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Federal Register / Vol. 86, No. 28 / Friday, February 12, 2021 / Rules and Regulations matters requiring board attention, documents of resolution, and supervisory recommendations a supervised financial institution for, and the Bureau will not issue an enforcement action on the basis of, a violation of or non-compliance with supervisory guidance. In some situations, examiners may reference including in writing supervisory guidance to provide examples of appropriate consumer protection and risk management practices and other actions for addressing compliance with laws or regulations.
Supervisory criticisms should continue to be specific as to practices, operations or other matters that could cause consumer harm or could cause violations of laws, regulations, final agency orders, or other legally enforceable conditions.
The Bureau may decide to seek public comment on supervisory guidance. Seeking public comment on supervisory guidance does not mean that the guidance is intended to be a regulation or have the force and effect of law. The comment process helps the Bureau to improve its understanding of an issue, to gather information on institutions risk management practices, or to seek ways to achieve a supervisory objective most effectively and with the least burden on institutions.
The Bureau will aim to reduce the issuance of multiple supervisory guidance documents on the same topic and will generally limit such multiple issuances going forward.
The Bureau will continue efforts to make the role of supervisory guidance clear in communications to examiners and to supervised financial institutions and encourages supervised institutions with questions about this statement or any applicable supervisory guidance to discuss the questions with their appropriate agency contact.
Dated: January 19, 2021.
Grace Feola, Federal Register Liaison, Bureau of Consumer Financial Protection.
FR Doc. 202101524 Filed 21121; 8:45 am BILLING CODE 4810AMP

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210027; Project Identifier MCAI202100048R; Amendment 3921425; AD 20210404
RIN 2120AA64

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

Examining the AD Docket
The FAA is superseding Airworthiness Directive AD 202019

SUMMARY:

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02, which applied to certain Airbus Helicopters previously Eurocopter France Model SA330J helicopters. AD
20201902 required repetitively inspecting affected tail rotor T/R
blades and depending on the inspection results, repairing or replacing the T/R
blade. AD 20201902 also prohibited installing an affected T/R blade unless it passed the inspections. This AD
retains the requirements of AD 2020
1902 and also clarifies the applicability, clarifies the affected T/R
blades in the required actions, reduces a compliance time, and corrects the prohibition requirement. This AD was prompted by the determination that these corrections are necessary. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD becomes effective March 1, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD
as of October 7, 2020 85 FR 59416, September 22, 2020.
The FAA must receive comments on this AD by March 29, 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 service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone 972641
0000 or 8002320323; fax 972641
3775; or at https www.airbus.com/
helicopters/services/technicalsupport.html. 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.
FAA20210027.
You may examine the AD docket at https www.regulations.gov by searching for and locating Docket No.

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FAA20210027; 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 Aviation Safety Agency now European Union Aviation Safety Agency EASA AD, any comments received, and other information. The street address for Docket Operations is listed above.
Matt Fuller, AD Program Manager, General Aviation & Rotorcraft Unit, Airworthiness Products Section, Operational Safety Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone 817 2225110; email matthew.fuller@faa.gov.

FOR FURTHER INFORMATION CONTACT:

SUPPLEMENTARY INFORMATION:

Background The FAA issued AD 20201902, Amendment 3921243 85 FR 59416, September 22, 2020 AD 20201902, for certain Airbus Helicopters previously Eurocopter France Model SA330J helicopters. AD 20201902
required, for each T/R blade part number P/N 330A120005all dash numbers and 330A120006all dash numbers, repetitively accomplishing a visual and in-depth inspection for debonding and eddy current inspecting for a crack. If there was debonding within allowable limits, AD 20201902
required repairing or replacing the T/R
blade. If there was debonding that exceeded allowable limits or a crack, AD 20201902 required replacing the T/R blade. AD 20201902 also prohibited installing an affected T/R
blade unless it passed the inspections.
AD 20201902 was prompted by EASA
AD No. 20160059E, dated March 22, 2016 EASA AD 20160059E, issued by the EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Airbus Helicopters formerly Eurocopter, Eurocopter France, Aerospatiale Model SA 330 J
helicopters. EASA AD 20160059E
retains the requirements of Direction Generale de lAviation Civile DGAC
France AD 87032052BR3, dated January 23, 1991, which it supersedes, and also mandates improved service instructions. EASA advises of two reports of cracked metal T/R blade skin, which subsequently led to rotor blade vibrations and forced landing of the helicopter. According to EASA, this condition, if not addressed, could result in additional occurrences of T/R blade structural damage, possibly resulting in significant vibrations and reduced control of the helicopter.

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