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Federal Register / Vol. 86, No. 222 / Monday, November 22, 2021 / Rules and Regulations
any missing cadmium plating and apply a chromate conversion coating.
2 Within 50 hours TIS after completion of paragraph g1 of this AD, and thereafter at intervals not to exceed 50 hours TIS:
i Using a 10X magnifying glass, visually inspect the neck and threaded area of each M/R clevis for wear, corrosion, and damage, which for the purposes of this inspection may be indicated by distortion, bending, a crack, or damaged M/R clevis threads. Refer to Figure 3 of ASB 4302160 for a depiction of the area to inspect on each M/R clevis. If there is any wear, corrosion, or damage, before further flight, remove the affected M/
R clevis from service and replace with an airworthy part.
ii Perform the actions required in paragraph g1iv of this AD for each M/R
clevis.
3 Within 150 hours TIS after the completion of paragraph g1 of this AD, and thereafter at intervals not to exceed 150
hours TIS, visually inspect and purge grease each universal bearing, by performing the actions as required in paragraphs g1ii and iii of this AD.
h Special Flight Permits A special flight permit may be permitted provided that there are no passengers onboard.

jspears on DSK121TN23PROD with RULES1

j Related Information 1 For more information about this AD, contact Hal Jensen, Aerospace Engineer, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 LEnfant Plaza N SW, Washington, DC 20024;
telephone 202 2679167; email hal.jensen@
faa.gov.
2 The subject of this AD is addressed in Transport Canada CF202126 AD, dated July 26, 2021. You may view the Transport Canada AD at https www.regulations.gov in Docket No. FAA20211011.
k 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 the AD specifies otherwise.

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Issued on November 16, 2021.
Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202125489 Filed 111821; 11:15 am
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 j1 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.

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i Bell Alert Service Bulletin 4302160, dated July 13, 2021.
ii Reserved 3 For service information identified in this AD, contact Bell Textron Canada Limited, 12,800 Rue de lAvenir, Mirabel, Quebec J7J 1R4, Canada; telephone 1450
4372862 or 18003638023; fax 1450
4330272; email productsupport@
bellflight.com; or at https
www.bellflight.com/support/contact-support.
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.
5 You may view this service information 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/
ibr-locations.html.

BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 89
Docket No.: FAA20191100

Policy Statement for the Reported Geometric Altitude of the Control Station of a Standard Remote Identification Unmanned Aircraft Federal Aviation Administration FAA, U.S. Department of Transportation DOT.
ACTION: Statement of policy.
AGENCY:

This action clarifies FAA
policy regarding the existing accuracy requirements for the reported geometric altitude of the control station of a standard remote identification unmanned aircraft. The FAA describes one acceptable way producers of unmanned aircraft can meet the minimum performance requirement for the accuracy of the control stations reported geometric altitude. The FAA
determined that this action is necessary to inform developers of means of compliance of one potential pathway to meet the performance requirement for the control stations reported geometric altitude.
DATES: The effective date of this policy is November 22, 2021.
SUMMARY:

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For information on where to obtain copies of this statement of policy and other information related to this statement, see Additional Information in the SUPPLEMENTARY INFORMATION
section of this document.
FOR FURTHER INFORMATION CONTACT: Paul Siegmund, Policy and Innovation Division, Federal Aviation Administration, 800 Independence Ave.
SW, Washington, DC 20591; telephone 1844FLYMYUA 18443596981;
email: UAShelp@faa.gov.
SUPPLEMENTARY INFORMATION:
ADDRESSES:

I. Overview A. Background On January 15, 2021, the FAA
published a final rule titled Remote Identification of Unmanned Aircraft Remote ID final rule with an original effective date of March 16, 2021.1 2 The Remote ID final rule requires the remote identification of unmanned aircraft in the airspace of the United States.
Remote identification is the capability of an unmanned aircraft, in flight, to provide certain identification, location, and performance information that people on the ground and other airspace users can receive.
In addition to the operating requirements, the Remote ID final rule provides the design and production requirements for the production of remote identification unmanned aircraft or broadcast modules. These requirements describe the performance standards for remote identification without establishing a specific means or process for regulated entities to follow.3
A person designing or producing a standard remote identification unmanned aircraft or remote identification broadcast module must show that the unmanned aircraft or broadcast module meets the performance requirements of the rule by following an FAA-accepted means of compliance. A means of compliance submitted to the FAA for acceptance 1 Remote Identification of Unmanned Aircraft final rule, 86 FR 4390 Jan. 15, 2021.
2 On March 10, 2021, the FAA published a correction to the Remote ID final rule in accordance with the memorandum titled Regulatory Freeze Pending Review 86 FR 7424, Jan 28, 2021, delaying the final rules effective date to April 21, 2021 86 FR 13629.
3 A standard remote identification unmanned aircraft broadcasts identification, location, and performance information of the unmanned aircraft and control station. This unmanned aircraft broadcasts the remote identification message elements directly from the unmanned aircraft from takeoff to shutdown. A remote identification broadcast module broadcasts identification, location, and take-off information; the broadcast module may be a separate device that is attached to an unmanned aircraft, or a feature built into the aircraft. 86 FR 4391 Jan. 15, 2021.

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