13640 Federal Register / Vol. 86, No. 45 / Wednesday, March 10, 2021 / Rules and Regulations 

(3) Where Table 2 of EASA AD 2020–0264 

specifies a column heading of ‘‘FH 

Accumulated,’’ for this AD use hours timein-service accumulated as of the effective 

date of this AD. 

(4) Where EASA AD 2020–0264 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

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

2020–0264 does not apply to this AD. 

(6) Although the service information 

referenced in EASA AD 2020–0264 specifies 

to return certain parts, this AD requires 

removing those parts from service instead. 

(7) Where the service information 

referenced in EASA AD 2020–0264 specifies 

‘‘compliance with the works steps concerned 

with the check is described in a video’’ this 

AD requires a complete rotation of the 

swashplate in both directions using a rate of 

one revolution per minute. 

(8) Where EASA AD 2020–0264 refers to 

flight hours (FH), this AD requires using 

hours time-in-service. The guidance provided 

by Note 1 to Table 1 and Table 2 in EASA 

AD 2020–0264 is still applicable. 

(i) No Reporting Requirement 

Although the service information 

referenced in EASA AD 2020–0264 specifies 

to submit certain information to the 

manufacturer, this AD does not include that 

requirement. 

(j) Special Flight Permit 

Special flight permits, as described in 14 

CFR 21.197 and 21.199, are not allowed. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Strategic Policy 

Rotorcraft Section, 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 Strategic Policy 

Rotorcraft Section, send it to: Manager, 

Strategic Policy Rotorcraft Section, FAA, 

10101 Hillwood Pkwy., Fort Worth, TX 

76177; phone: 817–222–5110. Information 

may be emailed to: 9-ASW-FTW-AMOCRequests@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. 

(l) Related Information 

(1) For more information about this AD, 

contact Kathleen Arrigotti, Aerospace 

Engineer, Large Aircraft Section, 

International Validation Branch, FAA, 2200 

South 216th St., Des Moines, WA 98198; 

phone and fax: 206–231–3218; email: 

kathleen.arrigotti@faa.gov. 

(m) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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 2020–0264, dated December 2, 

2020. 

(ii) [Reserved] 

(3) For EASA AD 2020–0264, contact the 

EASA, Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; phone: +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 service information 

at the FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood Pkwy., 

Room 6N–321, Fort Worth, TX 76177. For 

information on the availability of this 

material at the FAA, call 817–222–5110. This 

material may be found in the AD docket on 

the internet at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2021–0096. 

(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 fedreg.legal@

nara.gov, or go to https://www.archives.gov/ 

federal-register/cfr/ibr-locations.html. 

Issued on February 10, 2021. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2021–04869 Filed 3–9–21; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–0673; Product 

Identifier 2020–NM–076–AD; Amendment 

39–21395; AD 2021–02–12] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to all Airbus SAS Model 

A330–200 series airplanes, Model 

A330–200 Freighter series airplanes, 

Model A330–300 series airplanes, 

Model A330–900 series airplanes, 

Model A340–200 series airplanes, 

Model A340–300 series airplanes, 

Model A340–500 series airplanes, 

Model A340–600 series airplanes, 

Model A380–800 series airplanes; and 

Model A350–941 and –1041 airplanes. 

As published, multiple references to a 

European Union Aviation Safety Agency 

(EASA) AD number are incorrect 

throughout the AD. This document 

corrects those errors. In all other 

respects, the original document remains 

the same. 

DATES: This correction is effective 

March 30, 2021. The effective date of 

AD 2021–02–12 remains March 30, 

2021. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of March 30, 2021 (86 FR 10787, 

February 23, 2021). 

ADDRESSES: For material incorporated 

by reference (IBR) in this AD, 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 IBR material on the EASA 

website at https://ad.easa.europa.eu. 

You may view this IBR 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. 

It is also available in the AD docket on 

the internet at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

0673. 

