Quiero saber acerca de...

33108

Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations a certain compliance time. For this AD, report the inspection results of each inspection accomplished in this AD at the applicable time specified in paragraph h4i or ii of this AD.
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 30 days after the effective date of this AD.

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 adding the following new airworthiness directive:

20211204 Fokker Services B.V.:
Amendment 3921591; Docket No.
FAA20210448; Project Identifier MCAI202100044T.
a Effective Date This airworthiness directive AD becomes effective July 9, 2021.
b Affected ADs None.
c Applicability This AD applies to all Fokker Services B.V.
Model F28 Mark 0070 and 0100 airplanes, certificated in any category.
d Subject Air Transport Association ATA of America Code 57, Wings.
e Reason This AD was prompted by a report that corrosion was found on the horizontal flange on the front spar lower boom, between the rebate strap and the lower boom, and resulted in bulging. The FAA is issuing this AD to address corrosion on the horizontal flange, which could lead to reduced structural integrity of the wing torsion box structure.
f Compliance Comply with this AD within the compliance times specified, unless already done.

khammond on DSKJM1Z7X2PROD with RULES

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 20210014, dated January 13, 2021 EASA AD 20210014.
h Exceptions to EASA AD 20210014
1 Where EASA AD 20210014 refers to its effective date, this AD requires using the effective date of this AD.
2 Where paragraph 2 of EASA AD 2021
0014 requires additional actions for bulging between 0.5 mm and 3 mm, this AD
requires those additional actions for bulging 0.5 mm or more and 3.0 mm or less.
3 The Remarks section of EASA AD
20210014 does not apply to this AD.
4 Paragraph 5 of EASA AD 20210014
specifies to report inspection results within
VerDate Sep<11>2014

16:01 Jun 23, 2021

Jkt 253001

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 Fokker Services B.V.s EASA
Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
j Related Information For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 2062313226; email Tom.Rodriguez@
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 20210014, dated January 13, 2021.
ii Reserved 3 For EASA AD 20210014, 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
PO 00000

Frm 00028

Fmt 4700

Sfmt 4700

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. FAA20210448.
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 27, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202113108 Filed 62321; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210256; Project Identifier MCAI202000480R; Amendment 3921596; AD 20211209
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 all Airbus Helicopters Deutschland GmbH
AHD Model MBBBK 117 D2
helicopters. This AD was prompted by a short circuit in a yaw trim actuator connector that occurred during production electrical tests. This AD
requires replacing certain wire harness trim connector backshells backshells, as specified in a European Union 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 July 29, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of July 29, 2021.
ADDRESSES: For material incorporated by reference IBR in this AD, contact the 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 SUMMARY:

E:FRFM24JNR1.SGM

24JNR1