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Federal Register / Vol. 86, No. 124 / Thursday, July 1, 2021 / Rules and Regulations
Regulatory Findings The FAA determined that this AD
will not have federalism implications under Executive Order 13132. This AD
will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I
certify that this AD:
1 Is not a significant regulatory action under Executive Order 12866, and 2 Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

Authority: 49 U.S.C. 106g, 40113, 44701.
39.13

Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:

20211408 Airbus SAS: Amendment 39
21635; Docket No. FAA20210540;
Project Identifier MCAI202100694T.
a Effective Date This airworthiness directive AD becomes effective July 1, 2021.
b Affected ADs None.

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c Applicability This AD applies to all Airbus SAS Model A319151N, A319153N, A319171N, A320
251N, A320252N, A320253N, A320271N, A320272N, A320273N, A321251N, A321
251NX, A321252N, A321252NX, A321
253N, A321253NX, A321271N, A321
271NX, A321272N and A321272NX
airplanes, certificated in any category.
d Subject Air Transport Association ATA of America Code 34, Navigation.
e Reason This AD was prompted by reports of an increasing number of operational disruptions due to airspeed discrepancies that have occurred due to the large number of airplanes returning to service after airplanes have been parked or stored a large number of airplanes
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have been parked or stored due to the COVID19 pandemic. The FAA is issuing this AD to address airspeed discrepancies, which could lead to an unstable flight path after take-off, possibly resulting in reduced control of the airplane.
f Compliance Comply with this AD within the compliance times specified, unless already done.
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, European Union Aviation Safety Agency EASA AD 20210150, dated June 21, 2021; corrected June 25, 2021 EASA
AD 20210150.
h Exceptions to EASA AD 20210150
1 Where EASA AD 20210150 refers to its effective date, this AD requires using the effective date of this AD.
2 Paragraph 1 of EASA AD 20210150
specifies amending the applicable AFM
airplane flight manual, but this AD
requires amending the existing applicable AFM and applicable corresponding operational procedures.
3 Paragraph 3 of EASA AD 20210150
does not apply to this AD.
4 The Remarks section of EASA AD
20210150 does not apply to this AD.
5 Where paragraph 1 of EASA AD 2021
0150 specifies to inform all flight crews, and, thereafter, operate the aeroplane accordingly, this AD does not require those actions as those actions are already required by existing FAA operating regulations.
i Special Flight Permit Special flight permits, as described in 14
CFR 21.197 and 21.199, are not allowed after 7 days after the effective date of this AD
unless the AFM revision required by paragraph g of this AD is accomplished.
j Other FAA AD Provisions The following provisions also apply to this AD:
1 Alternative Methods of Compliance AMOCs: The Manager, Large Aircraft Section, 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 responsible Flight Standards Office, as appropriate. If sending information directly to the Large Aircraft Section, 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. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.
2 Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, Large Aircraft Section, International Validation Branch, FAA; or
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EASA; or Airbus SASs EASA Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
3 Required for Compliance RC: Except as required by paragraph j2 of this AD, if any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operators maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC.
k Related Information For more information about this AD, contact Sanjay Ralhan, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 2062313223; email Sanjay.Ralhan@
faa.gov.
l 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 European Union Aviation Safety Agency EASA AD 20210150, dated June 21, 2021;
corrected June 25, 2021.
ii Reserved 3 For EASA AD 20210150, 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 EASA AD on the EASA website at https
ad.easa.europa.eu.
4 You may view this 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. This material may be found in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA20210540.
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 fedreg.legal@
nara.gov, or go to: https www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on June 28, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202114158 Filed 62921; 11:15 am BILLING CODE 491013P

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