information, 

including suggestions for reducing this 

burden to Information Collection Clearance 

Officer, Federal Aviation Administration, 

10101 Hillwood Parkway, Fort Worth, TX 

76177–1524. 

(k) Related Information 

(1) For EASA AD 2019–0139, contact the 

EASA, Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; telephone +49 221 89990 

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, Office of the Regional 

Counsel, Southwest Region, 10101 Hillwood 

Pkwy, Room 6N–321, Fort Worth, TX 76177. 

For information on the availability of this 

material at the FAA, call 817–222–5110. This 

material may be found in the AD docket on 

the internet at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2020–1114. 

(2) For more information about this AD, 

contact Hal Jensen, Aerospace Engineer, 

Operational Safety Branch, FAA, 470 

L’Enfant Plaza SW, Washington, DC 20024; 

telephone 202–267–9167; email hal.jensen@

faa.gov. 

Issued on December 2, 2020. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2020–26965 Filed 12–9–20; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1118; Project 

Identifier MCAI–2020–00516–E] 

RIN 2120–AA64 

Airworthiness Directives; Safran 

Helicopter Engines, S.A. (Type 

Certificate Previously Held by 

Turbomeca, S.A.) Turboshaft Engines 

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 

Safran Helicopter Engines, S.A. Arriel 

2C, 2C1, 2S1, and 2S2 model turboshaft 

engines. This proposed AD was 

prompted by investigations by the 

manufacturer following level 1 failures 

in flight (minor anomalies) and level 2 

failures on the ground (minor failures), 

where cracks were found on the 

soldered joints of torque conformation 

boxes. This proposed AD would require 

performing initial and repetitive 

inspections of the resistance values of 

the torque conformation box and, 

depending on the results of the 

inspections, replacement of the torque 

conformation box. 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 January 25, 

2021. 

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 Safran Helicopter 

Engines, S.A., Avenue du 1er Mai, 

Tarnos, France; phone: +33 (0) 5 59 74 

45 11. You may view this service 

information at the FAA, Airworthiness 

Products Section, Operational Safety 

Branch, 1200 District Avenue, 

Burlington, MA 01803. For information 

on the availability of this material at the 

FAA, call (781) 238–7759. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2020–1118; 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: 

Wego Wang, Aviation Safety Engineer, 

ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: 

(781) 238–7134; fax: (781) 238–7199; 

email: wego.wang@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. 


jbell on DSKJLSW7X2PROD with PROPOSALS