Examining the AD Docket 

You may examine the AD docket on 

the internet at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2020– 

0673; or in person at Docket Operations 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

The AD docket contains this final rule, 

any comments received, and other 

information. The address for Docket 

Operations is U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE, 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aerospace Engineer, Large 

Aircraft Section, International 

Validation Branch, FAA, 2200 South 

216th St., Des Moines, WA 98198; 

phone and fax: 206–231–3225; email: 

dan.rodina@faa.gov. 

SUPPLEMENTARY INFORMATION: AD 2021– 

02–12, Amendment 39–21395 (86 FR 

10787, February 23, 2021) (AD 2021– 

02–12), currently requires repair of each 

affected part, or replacement with a 

serviceable part, as specified in an 

EASA AD. AD 2021–02–12 applies to all 

Airbus SAS Model A330–200 series 

airplanes, Model A330–200 Freighter 

series airplanes, Model A330–300 series 

Federal Register / Vol. 86, No. 45 / Wednesday, March 10, 2021 / Rules and Regulations 13641 

airplanes, Model A330–900 series 

airplanes, Model A340–200 series 

airplanes, Model A340–300 series 

airplanes, Model A340–500 series 

airplanes, Model A340–600 series 

airplanes, Model A380–800 series 

airplanes; and Model A350–941 and 

–1041 airplanes. 

Need for the Correction 

As published, the EASA AD number 

in the preamble and regulatory text is 

incorrectly identified as ‘‘EASA AD 

2020–100R1,’’ where the correct 

identification is ‘‘EASA AD 2020– 

0100R1.’’ 

Related Service Information Under 1 

CFR Part 51 

EASA AD 2020–0100R1, dated 

November 4, 2020, describes procedures 

for repair of each affected part, or 

replacement with a serviceable part. 

This material is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section 

Correction of Publication 

This document corrects multiple 

errors and correctly adds the AD as an 

amendment to 14 CFR 39.13. Although 

no other part of the preamble or 

regulatory information has been 

corrected, the FAA is publishing the 

entire rule in the Federal Register. 

The effective date of this AD remains 

March 30, 2021. 

Since this action only corrects 

references to an EASA AD number, it 

has no adverse economic impact and 

imposes no additional burden on any 

person. Therefore, the FAA has 

determined that notice and public 

procedures are unnecessary. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Correction 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, the Federal Aviation 

Administration amends part 39 of the 

Federal Aviation Regulations (14 CFR 

part 39) as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

39.13 [Corrected] 

■ 2. The FAA amends § 39.13 by 

revising the following new 

airworthiness directive to read: 

2021–02–12 Airbus SAS: Amendment 39– 

21395; Docket No. FAA–2020–0673; 

Product Identifier 2020–NM–076–AD. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective March 30, 2021. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Airbus SAS 

airplanes identified in paragraphs (c)(1) 

through (10) of this AD, certificated in any 

category. 

(1) Model A330–201, –202, –203, –223, and 

–243 airplanes. 

(2) Model A330–223F and –243F airplanes. 

(3) Model A330–301, –302, –303, –321, 

–322, –323, –341, –342, and –343 airplanes. 

(4) Model A330–941 airplanes. 

(5) Model A340–211, –212, and –213 

airplanes. 

(6) Model A340–311, –312, and –313 

airplanes. 

(7) Model A340–541 airplanes. 

(8) Model A340–642 airplanes. 

(9) Model A350–941 and –1041 airplanes. 

(10) Model A380–841, –842, and –861 

airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25, Equipment/furnishings. 

(e) Reason 

This AD was prompted by a report of a 

quality issue with a certain repair method of 

damage-through honeycomb core cargo 

linings by speed patches applied to both 

sides. The FAA is issuing this AD to address 

reduced ability of repaired linings to contain 

smoke or fire, resulting in an increased risk 

of an uncontained fire in the cargo 

compartment and consequent structural 

damage to 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 2020–0100R1, 

dated November 4, 2020 (EASA AD 2020– 

0100R1). 

