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Federal Register / Vol. 86, No. 159 / Friday, August 20, 2021 / Rules and Regulations 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, I certify that this AD:
1 Is not a significant regulatory action under Executive Order 12866, and 2 Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

1. The authority citation for part 39
continues to read as follows:

Authority: 49 U.S.C. 106g, 40113, 44701.
Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:

20211713 PZL Swidnik S.A.:
Amendment 3921696; Docket No.
FAA20210683; Project Identifier MCAI202000614R.
a Effective Date This airworthiness directive AD is effective September 7, 2021.

c Applicability This AD applies to PZL Swidnik S.A.
Model PZL W3A helicopters, certificated in any category, with a rescue hoist installed.

khammond on DSKJM1Z7X2PROD with RULES

d Subject Joint Aircraft Service Component JASC
Code: 3201, Landing Gear/Wheel Fairing.
e Unsafe Condition This AD was prompted by a report of a damaged wheel braking system pneumatic line fitting installed on the left-hand LH
main landing gear MLG leg. The FAA is issuing this AD to prevent damage to MLG
pneumatic wheel braking system. The unsafe condition, if not addressed, could result in loss of MLG wheel braking capability, and subsequent loss of control of the helicopter during a roll-on landing.

VerDate Sep<11>2014

16:42 Aug 19, 2021

Jkt 253001

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 i1 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.
i Related Information
b Affected ADs None.

f Compliance Comply with this AD within the compliance times specified, unless already done.

1 Within 30 days after the effective date of this AD, modify the LH MLG leg by installing shield assembly part number P/N
37.96.204.00.00.
Note 1 to paragraph g1: A sketch of the installation of shield P/N 37.96.204.01.00
and clamps P/N MS2192035, which together constitute shield assembly P/N
37.96.204.00.00, is available in Attachment 1, RNIA SPRZETU
of WYTWO
KOMUNIKACYJNEGO PZL-Swidnik Spo5ka Akcyjna Mandatory Bulletin No. BO
3718301, dated December 10, 2018.
2 As of the effective date of this AD, do not install a rescue hoist unless the action required by paragraph g1 of this AD has been accomplished concurrently with the rescue hoist installation or within 30 days after the effective date of this AD, whichever occurs later.
h Alternative Methods of Compliance AMOCs
PART 39AIRWORTHINESS
DIRECTIVES

39.13

g Required Actions
1 For more information about this AD, contact Fred Guerin, Aerospace Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 2200 S
216th St., Des Moines, WA 98198; telephone 202 2677457; email 9-ANM-Seattle-ACOAMOC-Requests@faa.gov.
2 For service information identified in this AD, contact WSK PZL-Swidnik S.A., Al. Lotnikow Polskich 1, 21045 Swidnik, Poland; telephone +48 81722 5716; fax +48 81722 5625; email: PLCustomerSupport.AW@
leonardocompany.com; or at https
www.pzlswidnik.pl/en/home. You may view this referenced 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.
3 The subject of this AD is addressed in European Aviation Safety Agency now European Union Aviation Safety Agency EASA AD 20180274, dated December 13, 2018. You may view the EASA AD at https
www.regulations.gov in Docket No. FAA
20210683.

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46771

Issued on August 12, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202117838 Filed 81921; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210374; Project Identifier MCAI202000543R; Amendment 3921663; AD 20211602
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 SA330J, AS332C, AS332L, AS332L1, AS332L2, and EC225LP helicopters. This AD was prompted by a report of a left-hand LH
side stairway door that inadvertently opened in flight and tore off from its attachment fittings. This AD requires inspecting the locking safety mechanism of the LH side stairway door handle and depending on the results, corrective action. This AD also requires modifying that locking safety mechanism as specified in a 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 September 24, 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.
ADDRESSES: For material incorporated by reference IBR in this AD, 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 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 2225110. It is also available in the AD docket on the internet at https www.regulations.gov by searching for and locating Docket No.
FAA20210374.
SUMMARY:

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