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Federal Register / Vol. 86, No. 221 / Friday, November 19, 2021 / Rules and Regulations
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, 2 Will not affect intrastate aviation in Alaska, and 3 Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.
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:
a. Removing Airworthiness Directive AD 20192110, Amendment 39
19776 84 FR 63794, November 19, 2019; and b. Adding the following new AD:

20212204 Airbus SAS: Amendment 39
21777; Docket No. FAA20201029;
Project Identifier MCAI202001126T.
a Effective Date This airworthiness directive AD is effective December 27, 2021.

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b Affected ADs This AD replaces AD 20192110, Amendment 3919776 84 FR 63794, November 19, 2019 AD 20192110.
c Applicability This AD applies to all Airbus SAS
airplanes identified in paragraphs c1
through 4 of this AD, certificated in any category.
1 Model A318111, 112, 121, and 122
airplanes.
2 Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes.
3 Model A320211, 212, 214, 216, 231, 232, and 233 airplanes.
4 Model A321111, 112, 131, 211, 212, 213, 231, and 232 airplanes.
d Subject Air Transport Association ATA of America Code 57, Wings.

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e Reason This AD was prompted by a quality control review, which determined that the wrong aluminum alloy was used to manufacture several structural parts and by the issuance of an updated list of suspected parts, including those that may have been improperly heat treated. The FAA is issuing this AD to address structural parts that may not meet the certified life limit, which could result in failure of the flap trailing edge and reduced controllability 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 20200174, dated August 5, 2020 EASA AD 20200174.
h Exceptions to EASA AD 20200174
1 Where EASA AD 20200174 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20200174 does not apply to this AD.
3 Where paragraphs 7 and 8 of EASA
AD 20200174 mandate a parts installation limitation, this AD requires the following parts installation limitation: From the effective date of this AD, only serviceable parts as defined in EASA AD 20200174 are allowed to be installed on any airplane.
4 Where any service information referenced in EASA AD 20200174 specifies reporting, this AD requires reporting all inspection results at the applicable time specified in paragraph h4i or ii of this AD. If operators have reported findings as part of obtaining any corrective actions approved by Airbus SASs EASA Design Organization Approval DOA, operators are not required to report those findings as specified in this paragraph.
i If the inspection was done on or after the effective date of this AD: Submit the report within 30 days after the inspection.
ii If the inspection was done before the effective date of this AD: Submit the report within 90 days after the effective date of this AD.
i 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 j of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. Before using any
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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 EASA; or Airbus SASs EASA DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
3 Required for Compliance RC: Except as required by paragraphs h4 and i2 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.
4 Paperwork Reduction Act Burden Statement: A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 21200056. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. All responses to this collection of information are mandatory as required by this AD. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to Information Collection Clearance Officer, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX
761771524.
j 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; phone and fax:
2062313223; email: sanjay.ralhan@faa.gov.
k 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.

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