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Federal Register / Vol. 86, No. 184 / Monday, September 27, 2021 / Rules and Regulations
to discard certain parts, this AD requires removing those parts from service.
5 While paragraph 2 of EASA AD 2020
0087 requires actions before next flight after each application of painting on the LH side stairway door or its external door handle, those actions are not required by this AD.
6 Where paragraph 3 of EASA AD 2020
0087 requires reconditioning the locking safety mechanism, and the service information referenced in paragraph 3 of EASA AD 20200087 specifies contacting the Airbus Helicopters Support and Services Department if it is impossible to recondition the locking safety mechanism by moving the door handle, this AD requires moving the external door handle from the Locked to the Unlocked position to determine if the safety mechanism can lock automatically. If the safety mechanism does not lock automatically, this AD requires, before further flight accomplishing paragraph 5 of EASA AD 20200087 or accomplishing corrective action using a method approved by the Manager, International Validation Branch, FAA. The Managers approval letter must specifically refer to this AD.
7 Where paragraph 5 of EASA AD 2020
0087 identifies the modification as required by paragraph 4 of EASA AD 20200087 as terminating action for the repetitive inspections as required by paragraph 2 of EASA AD 20200087 for that helicopter, the terminating action for the repetitive inspections as required by paragraph 2 of EASA AD 20200087 does not apply to this AD.
8 This AD does not mandate compliance with the Remarks section of EASA AD
20200087.
i No Reporting Requirement Although the service information referenced in EASA AD 20200087 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

lotter on DSK11XQN23PROD with RULES1

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 International Validation Branch, send it to the attention of the person identified in paragraph k 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.
k Related Information For more information about this AD, 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.

VerDate Sep<11>2014

16:20 Sep 24, 2021

Jkt 253001

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.
3 The following service information was approved for IBR on September 24, 2021 86
FR 46771.
i European Union Aviation Safety Agency EASA AD 20200087, dated April 15, 2020.
ii Reserved 4 For EASA AD 20200087, 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.
5 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.
This material may be found in the AD docket at https www.regulations.gov by searching for and locating FAA20210785.
6 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 September 8, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202120464 Filed 92421; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210723; Project Identifier MCAI202000268R; Amendment 3921716; AD 20211815
RIN 2120AA64

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

The FAA is adopting a new airworthiness directive AD for certain PZL Swidnik S.A. Model PZL W3A
helicopters. This AD was prompted by a report that displaced teeth were detected on the moveable assemblies of a main rotor MR blade droop stop.

SUMMARY:

Frm 00016

Fmt 4700

This AD becomes effective October 12, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD
as of October 12, 2021.
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, M30, 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 service information identified in this final rule, contact WSK PZLSwidnik S.A., Al. Lotnikow Polskich 1, 21045 Swidnik, Poland; telephone +48 81722 5716; fax +48 81722 5625;
email: PL-CustomerSupport.AW@
leonardocompany.com; or at https
www.pzlswidnik.pl/en/home. 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. It is also available at https www.regulations.gov by searching for and locating Docket No.
FAA20210723.
DATES:

Examining the AD Docket
Airworthiness Directives; PZL Swidnik S.A. Helicopters
PO 00000

This AD requires removing from service the moveable assemblies from each affected MR blade droop stop and prohibits installation of an affected MR
blade droop stop and moveable assemblies of affected MR blade droop stops. The FAA is issuing this AD to address the unsafe condition on these products.

Sfmt 4700

You may examine the AD docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210723; 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, the European Union Aviation Safety Agency EASA AD, any comments received, and other information. The street address for Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT:
Andrea Jimenez, Aerospace Engineer,
E:FRFM27SER1.SGM

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