Quiero saber acerca de...

Federal Register / Vol. 86, No. 34 / Tuesday, February 23, 2021 / Rules and Regulations l Related Information
DEPARTMENT OF TRANSPORTATION

1 Refer to Mandatory Continuing Airworthiness Information MCAI Canadian AD CF202009, dated April 7, 2020, for related information. This MCAI may be found in the AD docket on the internet at https www.regulations.gov by searching for and locating Docket No. FAA20200691.
2 For more information about this AD, contact Andrea Jimenez, Aerospace Engineer, Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 5162287330; fax 5167945531; email 9avs-nyaco-cos@faa.gov.
m Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference IBR 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 Bombardier Service Bulletin 601R32
112, dated November 11, 2019.
ii Reserved 3 For service information identified in this AD, contact MHI RJ Aviation ULC, 12655
Henri-Fabre Blvd., Mirabel, Quebec, J7N 1E1
Canada; Widebody Customer Response Center North America toll-free telephone +1
8442722720 or direct-dial telephone +1
5148558500; fax +15148558501; email thd.crj@mhirj.com; internet https
mhirj.com.
4 You may view this service information 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.
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 fedreg.legal@nara.gov, or go to: https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on December 28, 2020.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202103565 Filed 22221; 8:45 am BILLING CODE 491013P

VerDate Sep<11>2014

21:28 Feb 22, 2021

Jkt 253001

Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20200674; Product Identifier 2020NM070AD; Amendment 3921382; AD 20210106
RIN 2120AA64

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

The FAA is adopting a new airworthiness directive AD for certain Airbus SAS Model A330200 and A330300 series airplanes, and all Model A340200 and A340300 series airplanes. This AD was prompted by reports of hydraulic system failure due to fatigue failure of the screws attaching the manual valve to the ground service manifold GSM. This AD requires, for certain GSMs, repetitive replacement of the hydraulic system GSM manual valve attachment screws having certain part numbers; and, for certain other GSMs with certain screws installed, replacement of those screws, as specified in a European Union Aviation Safety Agency EASA AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective March 30, 2021.
The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD
as of March 30, 2021.
ADDRESSES: For EASA material incorporated by reference IBR in this AD, contact the EASA, KonradAdenauer-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. For Airbus material incorporated by reference in this AD, contact Airbus SAS, Airworthiness OfficeEAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36
96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com;
internet http www.airbus.com. 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.
SUMMARY:

PO 00000

Frm 00065

Fmt 4700

Sfmt 4700

10767

It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2020
0674.
Examining the AD Docket You may examine the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2020
0674; 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:
Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 2062313229; email vladimir.ulyanov@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion The EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD
20200093, dated April 24, 2020 EASA
AD 20200093 also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI, to correct an unsafe condition for certain Airbus SAS Model A330200 and A330300
series airplanes, and all Model A340
200 and A340300 series airplanes.
The FAA issued a notice of proposed rulemaking NPRM to amend 14 CFR
part 39 by adding an AD that would apply to certain Airbus SAS Model A330200 and A330300 series airplanes, and all Model A340200 and A340300 series airplanes. The NPRM
published in the Federal Register on July 31, 2020 85 FR 46012. The NPRM
was prompted by reports of hydraulic system failure due to fatigue failure of the screws attaching the manual valve to the GSM. The NPRM proposed to require, for certain GSMs, repetitive replacement of the hydraulic system GSM manual valve attachment screws having certain part numbers; and, for certain other GSMs with certain screws installed, replacement of those screws, as specified in an EASA AD.
Comments The FAA gave the public the opportunity to participate in developing this final rule. The following presents the comments received on the NPRM

E:FRFM23FER1.SGM

23FER1