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Federal Register / Vol. 86, No. 184 / Monday, September 27, 2021 / Rules and Regulations 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.
k Related Information For more information about this AD, contact Hal Jensen, Aerospace Engineer, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 LEnfant Plaza N SW, Washington, DC 20024;
telephone 2022679167; email hal.jensen@
faa.gov.
l Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference IBR 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 this AD specifies otherwise.
i European Aviation Safety Agency EASA AD 20180002, dated January 4, 2018.
ii Reserved 3 For EASA AD 20180002, contact the 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.
4 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 8172225110. This material may be found in the AD docket on the internet at https www.regulations.gov by searching for and locating Docket No. FAA20210505.
5 You may view this material that is incorporated by reference at the National Archives and Records Administration NARA. For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on August 30, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202120825 Filed 92421; 8:45 am
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210785; Project Identifier AD202100989R; Amendment 3921734; AD 20211916
RIN 2120AA64

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

The FAA is superseding Airworthiness Directive AD 202116
02, which applied to certain Airbus Helicopters Model SA330J, AS332C, AS332L, AS332L1, AS332L2, and EC225LP helicopters. AD 20211602
required inspecting the locking safety mechanism of the left-hand LH side stairway door handle and depending on the results, corrective action. AD 2021
1602 also required modifying that locking safety mechanism. This AD
retains the requirements in AD 2021
1602, as specified in a European Union Aviation Safety Agency EASA AD, which is incorporated by reference, and clarifies a certain exception. This AD
was prompted by the need to clarify that exception. The FAA is issuing this AD
to address the unsafe condition on these products.
DATES: This AD becomes effective October 12, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of September 24, 2021 86 FR 46771.
The FAA must receive comments on this AD by November 12, 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 4932251.
Mail: U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 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
SUMMARY:

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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, 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 817 222
5110. It is also available in the AD
docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210785.
Examining the AD Docket You may examine the AD docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210785; 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 AD, 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, 950 LEnfant Plaza N SW, Washington, DC 20024;
telephone 202 2679167; email hal.jensen@faa.gov.
SUPPLEMENTARY INFORMATION:
Background The FAA issued AD 20211602, Amendment 3921663 86 FR 46771, August 20, 2021 AD 20211602, for certain Airbus Helicopters Model SA330J, AS332C, AS332L, AS332L1, AS332L2, and EC225LP helicopters. AD
20211602 required inspecting the locking safety mechanism of the LH side stairway door handle and depending on the results, corrective action. AD 2021
1602 also required modifying that locking safety mechanism.
AD 20211602 was prompted by EASA AD 20200087, dated April 15, 2020 EASA AD 20200087, issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Airbus Helicopters AH, formerly Eurocopter, Eurocopter France, Aerospatiale, Sud Aviation, Model SA330J, AS332C, AS332L, AS332L1, AS332L2, and EC225LP helicopters, if equipped with an LH side stairway door, except helicopters modified in accordance with AH modification MOD 07 28281 AS 332, EC 225 or MOD 07 27338 SA 330. EASA issued EASA AD 20200087 to supersede EASA Emergency AD 20140241E, dated November 4, 2014 EASA AD
20140241E.

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