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Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
assembly. If the operational check fails, before next flight involving a hoist operation, repair or replace the anti-foul assembly.
B 3 hoist operating hours, clean, visually inspect the rescue hoist cable for damage, which may be indicated by a broken wire, kink, bird caging, flattened area, abrasion, or necking. If there is any damage, before further flight, replace the rescue hoist cable.
If there is no damage, before further flight, lubricate the rescue hoist cable. For purposes of this AD, hoist operating hours are counted anytime the hoist motor is operating.
Note 2 to paragraph g2iiiB: Bell Helicopter service information refers to hoist operating hours as hoisting hours.
C 800 hours TIS or 1 year, whichever occurs first, perform an operational check of the speed limit switches and perform an operational check of the 600-pound external hoist electrical system to inspect operation of the HOIST HOT caution light. If an operational check fails, before next flight involving a hoist operation, repair in accordance with FAA-approved procedures or replace the hoist.
D 2,200 hours TIS or 111 hoist operating hours, whichever occurs first, perform a functional check of the cable cutter cartridge electrical system to inspect for correct functioning of the cable cutter switches hoist pendant, pilot cyclic, and copilot cyclic and associated wiring. If a functional check fails, before next flight involving a hoist operation, repair in accordance with FAA-approved procedures or replace the hoist.
E 111 hoist operating hours, overhaul or replace the hoist.

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.
You may view this referenced 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 817 222
5110.
3 The subject of this AD is addressed in Transport Canada AD CF201716, dated May 17, 2017. You may view the Transport Canada AD at https www.regulations.gov in Docket No. FAA20210267.

h 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 i1 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.

RIN 2120AA64

i Related Information 1 For more information about this AD, contact Matt Fuller, AD Program Manager, General Aviation & Rotorcraft Unit, Airworthiness Products Section, Operational Safety Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817 222
5110; email matthew.fuller@faa.gov.
2 Chapter 4Airworthiness Limitations Schedule of Bell Helicopter 429 Maintenance Manual BHT429MM1 to Revision 26, dated September 9, 2016, which is not incorporated by reference, contains additional information about the subject of this AD. For service information identified in this AD, contact Bell Textron Canada
VerDate Sep<11>2014

16:01 Jun 23, 2021

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Issued on June 17, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202113193 Filed 62321; 8:45 am BILLING CODE 491013P

This AD is effective July 29, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of July 29, 2021.
ADDRESSES: For material incorporated by reference IBR in this AD, contact 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 IBR material on the EASA
website at https ad.easa.europa.eu.
You may view this IBR material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 2062313195.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2020
1178.
DATES:

DEPARTMENT OF TRANSPORTATION

Examining the AD Docket
Federal Aviation Administration
You may examine the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2020
1178; 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, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT:
Kathleen Arrigotti, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 2062313218.
SUPPLEMENTARY INFORMATION:

14 CFR Part 39
Docket No. FAA20201178; Project Identifier MCAI202001325T; Amendment 3921545; AD 20211012

Airworthiness Directives; Airbus SAS
Airplanes Federal Aviation Administration FAA, Department of Transportation DOT.
ACTION: Final rule.
AGENCY:

The FAA is superseding Airworthiness Directive AD 202009
14, which applied to certain Airbus SAS
Model A350941 and 1041 airplanes.
AD 20200914 required revising the existing airplane flight manual AFM to define a liquid-prohibited zone on the flight deck and provide procedures following liquid spillage on the center pedestal. AD 20200914 also required installing a removable integrated control panel ICP cover on the flight deck and further revising the AFM to include instructions for ICP cover use. This AD
requires installing a new, water-resistant ICP, which allows removing the ICP
protective cover and the AFM revisions, as specified in a European Union Aviation Safety Agency EASA AD, which is incorporated by reference. This AD was prompted by development of a new, water-resistant ICP. The FAA is issuing this AD to address the unsafe condition on these products.

SUMMARY:

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Background EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 20200203, dated September 23, 2020 EASA AD
20200203 also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI, to correct an unsafe condition for certain Airbus SAS
Model A350941 and 1041 airplanes.
The FAA issued a notice of proposed rulemaking NPRM to amend 14 CFR
part 39 to supersede AD 20200914, Amendment 3919910 85 FR 30601, May 20, 2020 AD 20200914. AD
20200914 applied to certain Airbus SAS Model A350941 and 1041
airplanes. The NPRM published in the
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