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39.13

Federal Register / Vol. 86, No. 103 / Tuesday, June 1, 2021 / Rules and Regulations Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:

20211025 Airbus Helicopters:
Amendment 3921558; Docket No.
FAA20210145; Project Identifier MCAI202001212R.

i No Reporting Requirement Although the service information referenced in EASA AD 20200187 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

a Effective Date This airworthiness directive AD is effective July 6, 2021.
b Affected ADs None.
c Applicability This AD applies to all Airbus Helicopters Model EC130B4 and EC130T2 helicopters, certificated in any category, with a tail rotor blade TRB, obtained by forging, part number 350A33300202, 350A33300203, 350A33300204, or 350A33300205
installed.
d Subject Joint Aircraft System Component JASC
Code 6410, Tail rotor blades.
e Reason This AD was prompted by a report of cracks and geometrical non-conformities of the TRBs; all cracks initiated in the drain hole area at the blade root section. The FAA
is issuing this AD to address geometrical non-conformities of the TRBs, which could lead to crack initiation and consequent blade failure, and possible loss of control of the helicopter.
f Compliance Comply with this AD within the compliance times specified, unless already done.

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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 20200187, dated August 21, 2020 EASA AD 20200187.
h Exceptions to EASA AD 20200187
1 Where EASA AD 20200187 refers to its effective date, this AD requires using the effective date of this AD.
2 The Remarks section of EASA AD
20200187 does not apply to this AD.
3 Although the service information referenced in EASA AD 20200187 specifies to discard certain parts, this AD does not include that requirement.
4 Although the service information referenced in EASA AD 20200187 specifies to return certain parts, this AD does not include that requirement.
5 Where EASA AD 20200187 refers to flight hours FH, this AD requires using hours time-in-service.
6 Where the service information referenced in EASA AD 20200187 specifies to contact customer support, this AD does not include that requirement.
7 Where the service information referenced in EASA AD 20200187 specifies
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to measure using the Smartphone application, the PowerPoint method, or Contacting customer support with a specific procedure, those methods of measurement are not required by this AD.

j Special Flight Permit Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199
to operate the helicopter to a location where the helicopter can be modified if the operator elects to do so, provided that the helicopter is operated under visual flight rules.
k Alternative Methods of Compliance AMOCs 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 l 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.
l Related Information For more information about this AD, contact Hal Jensen, Aerospace Engineer, Operational Safety Branch, FAA, 950
LEnfant Plaza SW, Washington, DC 20024;
phone: 2022679167; email: hal.jensen@
faa.gov.
m 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 20200187, dated August 21, 2020.
ii Reserved 3 For EASA AD 20200187, contact the EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; phone: +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 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 8172225110. This
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material may be found in the AD docket on the internet at https www.regulations.gov by searching for and locating Docket No.
FAA20210145.
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.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202111393 Filed 52821; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210030; Project Identifier MCAI202001395T; Amendment 3921555; AD 20211022
RIN 2120AA64

Airworthiness Directives; Bombardier, Inc., Airplanes Federal Aviation Administration FAA, Department of Transportation DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Bombardier, Inc., Model BD7001A10
airplanes. This AD was prompted by a report indicating that during installation, a fuel pipe bracket assembly on the intermediate rib in the center fuel tank was mislocated, resulting in an offset between the fitting assembly and the refuel/defuel tube assembly. This AD requires modification of the fuel pipe bracket assembly, including all related investigative actions and corrective actions, if necessary; and performing an operational test of the refuel and defuel system. 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 publication listed in this AD
as of July 6, 2021.
ADDRESSES: For service information identified in this final rule, contact Bombardier, Inc., 400 Cote-Vertu Road West, Dorval, Quebec H4S 1Y9, Canada;
telephone 5148555000; fax 514855
7401; email thd.crj@
aero.bombardier.com; internet https
SUMMARY:

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