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68894

Federal Register / Vol. 86, No. 231 / Monday, December 6, 2021 / Rules and Regulations
c Applicability This AD applies to Leonardo S.p.a. Model A109E helicopters, certificated in any category, as identified in European Union Aviation Safety Agency EASA AD 2020
0256, dated November 17, 2020 EASA AD
20200256.
d Subject Joint Aircraft Service Component JASC
Code: 5300, Fuselage Structure.
e Unsafe Condition This AD was prompted by reports of cracking in the center fuselage frame assembly in the intersection of the lateral pylon and floor spar at station STA 1815 on the leftand right-hand sides. The FAA is issuing this AD to address cracking in the intersection of the lateral pylon and floor spar at STA 1815 on the leftand right-hand sides, which, if not addressed, could affect the structural integrity of the helicopter.
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 20200256.

khammond on DSKJM1Z7X2PROD with RULES

h Exceptions to EASA AD 20200256
1 Where EASA AD 20200256 requires compliance in terms of flight hours, this AD
requires using hours time-in-service.
2 Where EASA AD 20200256 AD refers to its effective date, this AD requires using the effective date of this AD.
3 Where Figure 1 of the service information referenced in EASA AD 2020
0256 depicts the AFT bulkhead twice, for clarification, the FWD bulkhead is mislabeled as AFT and depicted on the left side of Figure 1, below 109032096 POST
ASSY REF and above FWD CAP.
4 Where the service information referenced in EASA AD 20200256 specifies discarding parts, this AD requires removing those parts from service.
5 Where paragraph 2 of EASA AD 2020
0256 or the service information referenced in EASA AD 20200256 specifies to contact the manufacturer for repair information, for this AD: Before further flight, do the repair using a method approved by the Manager, International Validation Branch, FAA; or EASA; or Leonardo S.p.a.s EASA Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
6 This AD does not mandate compliance with the Remarks section of EASA AD
20200256.
i No Reporting Requirement Although the service information referenced in EASA AD 20200256 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

VerDate Sep<11>2014

15:44 Dec 03, 2021

Jkt 256001

j Alternative Methods of Compliance AMOCs
DEPARTMENT OF TRANSPORTATION

1 The Manager, 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the 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.
2 Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.

Federal Aviation Administration
k Related Information For more information about this AD, contact Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590;
telephone 516 2287330; email andrea.jimenez@faa.gov.
l 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 Union Aviation Safety Agency EASA AD 20200256, dated November 17, 2020.
ii Reserved.
3 For EASA AD 20200256, 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 the EASA material on the EASA website at https ad.easa.europa.
4 You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 817 2225110.
This material may be found in the AD docket at https www.regulations.gov by searching for and locating Docket No. FAA20210697.
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 fr.inspection@nara.gov, or go to: https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on October 26, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202126333 Filed 12321; 8:45 am BILLING CODE 491013P

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14 CFR Part 39
Docket No. FAA20210722; Project Identifier MCAI202100329T; Amendment 3921813; AD 20212315
RIN 2120AA64

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

The FAA is adopting a new airworthiness directive AD for certain 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.
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. This AD
requires modifying the waste compartment door of each affected galley, as specified in a European 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 January 10, 2022.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of January 10, 2022.
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 information on the availability of this material at the FAA, call 2062313195.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0722.
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
SUMMARY:

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06DER1