Food Additives, 17941 [2022-06677]
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Federal Register / Vol. 87, No. 60 / Tuesday, March 29, 2022 / Rules and Regulations
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.
lotter on DSK11XQN23PROD with RULES1
(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
VerDate Sep<11>2014
16:11 Mar 28, 2022
Jkt 256001
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.
PO 00000
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17941
(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
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[Federal Register Volume 87, Number 60 (Tuesday, March 29, 2022)]
[Rules and Regulations]
[Page 17941]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-06677]
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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.
0
In Title 21 of the Code of Federal Regulations, Parts 170 to 199,
revised as of April 1, 2021, in Sec. 170.30, reinstate paragraph (g)
to read as follows:
Sec. 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
