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Federal Register / Vol. 86, No. 103 / Tuesday, June 1, 2021 / Rules and Regulations a Effective Date This airworthiness directive AD becomes effective June 16, 2021.
b Affected ADs None.
c Applicability This AD applies to Airbus SAS Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency EASA AD 2020
0218, dated October 12, 2020 EASA AD
20200218.
d Subject Air Transport Association ATA of America Code 53, Fuselage.
e Reason This AD was prompted by a determination that the cabin swift broadband antenna doubler installation does not meet widespread fatigue damage WFD
requirements. The FAA is issuing this AD to address the potential effects of WFD on the installation. This condition, if not corrected, could reduce the structural integrity of the fuselage.
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 20200218.

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h Exceptions to EASA AD 20200218
1 Where EASA AD 20200218 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20200218 does not apply to this AD.
3 Where paragraph 3 of EASA AD 2020
0218 specifies actions if any discrepancy is detected, for this AD a discrepancy is defined as any crack, oversized hole, corrosion, or other damage.
4 Where paragraph 3 of EASA AD 2020
0218 specifies to contact Airbus for applicable corrective actions, if corrective actions are associated with cracking, the cracking must be repaired before further flight 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.
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
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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 DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
3 Required for Compliance RC: Except as required by paragraph 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.
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 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 20200218, dated October 12, 2020.
ii Reserved 3 For EASA AD 20200218, 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. FAA20210367.

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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 May 7, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202111428 Filed 52821; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210126; Project Identifier MCAI202000266R; Amendment 3921556; AD 20211023
RIN 2120AA64

Airworthiness Directives; Airbus Helicopters Deutschland GmbH AHD
Helicopters Federal Aviation Administration FAA, DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for Airbus Helicopters Deutschland GmbH AHD
Model MBBBK 117 D2 helicopters.
This AD was prompted by a report of a broken Titanium Ti bolt. This AD
requires removing certain Ti-bolts from service and prohibits installing these Tibolts in a critical area. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective July 6, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD
as of July 6, 2021.
ADDRESSES: For service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052;
telephone 972 6410000 or 800 232
0323; fax 972 6413775; or at https
www.airbus.com/helicopters/services/
technical-support.html. You may view the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX
76177. It is also available at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0126.
SUMMARY:

Examining the AD Docket You may examine the AD docket at https www.regulations.gov by
E:FRFM01JNR1.SGM

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