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Federal Register / Vol. 86, No. 139 / Friday, July 23, 2021 / Rules and Regulations 3 If, during the maintenance records review required by paragraph g1 of the this AD or during the inspection required by paragraph g2 of this AD, you can positively determine that a disc assembly P/
N 1015841 or 2 is not installed, before further flight, make an entry in the log book showing compliance with this AD.
4 If, during the maintenance records review required by paragraph g1 of this AD or during the inspection required by paragraph g2 of this AD, you can positively determine that a disc assembly P/
N 1015841 or 2 is installed, within 30 days or 100 hours TIS after the effective date of this AD, whichever occurs first, replace disc assembly P/N 1015841 or 2 with disc assembly P/N 327211.

Canada Limited, 12,800 Rue de lAvenir, Mirabel, Quebec J7J1R4; phone: 450437
2862 or 8003638023; fax: 450 4330272;
internet: https www.bellcustomer.com.
4 You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 817 2225110.
5 You may view this service information that is incorporated by reference at the National Archives and Records Administration NARA. For information on the availability of this material at NARA, email: fedreg.legal@nara.gov, or go to:
https www.archives.gov/federal-register/cfr/
ibr-locations.html.

h Parts Installation Prohibition As of the effective date of this AD, do not install disc assembly P/N 1015841 or 2.

Issued on July 9, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.

i 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 International Validation Branch, send it to the attention of the person identified in paragraph j1 of this AD.
Information may be emailed to: 9-AVS-AIR730-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.

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j Related Information 1 For more information about this AD, contact Kathleen Arrigotti, Program Manager, Large Aircraft Section, International Validation Branch, Compliance &
Airworthiness Division, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206 2313218; email:
kathleen.arrigotti@faa.gov.
2 The subject of this AD is addressed in Transport Canada Civil Aviation TCCA
Canadian AD CF201007, dated February 24, 2010. You may view the TCCA AD at https www.regulations.gov in Docket No.
FAA20100865.
k Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552a and 1 CFR
part 51.
2 You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
i Bell Helicopter Alert Service Bulletin 20609123, Revision A, dated June 10, 2009.
ii Bell Helicopter Alert Service Bulletin 206L09157, Revision A, dated June 10, 2009.
3 For service information identified in this AD, contact Bell Helicopter Textron
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FR Doc. 202115478 Filed 72221; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210188; Project Identifier MCAI202000642R; Amendment 3921572; AD 20211110
RIN 2120AA64

Airworthiness Directives; Airbus Helicopters Federal Aviation Administration FAA, DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Airbus Helicopters Model SA365N, SA365N1, AS365N2, and AS 365 N3
helicopters. This AD was prompted by a report that damage scorch marks was found on an internal life raft installation that contained a half rescue kit. This AD
requires identifying the part number and serial number of each half rescue kit located in the internal life raft installation and, depending on the findings, inspecting the life raft for damage, inspecting the condition of the flashlight battery, testing the flashlight battery, and replacing the life raft or flashlight battery including the leak test as applicable, as specified in a European Aviation Safety Agency now European Union Aviation Safety Agency EASA AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective August 27, 2021.
SUMMARY:

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The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD
as of August 27, 2021.
ADDRESSES: For EASA material incorporated by reference IBR in this AD, contact the EASA, KonradAdenauer-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. For Zodiac Aerospace service information identified in this final rule, contact Safran AerosystemsPlaisir, 61 rue Pierre Curie CS20001, 78373 Plaisir Cedex, France; telephone 33 1 61 34 23
23; fax 33 1 61 34 24 41; or at https
www.safran-aerosystems.com. You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 8172225110.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0188.
Examining the AD Docket You may examine the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0188; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
The AD docket contains this final rule, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT:
Kathleen Arrigotti, Program Manager, Large Aircraft Section, International Validation Branch, Compliance &
Airworthiness Division, FAA, 2200
South 216th St., Des Moines, WA 98198;
telephone and fax 2062313218; email kathleen.arrigotti@faa.gov.
SUPPLEMENTARY INFORMATION:
Background The EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD
20160028, dated February 15, 2016
EASA AD 20160028 also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI, to correct an unsafe condition for certain Airbus Helicopters Model
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