40779 Federal Register / Vol. 86, No. 143 / Thursday, July 29, 2021 / Rules and Regulations 
Authority: 15 U.S.C. 634(b)(6), (b)(7), 
(b)(14), (h), and note, 636(a), (h), and (m), 
636m, 650, 687(f), 696(3), 697, 697a, and 697e; Public Law 111–5, 123 Stat. 115; Public Law 111–240, 124 Stat. 2504; Public Law 116–260, 134 Stat. 1182. 
■2. Amend § 120.882 as follows: 
■a. Remove the number ‘‘50’’ in 
paragraph (e) introductory text and add 
the number ‘‘100’’ in its place. 
■b. Revise paragraphs (g)(3) and (11); 
■c. Redesignate paragraph (g)(15) as 
paragraph (g)(16); 
■d. Add a new paragraph (g)(15); 
■e. In the newly redesignated 
paragraph (g)(16): 
■i. Remove the paragraph heading; 
■ii. In the definition for the term 
Qualified debt: 
■A. Redesignate paragraphs (i) through 
(vii) as paragraphs (A) through (G); 
■B. Revise newly redesignated 
paragraph (A); 
■C. Remove newly redesignated 
paragraphs (B) and (G) and further redesignate paragraphs (C) through (F) as paragraphs (B) through (E); 
■D. In newly redesignated paragraph 
(B), remove ‘‘(iii)’’, ‘‘13 CFR 120.131 and 13 CFR 120.870(b)’’, and ‘‘13 CFR 120.131(b)’’ and add in their places ‘‘(B)’’, ‘‘§§ 120.131 and 120.870(b)’’, and ‘‘§ 120.131(b)’’, respectively; 
■E. Add the word ‘‘and’’ at the end of 
newly redesignated paragraph (D); and 
■F. Revise newly redesignated 
paragraph (E); and 
■iii. Revise the definition for the term 
Same institution debt. 
The revisions and addition read as 
follows: 
§ 120.882 Eligible Project costs for 504 
loans. 
* * * * * 
(g) * * * 
(3) A loan that is subject to a 
guarantee by a Federal agency or department may be refinanced under the following conditions and requirements: 
(i) An existing 504 loan may be 
refinanced if both the Third Party Loan and the 504 Loan are being refinanced or the Third Party Loan has been paid in full. 
(ii) An existing 7(a) loan may be 
refinanced if the CDC verifies in writing that the present lender is either unwilling or unable to modify the current payment schedule. In the case of same institution debt, if the Third Party Lender or the CDC affiliate as authorized under § 120.820 is the 7(a) lender, the loan will be eligible for 504 refinancing only if the lender is unable to modify the terms of the existing loan because a secondary market investor will not agree to modified terms. (iii) The refinancing will provide a 
substantial benefit to the borrower. For 
purposes of this paragraph (g)(3)(iii), ‘‘substantial benefit’’ means that the portion of the new installment amount attributable to the debt being refinanced must be at least 10 percent less than the existing installment amount(s). Prepayment penalties, financing fees, and other financing costs must be added to the amount being refinanced in calculating the percentage reduction in the new installment payment, but the portion of the new installment amount attributable to Eligible Business Expenses (as described in paragraph (g)(6)(ii) of this section) is not included in this calculation. Exceptions to the 10 percent reduction requirement may be approved by the Director, Office of Financial Assistance (D/FA) or designee for good cause. PCLP CDCs may not use their delegated authority to approve a loan requiring the exception in this paragraph (g)(3)(iii). 
* * * * * 
(11) PCLP CDCs may not approve the 
refinancing of same institution debt 
under their delegated authority and must submit the application to SBA for approval. 
* * * * * 
(15) Notwithstanding § 120.860, a 
debt may be refinanced under this 
paragraph (g) if it does not meet the job creation or other economic development objectives set forth in § 120.861 or § 120.862. In such case, the 504 loan may not exceed the product obtained by multiplying the number of employees of the Borrower by $75,000. The number of employees of the Borrower is equal to the sum of: 
(i) The number of full-time employees 
of the Borrower on the date of the application; and 
(ii) The product obtained by 
multiplying: 
(A) The number of part-time 
employees of the Borrower on the date of the application; by 
(B) The quotient obtained by dividing 
the average number of hours each part- time employee of the Borrower works each week by 40. 
