Quiero saber acerca de...

6276

Federal Register / Vol. 86, No. 12 / Thursday, January 21, 2021 / Proposed Rules
the applicable times specified in the Compliance paragraph of Boeing Alert Requirements Bulletin 73727A1313 RB, Revision 1, dated June 24, 2020, or Boeing Alert Requirements Bulletin 73727A1314
RB, Revision 1, dated June 24, 2020, as applicable, except as specified by paragraph i of this AD, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 73727A1313 RB, Revision 1, dated June 24, 2020, or Boeing Alert Requirements Bulletin 73727A1314
RB, Revision 1, dated June 24, 2020, as applicable.
Note 1 to paragraph h: Guidance for accomplishing the actions required by paragraph h of this AD can be found in Boeing Alert Service Bulletin 73727A1313, Revision 1, dated June 24, 2020, and Boeing Alert Service Bulletin 73727A1314, Revision 1, dated June 24, 2020, which are referred to in Boeing Alert Requirements Bulletin 73727A1313 RB, Revision 1, dated June 24, 2020, and Boeing Alert Requirements Bulletin 73727A1314 RB, Revision 1, dated June 24, 2020, respectively.
i Exception to Service Information Specifications Where Boeing Alert Requirements Bulletin 73727A1313 RB, Revision 1, dated June 24, 2020, and Boeing Alert Requirements Bulletin 73727A1314 RB, Revision 1, dated June 24, 2020, use the phrase the original issue date of each Requirements Bulletin for compliance, this AD requires using the effective date of this AD.

jbell on DSKJLSW7X2PROD with PROPOSALS

j Credit for Previous Actions This paragraph provides credit for the actions specified in paragraph h of this AD, if those actions were performed before the effective date of this AD using Boeing Alert Requirements Bulletin 73727A1313 RB, dated March 18, 2020, or Boeing Alert Requirements Bulletin 73727A1314 RB, dated March 18, 2020.
k Parts Installation Limitation 1 For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after the effective date of this AD: As of the effective date of this AD, no person may install a captains or first officers rudder pedal cover or shroud assembly on any airplane, unless the cover or shroud assembly has been modified in accordance with the requirements of paragraph h of this AD.
2 For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued prior to the effective date of this AD: After the modification required by paragraph h of this AD has been done, no person may install a captains or first officers rudder pedal cover or shroud assembly on any airplane, unless the cover or shroud assembly has been modified in accordance with the requirements of paragraph h of this AD.
Reinstallation of a rudder pedal cover or shroud assembly that has not been modified in accordance with paragraph h of this AD
but has been removed for other maintenance is allowed.

VerDate Sep<11>2014

15:58 Jan 19, 2021

Jkt 253001

l Alternative Methods of Compliance AMOCs 1 The Manager, Seattle ACO 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph m1 of this AD. Information may be emailed to: 9ANM-Seattle-ACO-AMOC-Requests@faa.gov.
2 Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.
3 An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by The Boeing Company Organization Designation Authorization ODA that has been authorized by the Manager, Seattle ACO Branch, FAA, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD.
4 AMOCs approved previously for AD
20171413 are not approved as AMOCs for the corresponding provisions of this AD.
5 For service information that contains steps that are labeled as Required for Compliance RC, the provisions of paragraphs l5i and ii of this AD apply.
i The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or substep is labeled RC Exempt, then the RC
requirement is removed from that step or substep. An AMOC is required for any deviations to RC steps, including substeps and identified figures.
ii Steps not labeled 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 RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition.
m Related Information 1 For more information about this AD, contact Douglas Tsuji, Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206
2313548; email: douglas.tsuji@faa.gov.
2 For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services C&DS, 2600 Westminster Blvd., MC 110SK57, Seal Beach, CA 907405600;
telephone 5627971717; internet https
www.myboeingfleet.com. You may view this referenced service information 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.

PO 00000

Frm 00008

Fmt 4702

Sfmt 4702

Issued on December 17, 2020.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202101161 Filed 11921; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20200587; Product Identifier 2020NM086AD
RIN 2120AA64

Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration FAA, DOT.
ACTION: Supplemental notice of proposed rulemaking SNPRM;
reopening of comment period.
AGENCY:

The FAA is revising an earlier proposal for all The Boeing Company Model 737100, 200, 200C, 300, 400, and 500 series airplanes. This action revises the notice of proposed rulemaking NPRM by reducing the compliance time for certain airplanes.
The FAA is proposing this airworthiness directive AD to address the unsafe condition on these products.
Since these actions would impose an additional burden over that in the NPRM, the FAA is reopening the comment period to allow the public the chance to comment on these changes.
DATES: The comment period for the NPRM published in the Federal Register on July 28, 2020 85 FR 45355, is reopened.
The FAA must receive comments on this SNPRM by March 8, 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, M30, 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 Boeing service information identified in this SNPRM, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services SUMMARY:

E:FRFM21JAP1.SGM

21JAP1