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Federal Register / Vol. 86, No. 120 / Friday, June 25, 2021 / Rules and Regulations Regulatory Findings The FAA determined that this AD
would not have federalism implications under Executive Order 13132. This 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 regulation:
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:
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

Authority: 49 U.S.C. 106g, 40113, 44701.
39.13

Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:

20211321 Leonardo S.p.a.: Amendment 3921627; Docket No. FAA20210512;
Project Identifier MCAI202001621R.
a Effective Date This airworthiness directive AD becomes effective July 12, 2021.
b Affected ADs None.
c Applicability This AD applies to Leonardo S.p.a. Model AB139, AW139, and AW189 helicopters, certificated in any category, equipped with a main rotor swashplate boot, having part number P/N 3G6230V00251.

lotter on DSK11XQN23PROD with RULES1

d Subject Joint Aircraft System Component JASC
Code 6230 Main Rotor Mast/Swashplate.
e Unsafe Condition This AD was prompted by a report of the in-flight failure of one of the three stainless steel external rings bonded to the main rotor swashplate boot. The FAA is issuing this AD
to address corrosion, cracking, and damage to the adhesive e.g., disbonding of any stainless steel external ring bonded to the main rotor swashplate boot, which could result in release of a ring from the main rotor
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swashplate boot, resulting in damage to, and reduced control of, the helicopter.

telephone 516 2287323; email Darren.Gassetto@faa.gov.

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

k 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 Union Aviation Safety Agency EASA AD 20200271, dated December 8, 2020.
ii Reserved 3 For EASA AD 20200271, 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 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 on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA20210512.
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 fedreg.legal@
nara.gov, or go to https www.archives.gov/
federal-register/cfr/ibr-locations.html.

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, European Union Aviation Safety Agency EASA AD 20200271, dated December 8, 2020 EASA AD 20200271.
h Exceptions to EASA AD 20200271
1 Where EASA AD 20200271 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20200271 does not apply to this AD.
3 Where EASA AD 20200271 refers to flight hours FH, this AD requires using hours time-in-service.
4 Where paragraphs 3 and 6 of EASA
AD 20200271 refer to any discrepancy or discrepancies, for this AD, discrepancies include corrosion including superficial oxidation and cracking.
5 Where paragraph 4 of EASA AD 2020
0271 refers to any discrepancy, for this AD, discrepancies include corrosion including superficial oxidation, cracking, and damage to the adhesive e.g., disbonding.
6 Paragraph 6 of EASA AD 20200271
specifies to report inspection results to Leonardo S.p.a. within a certain compliance time. For this AD, report inspection results at the applicable time specified in paragraph h6i 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 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 j 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.
j Related Information For more information about this AD, contact Darren Gassetto, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590;

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Issued on June 18, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202113668 Filed 62321; 11:15 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 97
Docket No. 31373; Amdt. No. 3959

Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures;
Miscellaneous Amendments Federal Aviation Administration FAA, DOT.
ACTION: Final rule.
AGENCY:

This rule establishes, amends, suspends, or removes Standard Instrument Approach Procedures SIAPS and associated Takeoff Minimums and Obstacle Departure procedures ODPs for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or
SUMMARY:

E:FRFM25JNR1.SGM

25JNR1