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Federal Register / Vol. 86, No. 234 / Thursday, December 9, 2021 / Rules and Regulations accumulating 500 total hours TIS since new and thereafter at intervals not to exceed 50
hours TIS, or 70 engine start-stop cycles, whichever occurs first, inspect the cooling fan front flange for a crack in accordance with Section E, Maintenance Instructions, sub section 52A10 Cooling Fan Inspection, paragraph c, on page E553, of MM J70
002 Issue 06, except where MM J70002
Issue 06 specifies to use a torchlight, use a flashlight. If any crack is found, before further flight, remove the cooling fan front flange from service.
iii Cooling fan front flange P/N G5202
201 mounted on pulley 24 screws P/N G52
10102 and having never been mounted on pulley 12 screws P/N G5210100 or G52
10101, installed on cooling fan P/N G52
00002: Before accumulating 500 total hours TIS since new and thereafter at intervals not to exceed 100 hours TIS, inspect the cooling fan front flange for a crack in accordance with Section E, Maintenance Instructions, sub section 52A10 Cooling Fan Inspection, paragraph c, on page E553, of MM J70
002 Issue 06, except where MM J70002
Issue 06 specifies to use a torchlight, use a flashlight. If any crack is found, before further flight, remove the cooling fan front flange from service.
iv For helicopters with tail boom P/N
G6500101, G6500102 or G6500103
and subsequent installed: Before further flight after the effective date of this AD, paint or verify the tail boom upper surface in accordance with Section C, Airworthiness Limitations, sub section C23 Tail Structure Paint, on page C6, of MM J70002 Issue 06, as applicable to your helicopter.

khammond on DSKJM1Z7X2PROD with RULES

h Credit for Previous Actions This paragraph provides credit for the actions specified in paragraphs g2i through iii of this AD, if those actions were performed before the effective date of this AD
using Section E, Maintenance Instructions, sub section 52A10 Cooling Fan Inspection, paragraphs c and d, of Guimbal France Helicopteres Guimbal Cabri G2 MM and Instructions for Continued Airworthiness, J70002 Issue05.1, dated October 30, 2015.
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.

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.
2 Service information identified in this AD that is not incorporated by reference is available at the contact information specified in paragraphs k3 and 4 of this AD.
3 The subject of this AD is addressed in European Aviation Safety Agency now European Union Aviation Safety Agency EASA AD 20190025, dated February 4, 2019. You may view the EASA AD on the internet at https www.regulations.gov in Docket No. FAA20210688.
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.
i Page C6 of Section C, Airworthiness Limitations, of Guimbal France Helicopteres Guimbal Cabri G2 Maintenance Manual and Instructions for Continued Airworthiness, J70002Issue 06, dated December 6, 2018.
ii Page E553 of Section E, Maintenance Instructions, of Guimbal France Helicopteres Guimbal Cabri G2 Maintenance Manual and Instructions for Continued Airworthiness, J70002Issue 06, dated December 6, 2018.
3 For service information identified in this AD, contact Helicopteres Guimbal, 1070, rue du Lieutenant Parayre, Aerodrome dAixen-Provence, 13290 Les Milles, France;
telephone 330442391088; email support@guimbal.com; or at https
www.guimbal.com.
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.
Issued on October 14, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202126543 Filed 12821; 8:45 am BILLING CODE 491013P

j Related Information 1 For more information about this AD, contact Andrea Jimenez, Aerospace Engineer,
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DEPARTMENT OF COMMERCE
Bureau of Industry and Security 15 CFR Part 705
Docket No. 2111150229
RIN 0694AH55

Removal of Certain General Approved Exclusions GAEs Under the Section 232 Steel and Aluminum Tariff Exclusions Process Bureau of Industry and Security, U.S. Department of Commerce.

AGENCY:
ACTION:

Interim final rule.

On December 14, 2020, the Department of Commerce published an interim final rule the December 14
rule that revised aspects of the process for requesting exclusions from the duties and quantitative limitations on imports of aluminum and steel discussed in three previous Department of Commerce Commerce interim final rules implementing the exclusion process authorized by the President under Section 232 of the Trade Expansion Act of 1962, as amended, as well as a May 26, 2020 notice of inquiry.
The December 14 rule included adding 123 General Approved Exclusions GAEs to the regulations. Subsequently, based on Commerces review of the public comments received in response to the December 14 rule and additional analysis conducted by Commerce on the Section 232 exclusion request submissions, Commerce determined that a subset of the GAEs added in the December 14 rule no longer meets the criteria for inclusion as a GAE and should therefore be removed. Commerce is removing these GAEs in this interim final rule to ensure only those GAEs that meet the stated criteria from the December 14 rule will continue to be included as eligible GAEs. This interim final rule removes thirty of the GAEs that were added to the regulations in the December 14 rule, consisting of twentysix GAEs for steel and four GAEs for aluminum. As a conforming change to a recent U.S. International Trade Commission ITC decision, this rule also removes one additional steel GAE.
Lastly, this interim final rule adds a note to both GAE supplements to address future changes to the Harmonized Tariff Schedule of the United States HTSUS.

SUMMARY:

E:FRFM09DER1.SGM

09DER1