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Federal Register / Vol. 86, No. 248 / Thursday, December 30, 2021 / Rules and Regulations
b Affected ADs This AD replaces AD 20212406, Amendment 3921827 86 FR 66934, November 24, 2021 AD 20212406.
c Applicability This AD applies to Airbus Helicopters Model EC130T2 helicopters, certificated in any category, as identified in European Union Aviation Safety Agency EASA
Emergency AD 20210283E, dated December 17, 2021 EASA AD 20210283E.
d Subject Joint Aircraft System Component JASC
Code: 5300, Fuselage Structure.
e Unsafe Condition This AD was prompted by a report of degradation of the rear transmission shaft bearing support and the determination that all of the attachment rivets of the transmission shaft bearing support were sheared. The FAA is issuing this AD to address sheared attachment rivets of the transmission shaft bearing support. This condition, if not addressed, could lead to failure of the tail rotor drive shaft and subsequent loss of yaw control of the helicopter.
f Compliance Comply with this AD within the compliance times specified, unless already done.

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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, EASA AD 20210283E.
h Exceptions to EASA AD 20210283E
1 Where EASA AD 20210283E refers to November 1, 2021 the effective date of EASA
Emergency AD 20210235E, dated October 28, 2021, this AD requires using December 9, 2021 the effective date of AD 202124
06.
2 Where EASA AD 20210283E refers to its effective date, this AD requires using the effective date of this AD.
3 Where EASA AD 20210283E requires compliance in terms of flight hours, this AD
requires using hours time-in-service.
4 Where paragraphs 1 and 2 of EASA
AD 20210283E require accomplishing inspections after each last flight of the day or ALF, this AD requires accomplishing those inspections before each first flight of the day.
5 Where the service information referenced in EASA AD 20210283E
specifies that certain inspections can be done by a mechanical technician, a pilot with correct training and accreditation, or a pilotowner, this AD requires that those inspections be done by a qualified mechanic.
6 Where paragraphs 3 and 4 of EASA
AD 20210283E specify contacting Airbus Helicopters to obtain approved repair instructions and accomplishing those instructions, this AD requires repair done in accordance with a method approved by the Manager, General Aviation & Rotorcraft Section, International Validation Branch, FAA; or EASA; or Airbus Helicopters EASA
Design Organization Approval DOA. If
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approved by the DOA, the approval must include the DOA-authorized signature.
7 Where paragraph 6 of EASA AD 2021
0283E requires reporting inspection results to Airbus Helicopters within 30 days after each rivet replacement, this AD requires reporting inspection results at the applicable time in paragraph h7i or ii of this AD.
i If the inspection was done on or after the effective date of this AD: Submit the report within 10 days after each rivet replacement.
ii If the inspection was done before the effective date of this AD: Submit the report within 10 days after the effective date of this AD.
8 This AD does not mandate compliance with the Remarks section of EASA AD
20210283E.
i Special Flight Permit Special flight permits may be permitted to accomplish the actions required by paragraphs 1 and 2 of EASA AD 2021
0283E for the before each first flight of the day compliance time only, provided that there are no passengers on board. Special flight permits are prohibited for any other actions required by this AD.
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 Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590;
telephone 516 2287330; email andrea.jimenez@faa.gov.
l Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference 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 Emergency AD 20210283E, dated December 17, 2021.
ii Reserved 3 For EASA AD 20210283E, contact EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999

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000; email ADs@easa.europa.eu; Internet www.easa.europa.eu. You may find the EASA material 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 at https www.regulations.gov by searching for and locating Docket No. FAA20211165.
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 December 22, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202128340 Filed 122721; 4:15 pm BILLING CODE 491013P

DEPARTMENT OF LABOR
Office of Labor-Management Standards 29 CFR Parts 403 and 408
RIN 1245AA12

Rescission of Labor Organization Annual Financial Report for Trusts In Which A Labor Organization Is Interested, Form T1
Office of Labor-Management Standards, Department of Labor.
ACTION: Final rule.
AGENCY:

This rule rescinds the final rule published in the Federal Register on March 6, 2020, 2020 Form T1 rule, which established the Form T1, Trust Annual Report, required to be filed by labor organizations about certain trusts in which they are interested pursuant to the Labor-Management Reporting and Disclosure Act LMRDA. Upon further review of the 2020 Form T1 rule, including the pertinent facts and legally relevant policy considerations surrounding that rulemaking, the Department of Labor Department withdraws the rule implementing the Form T1, because it has determined that the 2020 rulemaking record, particularly its analysis of the burden and the benefit of the rule, was insufficient as a matter of policy to justify the trust reporting requirements set forth in the 2020 Form T1 rule.
Further, by requiring reporting on entities not controlled or dominated by
SUMMARY:

E:FRFM30DER1.SGM

30DER1