Quiero saber acerca de...

32656

Federal Register / Vol. 86, No. 117 / Tuesday, June 22, 2021 / Proposed Rules
2 Model A319111, 112, 113, 114, 115, 131, 132, and 133 airplanes.
3 Model A320211, 212, 214, 216, 231, 232, and 233 airplanes.
4 Model A321111, 112, 131, 211, 212, 213, 231, and 232 airplanes.
d Subject Air Transport Association ATA of America Code 25, Equipment/furnishings.
e Reason This AD was prompted by reports of damaged lower lateral fittings of the 80VU
rack, and reports of new damage on airplanes on which certain optional service information had been accomplished. The FAA is issuing this AD to address damage or cracking of the 80VU fittings and supports, which could lead to possible disconnection of the cable harnesses to one or more computers, and if occurring during a critical phase of flight, could result in reduced control of the airplane.
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 20210045, dated February 16, 2021 EASA AD 20210045.

lotter on DSK11XQN23PROD with PROPOSALS1

h Exceptions to EASA AD 20210045
1 Where EASA AD 20210045 refers to its effective date, this AD requires using the effective date of this AD.
2 The remarks section of EASA AD 2021
0045 does not apply to this AD.
3 Where paragraph 2 of EASA AD 2021
0045 specifies any discrepancy, for this AD
any discrepancy includes broken fittings, missing bolts, an electronics rack FIN 80VU
that is in contact with structure, any bush that has migrated, burred material, and cracks.
4 Paragraph 4 of EASA AD 20210045
specifies to report inspection results to Airbus within a certain compliance time. For this AD, report inspection results at the applicable time specified in paragraph h4i or ii of this AD.
i If the inspection was done on or after the effective date of this AD: Submit the report within 90 days after the inspection.
ii If the inspection was done before the effective date of this AD: Submit the report within 90 days after the effective date of this AD.
i 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
VerDate Sep<11>2014

18:16 Jun 21, 2021

Jkt 253001

information directly to the Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph j2 of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
i Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.
ii AMOCs approved previously for AD
20132511 are approved as AMOCs for the corresponding provisions of EASA AD 2021
0045 that are required by paragraph g of this AD.
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
20210045 that contains RC procedures and tests: Except as required by paragraph i2
of this AD, RC 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.
4 Paperwork Reduction Act Burden Statement: A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 21200056. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. All responses to this collection of information are mandatory as required by this AD. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to Information Collection Clearance Officer, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX
761771524.
j Related Information 1 For information about EASA AD 2021
0045, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49
221 8999 000; email ADs@easa.europa.eu;

PO 00000

Frm 00004

Fmt 4702

Sfmt 4702

internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https ad.easa.europa.eu. 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.
FAA20210506.
2 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.
Issued on June 15, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202113057 Filed 62121; 8:45 am BILLING CODE 491013P

ENVIRONMENTAL PROTECTION
AGENCY
40 CFR Part 52
EPAR08OAR20210262; FRL10025
02Region 8

Approval and Promulgation of Implementation Plans; Colorado;
Revisions to Regulation Number 7;
Aerospace, Oil and Gas, and Other RACT Requirements for 2008 8-Hour Ozone Standard for the Denver Metro/
North Front Range Nonattainment Area Environmental Protection Agency EPA.
ACTION: Proposed rule.
AGENCY:

The Environmental Protection Agency EPA is proposing approval of State Implementation Plan SIP
revisions submitted by the State of Colorado on May 14, 2018, May 8, 2019, and May 13, 2020. The revisions are to Colorado Air Quality Control Commission Commission or AQCC
Regulation Number 7 Reg. 7. The revisions to Reg. 7 address Colorados SIP obligation to require reasonably available control technology RACT for sources covered by the 2016 oil &
natural gas control techniques guidelines CTG or CTGs for Moderate nonattainment areas under the 2008
ozone National Ambient Air Quality Standard NAAQS; update RACT
requirements for major sources of volatile organic compounds VOC and nitrogen oxides NOx; reorganize the regulation; add incorporation by reference dates to rules and reference
SUMMARY:

E:FRFM22JNP1.SGM

22JNP1