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Federal Register / Vol. 86, No. 232 / Tuesday, December 7, 2021 / Rules and Regulations 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:

20212318 Airbus Helicopters Deutschland GmbH: Amendment 39
21817; Docket No. FAA20210779;
Project Identifier MCAI202001505R.
a Effective Date This airworthiness directive AD is effective January 11, 2022.
b Affected ADs None.
c Applicability This AD applies to Airbus Helicopters Deutschland GmbH Model MBBBK 117 D
2 helicopters, certificated in any category, as identified in European Union Aviation Safety Agency EASA AD 20200246, dated November 10, 2020 EASA AD 20200246.
d Subject Joint Aircraft Service Component JASC
Code: 2597, Equip/Furnishing System Wiring.

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e Unsafe Condition This AD was prompted by a report of chafing marks on a wiring harness near the locking washer of the lateral control rod. The FAA is issuing this AD to address chafing marks on a wiring harness near the locking washer of the lateral control rod. The unsafe condition, if not addressed, could result in in-flight loss of the hoist load and possible personal injury, or could generate a burning smell and possible need for the flight crew to implement the applicable emergency procedure.
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 20200246.

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h Exceptions to EASA AD 20200246
1 Where EASA AD 20200246 requires compliance in terms of flight hours, this AD
requires using hours time-in-service.
2 Where EASA AD 20200246 refers to its effective date, this AD requires using the effective date of this AD.
3 Where Paragraph 3 of EASA AD 2020
0246 specifies to update the Aircraft Maintenance Programme AMP with certain tasks included in the service information referenced by EASA AD 20200246, this AD
does not include that requirement.
4 This AD does not require the Remarks section of EASA AD 20200246.
i 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 actions of this AD can be performed, provided that no debris from chafing is visible that would allow jamming or fouling of the flight controls, the chafing does not interfere with the flight controls by jamming or fouling, and the systems impacted by the wiring harness are rendered inoperable by collaring the circuit breaker.
j 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 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.
k Related Information For more information about this AD, contact Jacob Fitch, Aerospace Engineer, COS
Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; phone: 817 2224130;
email: jacob.fitch@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 20200246, dated November 10, 2020.
ii Reserved.
3 For EASA AD 20200246, contact EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; phone: +49 221 8999 000;
email: ADs@easa.europa.eu; internet:

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www.easa.europa.eu. You may find the EASA material 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 817 2225110.
This material may be found in the AD docket at https www.regulations.gov by searching for and locating Docket No. FAA20210779.
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 November 4, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202126497 Filed 12621; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210213; Project Identifier 2018CE036AD; Amendment 3921818; AD 20212319
RIN 2120AA64

Airworthiness Directives; Pacific Aerospace Limited Airplanes Federal Aviation Administration FAA, DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Pacific Aerospace Limited Model 750XL
airplanes. This AD results from mandatory continuing airworthiness information MCAI originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI
identifies the unsafe condition as insufficient separation of ground terminations for individual power sources and static grounds. This AD
requires inspecting and separating, if applicable, the battery and generator common ground connections on the airframe. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective January 11, 2022.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of January 11, 2022.
SUMMARY:

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