(h) Exceptions to EASA AD 2020–0100R1 

(1) Where EASA AD 2020–0100R1 refers to 

its effective date, this AD requires using the 

effective date of this AD. 

(2) Where EASA AD 2020–0100R1 refers to 

‘‘19 May 2020 [the effective date of EASA AD 

2020–0100 at original issue],’’ this AD 

requires using the effective date of this AD. 

(3) Where task Aircraft Maintenance 

Manual (AMM) A330–A–25–XX–3743– 

02001–690A–C specified in Airbus Service 

Bulletin A330–25–3743, dated September 23, 

2019, states the measured dimension shall be 

equal to or more than ‘‘30 mm (1.81 in),’’ this 

AD requires using the measured dimension 

of ‘‘30 mm (1.18 in).’’ 

(4) Where AMM task A330–A–25–XX– 

3743–01001–520A–A of Airbus Service 

Bulletin A330–25–3743, dated September 23, 

2019, states, ‘‘For the FWD cargocompartment, refer to Ref. AMM Task 25–54– 

00–000–801,’’ this AD requires using, ‘‘For 

the FWD cargo-compartment, refer to Ref. 

AMM Task 25–52–00–000–801.’’ 

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

2020–0100R1 does not apply to 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 

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 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 (i)(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. 

(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; phone and fax: 

206–231–3225; email: dan.rodina@faa.gov. 

13642 Federal Register / Vol. 86, No. 45 / Wednesday, March 10, 2021 / Rules and Regulations 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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. 

(3) The following service information was 

approved for IBR on March 30, 2021 (86 FR 

10787, February 23, 2021). 

(i) European Union Aviation Safety Agency 

(EASA) AD 2020–0100R1, dated November 4, 

2020. 

(ii) [Reserved] 

(4) For EASA AD 2020–0100R1, contact the 

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. 

(5) 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. This material may be found 

in the AD docket on the internet at https:// 

www.regulations.gov by searching for and 

locating Docket No. FAA–2020–0673. 

(6) 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 fedreg.legal@

nara.gov, or go to: https://www.archives.gov/ 

federal-register/cfr/ibr-locations.html. 

Issued on March 3, 2021. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2021–04784 Filed 3–9–21; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2020–0923; Airspace 

Docket No. 20–AEA–18] 

RIN 2120–AA66 

Amendment, Establishment, and 

Revocation of Multiple Air Traffic 

Service (ATS) Routes in the Vicinity of 

Henderson, WV 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action amends Jet Route 

J–134, Area Navigation (RNAV) route 

Q–67, and VHF Omnidirectional Range 

(VOR) Federal airways V–45 and V–119; 

establishes RNAV route Q–176; and 

removes Jet Route J–91 and VOR Federal 

airway V–174 in the vicinity of 

Henderson, WV. The Air Traffic Service 

(ATS) route modifications are necessary 

due to the planned decommissioning of 

the VOR portion of the Henderson, WV, 

VOR/Tactical Air Navigation (VORTAC) 

navigation aid (NAVAID). The 

Henderson VORTAC provides 

navigation guidance for portions of the 

affected air traffic service (ATS) routes 

and the VOR portion is being 

decommissioned as part of the FAA’s 

VOR Minimum Operational Network 

(MON) program. 

DATES: Effective date 0901 UTC, June 

17, 2021. The Director of the Federal 

Register approves this incorporation by 

reference action under 1 CFR part 51, 

subject to the annual revision of FAA 

Order 7400.11 and publication of 

conforming amendments. 

ADDRESSES: FAA Order 7400.11E, 

Airspace Designations and Reporting 

Points, and subsequent amendments can 

be viewed online at https://

www.faa.gov/air_traffic/publications/. 

For further information, you can contact 

the Rules and Regulations Group, 

Federal Aviation Administration, 800 

Independence Avenue SW, Washington, 

DC 20591; telephone: (202) 267–8783. 

