Federal Register / Vol. 87, No. 60 / Tuesday, March 29, 2022 / Rules and Regulations 17941 

elements, which could result in reduced 

structural integrity of the fuselage. 

(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, European Union Aviation 

Safety Agency (EASA) AD 2021–0093, dated 

March 30, 2021 (EASA AD 2021–0093). 

(h) Exceptions to EASA AD 2021–0093 

(1) Where EASA AD 2021–0093 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

(2) The requirements specified in 

paragraphs (1) and (2) of EASA AD 2021– 

0093 do not apply to this AD. 

(3) Paragraph (3) of EASA AD 2021–0093 

specifies revising ‘‘the approved AMP’’ 

within 12 months after its effective date, but 

this AD requires revising the existing 

maintenance or inspection program, as 

applicable within 90 days after the effective 

date of this AD. 

(4) The initial compliance time for doing 

the tasks specified in paragraph (3) of EASA 

2021–0093 is at the applicable ‘‘thresholds’’ 

as incorporated by the requirements of 

paragraph (3) of EASA AD 2021–0093, or 

within 90 days after the effective date of this 

AD, whichever occurs later. 

(5) The provisions specified in paragraph 

(4) of EASA AD 2021–0093 do not apply to 

this AD. 

(6) The ‘‘Remarks’’ section of EASA AD 

2021–0093 does not apply to this AD. 

(i) Provisions for Alternative Actions and 

Intervals 

After the existing maintenance or 

inspection program has been revised as 

required by paragraph (g) of this AD, no 

alternative actions (e.g., inspections) or 

intervals are allowed unless they are 

approved as specified in the provisions of the 

‘‘Ref. Publications’’ section of EASA AD 

2021–0093. 

(j) Terminating Action for Certain 

Requirements of AD 2019–21–01 and AD 

2020–23–11 

(1) Accomplishing the actions required by 

this AD terminates the corresponding 

requirements of AD 2019–21–01, for the tasks 

identified in the service information referred 

to in EASA AD 2021–0093 only. 

(2) Accomplishing the actions required by 

this AD terminates the corresponding 

requirements of AD 2020–23–11, for the tasks 

identified in the service information referred 

to in EASA AD 2021–0093 only. 

(k) 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 (l) 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 SAS’s 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 (k)(2) 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 operator’s 

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. 

(l) 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 206–231–3225; email dan.rodina@

faa.gov. 

(m) 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. 552(a) 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 2021–0093, dated March 30, 

2021. 

(ii) [Reserved] 

(3) For EASA AD 2021–0093, 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 

206–231–3195. 

(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 December 15, 2021. 

Ross Landes, 

Deputy Director for Regulatory Operations, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

Note: This document was received for 

publication by the Office of the Federal 

Register on March 24, 2022. 

[FR Doc. 2022–06535 Filed 3–28–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 170 

Food Additives 

CFR Correction 

This rule is being published by the 

Office of the Federal Register to correct 

an editorial or technical error that 

appeared in the most recent annual 

revision of the Code of Federal 

Regulations. 

■ In Title 21 of the Code of Federal 

Regulations, Parts 170 to 199, revised as 

of April 1, 2021, in § 170.30, reinstate 

paragraph (g) to read as follows: 

§ 170.30 Eligibility for classification as 

generally recognized as safe (GRAS). 

* * * * * 

(g) A food ingredient that is not GRAS 

or subject to a prior sanction requires a 

food additive regulation promulgated 

under section 409 of the act before it 

may be directly or indirectly added to 

food. 

* * * * * 

[FR Doc. 2022–06677 Filed 3–28–22; 8:45 am] 

BILLING CODE 0099–10–D 


lotter on DSK11XQN23PROD with RULES1