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Federal Register / Vol. 86, No. 195 / Wednesday, October 13, 2021 / Rules and Regulations airplane flight manual, however this AD
requires amending the applicable existing AFM and applicable corresponding operational procedures.
4 The Remarks section of EASA AD
20210061 does not apply to this AD.

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:

20212004 Airbus SAS: Amendment 39
21742; Docket No. FAA20210563;
Project Identifier MCAI202100282T.
a Effective Date This airworthiness directive AD is effective November 17, 2021.
b Affected ADs None.
c Applicability This AD applies to Airbus SAS Model A350941 and 1041 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency EASA AD
20210061, dated March 5, 2021 EASA AD
20210061.
d Subject Air Transport Association ATA of America Code 31, Instruments.
e Reason This AD was prompted by a report that during flight tests, the opening of the ram air outlet flaps was found to cause a disturbance of the air flow around the ram air turbine RAT when the landing gear is extended.
The FAA is issuing this AD to address a nonnegligible effect on the overall performance of the RAT in case of total engine flame out TEFO or electrical emergency configuration combined with the auxiliary power unit APU running, which could lead to partial or total loss of RAT electrical power generation when the RAT is deployed in an emergency condition with the landing gear extended, and possibly result in reduced control of the airplane.
f Compliance Comply with this AD within the compliance times specified, unless already done.

jspears on DSK121TN23PROD with RULES1

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 20210061.
h Exceptions to EASA AD 20210061
1 Where EASA AD 20210061 refers to its effective date, this AD requires using the effective date of this AD.
2 Where paragraph 1 of EASA AD 2021
0061 specifies to inform all flight crews, and, thereafter, operate the aeroplane accordingly, this AD does not require those actions as those actions are already required by existing FAA operating regulations.
3 Paragraph 1 of EASA AD 20210061
specifies amending the applicable AFM

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15:51 Oct 12, 2021

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i Additional 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 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: 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 Dan Rodina, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 2062313225; email Dan.Rodina@
faa.gov.
k 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 20210061, dated March 5, 2021.

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ii Reserved 3 For EASA AD 20210061, 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.
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 September 15, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202122198 Filed 101221; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 97
Docket No. 31394; Amdt. No. 3978

Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures;
Miscellaneous Amendments Federal Aviation Administration FAA, DOT.
ACTION: Final rule.
AGENCY:

This rule amends, suspends, or removes Standard Instrument Approach Procedures SIAPs and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
DATES: This rule is effective October 13, 2021. The compliance date for each SIAP, associated Takeoff Minimums, and ODP is specified in the amendatory provisions.
SUMMARY:

E:FRFM13OCR1.SGM

13OCR1