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49903

Rules and Regulations
Federal Register Vol. 86, No. 170
Tuesday, September 7, 2021

This section of the FEDERAL REGISTER
contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510.

information on the availability of this material at the FAA, call 2062313195.
It is also available in the AD docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210334.

The Code of Federal Regulations is sold by the Superintendent of Documents.

Examining the AD Docket
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210334; Project Identifier MCAI202001662T; Amendment 3921686; AD 20211703
RIN 2120AA64

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

The FAA is correcting an airworthiness directive AD that was published in the Federal Register. That AD applies to certain Airbus SAS Model A318111, 112, and 122 airplanes;
Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes;
and Model A320211, 212, 214, 231, 232, and 233 airplanes. As published, the AD number specified in the preamble and regulatory text is incorrect. This document corrects this error. In all other respects, the original document remains the same.
DATES: This correction is effective October 5, 2021.
The effective date of AD 20211703
remains October 5, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of October 5, 2021 86 FR 48485, August 31, 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
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SUMMARY:

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16:15 Sep 03, 2021

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You may examine the AD docket at https www.regulations.gov under Docket No. FAA20210334; 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, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION 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.
SUPPLEMENTARY INFORMATION: AD 2021
1703, Amendment 3921686 86 FR
48485, August 31, 2021 AD 202117
03, requires repetitive inspections for cracking at the leftLH and right-hand RH sides of the fuselage skin at certain frames, and repair if necessary, as specified in European Union Aviation Safety Agency EASA AD 20200280, dated December 14, 2020 EASA AD
20200280. That AD applies to certain Airbus SAS Model A318111, 112, and 122 airplanes; Model A319111, 112, 113, 114, 115, 131, 132, and 133
airplanes; and Model A320211, 212, 214, 231, 232, and 233 airplanes.
As the AD was published, the AD
number specified in the preamble and regulatory text is incorrect. AD 2021
1703 incorrectly identified the AD
number as 20171703. The correct AD
number for this AD is 20211703.
Related Service Information Under 1
CFR Part 51
EASA AD 20200280 describes procedures for doing repetitive external general visual inspections or special detailed inspections i.e., phased array ultrasonic technology inspections of the external skin, or detailed inspections for
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Fmt 4700

Sfmt 4700

Correction of Publication This document corrects an error in two locations and correctly adds the AD
as an amendment to 14 CFR 39.13.
Although no other part of the preamble or regulatory information has been corrected, the FAA is publishing the entire rule in the Federal Register.
The effective date of this AD remains October 5, 2021.
Since this action only corrects the AD
number, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Adoption of the Correction Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations 14 CFR
part 39 as follows:
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

Need for the Correction
PO 00000

primer/paint cracks and high frequency eddy current inspections of the internal skin and repair for cracking at the LH
and RH sides of the fuselage skin, above stringer 6 from FR35 to FR47. This material is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section.

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

Corrected
2. The FAA corrects 39.13 by correcting the airworthiness directive published at 86 FR 48485 August 31, 2021 to read:

20211703 Airbus SAS: Amendment 39
21686; Docket No. FAA20210334;
Project Identifier MCAI202001662T.
a Effective Date This airworthiness directive AD is effective October 5, 2021.

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