The Order is also available for 

inspection at the National Archives and 

Records Administration (NARA). For 

information on the availability of FAA 

Order 7400.11E at NARA, email: 

fedreg.legal@nara.gov or go to https://

www.archives.gov/federal-register/cfr/ 

ibr-locations.html. 

FOR FURTHER INFORMATION CONTACT: 

Colby Abbott, Rules and Regulations 

Group, Office of Policy, Federal 

Aviation Administration, 800 

Independence Avenue SW, Washington, 

DC 20591; telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

Authority for This Rulemaking 

The FAA’s authority to issue rules 

regarding aviation safety is found in 

Title 49 of the United States Code. 

Subtitle I, Section 106 describes the 

authority of the FAA Administrator. 

Subtitle VII, Aviation Programs, 

describes in more detail the scope of the 

agency’s authority. This rulemaking is 

promulgated under the authority 

described in Subtitle VII, Part A, 

Subpart I, Section 40103. Under that 

section, the FAA is charged with 

prescribing regulations to assign the use 

of the airspace necessary to ensure the 

safety of aircraft and the efficient use of 

airspace. This regulation is within the 

scope of that authority as it modifies the 

route structure as necessary to preserve 

the safe and efficient flow of air traffic 

within the National Airspace System. 

History 

The FAA published a notice of 

proposed rulemaking (NPRM) for 

Docket No. FAA–2020–0923 in the 

Federal Register (85 FR 70093; 

November 4, 2020), to amend Jet Route 

J–134, RNAV route Q–67, and VOR 

Federal airways V–45 and V–119; 

establish RNAV route Q–176; and 

remove Jet Route J–91 and VOR Federal 

airway V–174 in the vicinity of 

Henderson, WV. The proposed 

amendment, establishment, and 

revocation actions were due to the 

planned decommissioning of the VOR 

portion of the Henderson, WV, VORTAC 

NAVAID. Interested parties were invited 

to participate in this rulemaking effort 

by submitting written comments on the 

proposal. No comments were received. 

Subsequent to the NPRM, the Office 

of the Federal Register published a 

NPRM correction for Docket No. FAA– 

2020–0923 in the Federal Register (85 

FR 71293; November 9, 2020), 

correcting the RNAV route formatting 

for the Q–67 and Q–176 descriptions in 

the regulatory text and also adding the 

missing ‘‘Paragraph 6010(a) Domestic 

VOR Federal Airways’’ heading between 

the RNAV route Q–176 and VOR 

Federal airway V–45 descriptions in the 

regulatory text. The correct RNAV route 

formatting and Domestic VOR Federal 

Airways heading are included in the 

regulatory text in this rule. 

Additionally, subsequent to the 

NPRM, the FAA published a rule for 

Docket No. FAA–2020–0709 in the 

Federal Register (85 FR 79117; 

December 9, 2020), amending VOR 

Federal airway V–119 by removing the 

airway segment overlying the Clarion, 

PA, VOR/Distance Measuring 

Equipment (VOR/DME) between the 

Indian Head, PA, VORTAC and the 

Clarion, PA, VOR/DME. That airway 

amendment, effective February 25, 

2021, is included in this rule. 

Lastly, the state reference for the 

Henderson, WV, VORTAC was 

incorrectly listed as Kentucky (KY) in 

the Proposal section of the NPRM for Jet 

Routes J–91 and J–134. The correct state 

is WV and this action corrects those 

errors. 

Jet Routes are published in paragraph 

2004, United States RNAV Q-routes are 

published in paragraph 2006, and VOR 

Federal airways are published in 

paragraph 6010(a) of FAA Order 

7400.11E, dated July 21, 2020, and 

effective September 15, 2020, which is 

incorporated by reference in 14 CFR 

71.1. The ATS routes listed in this 

document will be published 

subsequently in the Order.