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Federal Register / Vol. 86, No. 231 / Monday, December 6, 2021 / Rules and Regulations
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.
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:

20212315 Airbus SAS: Amendment 39
21813; Docket No. FAA20210722;
Project Identifier MCAI202100329T.
a Effective Date This airworthiness directive AD is effective January 10, 2022.
b Affected ADs None.
c Applicability This AD applies to Airbus SAS Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes; Model A320211, 212, 214, 216, 231, 232, and 233
airplanes; and Model A321111, 112, 131, 211, 212, 213, 231, and 232 airplanes;
certificated in any category; as identified in European Aviation Safety Agency EASA AD
20180255, dated November 27, 2018 EASA
AD 20180255.

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d Subject Air Transport Association ATA of America Code 25, Equipment/Furnishings.
e Reason This AD was prompted by a report that during re-engineering of galley G5, a 9G
forward full scale qualification test was performed, and the door of the waste compartment opened before the required load was reached. The FAA is issuing this AD to address failure of the galley door and release of trolleys during a rejected take-off or an emergency landing, which could result in injury to occupants and damage to the airplane.

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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, EASA AD 20180255.
h Exceptions to EASA AD 20180255
1 Where EASA AD 20180255 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20180255 does not apply to this AD.
h Clarification of Required Service Information Where Paragraph 1 of EASA AD 2018
0255 requires using, among other service information, Zodiac Galleys Europe SB
21351025001 rev. B, this AD requires using Zodiac Galleys Europe Service Bulletin 21351025001, Revision B, dated January 28, 2018; or Zodiac Galleys Europe Service Bulletin 21351025001, Revision C, dated May 24, 2018; or Safran Service Bulletin 21351025001, Revision D, dated August 15, 2019.
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 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 Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
3 Required for Compliance RC: For any service information referenced in EASA AD
20180255 that contains RC procedures and tests: Except as required by paragraph i2
of this AD, RC 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
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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.
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; telephone 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 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 Aviation Safety Agency EASA AD 20180255, dated November 27, 2018.
ii Zodiac Galleys Europe Service Bulletin 21351025001, Revision B, dated January 28, 2018.
iii Zodiac Galleys Europe Service Bulletin 21351025001, Revision C, dated May 24, 2018.
iv Safran Service Bulletin 21351025
001, Revision D, dated August 15, 2019.
3 For EASA AD 20180255, 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 For Zodiac Galleys Europe and Safran service information identified in this AD, contact Safran Cabin CZ s.r.o., Univerzitni 1119/34, 301 00 Plzen, Czech Republic;
telephone: +420 377 664 111; internet https www.safran-group.com/companies/
safran-cabin.
5 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.
6 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 fr.inspection@nara.gov, or go to: https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on November 2, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202126394 Filed 12321; 8:45 am BILLING CODE 491013P

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