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Federal Register / Vol. 86, No. 176 / Wednesday, September 15, 2021 / Rules and Regulations
any bulk cargo door seals having p/n D5237200220000 or D5237200220200, as those actions are now required by paragraph 1 of EASA AD 20210049.
3 Where paragraph 4 of EASA AD 2021
0049 specifies amending the aircraft flight manual AFM and operating that aeroplane accordingly, this AD does not include a requirement for operating that aeroplane accordingly as that action is already required by existing FAA operating regulations.
4 Paragraph 4 of EASA AD 20210049
specifies amending the Aircraft Flight Manual AFM of the aeroplane, however, this AD requires amending the existing AFM and applicable corresponding operational procedures. Inserting a copy of EASA AD 20210049 into the existing AFM
and applicable corresponding operational procedures is an acceptable method to comply with this requirement.
5 The Remarks section of EASA AD
20210049 does not apply to this AD.

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.

i Terminating Action for AD 20201601
Accomplishing the terminating action on an airplane, as specified in paragraph 6 of EASA AD 20210049, for the affected parts defined in EASA AD 20210049 terminates all requirements of AD 20201601 for forward and aft cargo door seals having part number p/n D5237106020000, D5237106020200, D5237106020400, D5237300120000, or D5237300120200; and bulk cargo door seals having p/n D5237200220000 or D5237200220200 only.

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 20210049, dated February 18, 2021.
ii Reserved 3 For EASA AD 20210049, 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. FAA20210368.
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.

j 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 k 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 Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
3 Required for Compliance RC: For any service information referenced in EASA AD
20210049 that contains RC procedures and tests: Except as required by paragraph j2
of this AD, RC procedures and tests must be done to comply with this AD; any procedures
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k 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.
l Material Incorporated by Reference
Issued on August 19, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202119816 Filed 91421; 8:45 am BILLING CODE 491013P

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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210698; Project Identifier MCAI202100284T; Amendment 3921703; AD 20211802
RIN 2120AA64

Airworthiness Directives; Fokker Services B.V. Airplanes Federal Aviation Administration FAA, DOT.
ACTION: Final rule; request for comments.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes. This AD
was prompted by a report of a crack found on the forward pressure bulkhead web plate, at the edge of a bonded doubler. This AD requires a one-time inspection of the forward bulkhead for cracking, repair if necessary, and a report of inspection results, 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 becomes effective September 30, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of September 30, 2021.
The FAA must receive comments on this AD by November 1, 2021.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https www.regulations.gov. Follow the instructions for submitting comments.
Fax: 2024932251.
Mail: U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays.
For the material incorporated by reference IBR in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
89990 1000; 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 SUMMARY:

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