Example to paragraph (g)(15): 30 full- 
time employees and 35 part-time employees working 20 hours per week is calculated as follows: 30 + (35 × (20/ 
40)) = 47.5. The maximum amount of the 504 loan would be 47.5 multiplied by $75,000, or $3,562,500. 
(16) * * * 
Qualified debt ***  (A) That was incurred not less than 6 
months before the date of the 
application for refinancing available 
under this paragraph (g). 
* * * * * (E) That is not a Third Party Loan that 
is part of an existing 504 Project, except 
as allowed under paragraph (g)(3) of this section. 
* * * * * 
Same institution debt means any debt 
of the CDC or the Third Party Lender, 
or an affiliate of either, that is providing funds for the refinancing. 
Isabella Casillas Guzman, 
Administrator. 
[FR Doc. 2021–15975 Filed 7–28–21; 8:45 am] 
BILLING CODE 8026–03–P 
DEPARTMENT OF TRANSPORTATION 
Federal Aviation Administration 
14 CFR Part 39 
[Docket No. FAA–2021–0605; Project 
Identifier AD–2021–00805–R; Amendment 39–21664; AD 2021–15–52] 
RIN 2120–AA64 
Airworthiness Directives; Various 
Restricted Category Helicopters 
AGENCY : Federal Aviation 
Administration (FAA), DOT. 
ACTION : Final rule; request for 
comments. 
SUMMARY : The FAA is adopting a new 
airworthiness directive (AD) for various 
restricted category helicopters originally manufactured by Bell Textron Inc. This AD was prompted by a fatal accident in which an outboard main rotor hub strap pin (pin) sheared off during flight, resulting in the main rotor blade and the main rotor head detaching from the helicopter. This AD requires removing certain pins from service and prohibits installing those pins on any helicopter. The FAA previously sent an emergency AD to all known U.S. owners and operators of these restricted category helicopters and is now issuing this AD to address the unsafe condition on these products. 
DATES : This AD is effective August 13, 
2021. Emergency 2021–15–52, issued on July 8, 2021, which contained the requirements of this amendment, was effective with actual notice. 
The FAA must receive comments on 
this AD by September 13, 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: (202) 493–2251. 
•Mail: U.S. Department of 
Transportation, Docket Operations, 
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M–30, West Building Ground Floor, 
Room W12–140, 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 service information identified in 
this final rule, contact Bell Textron, Inc., P.O. Box 482, Fort Worth, TX 76101, United States; telephone 1–450–437– 2862 or 1–800–363–8023; fax 1–450– 433–0272; email productsupport@bellflight.com; or at https://
www.bellflight.com/support/contact- support. 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. 
Examining the AD Docket 
You may examine the AD docket at 
https://www.regulations.gov by 
searching for and locating Docket No. 
FAA–2021–0605; 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, the Transport Canada AD, any comments received, and other information. The street address for Docket Operations is listed above. 
FOR FURTHER INFORMATION CONTACT : 
David Wilson, Aerospace Engineer, DSCO Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5786; email david.wilson@faa.gov. 
SUPPLEMENTARY INFORMATION : 
Background 
On July 6, 2021, the FAA issued 
Emergency AD 2021–15–51 (Emergency AD 2021–15–51) for Bell Textron Inc. Model 204B, 205A, 205A–1, 205B, and 212 helicopters. That action was prompted by a Bell Textron Inc., Model 212 helicopter fatal accident in which a pin part number (P/N) 204–012–104– 005 with a serial number (S/N) prefix ‘‘FNFS’’ sheared off during flight, resulting in the main rotor blade and the main rotor head detaching from the helicopter. The pin had accumulated only 20 total hours time-in-service (TIS). 
An inspection of a different Model 212 helicopter revealed that another pin installed, and made by the same manufacturer with the same S/N prefix, was deformed; this pin had accumulated only 29 total hours TIS. Failure of the pin could result in the main rotor blade detaching from the helicopter and subsequent loss of control of the helicopter. Transport Canada, which is the 
aviation authority for Canada, has issued Canadian Emergency AD CF– 2021–23, dated July 5, 2021 (Transport Canada Emergency AD CF–2021–23), to correct an unsafe condition for Bell Helicopter Textron Inc., Model 204B helicopters, S/Ns 2001 through 2070 and 2196 through 2199; Model 205A–1 helicopters, S/Ns 30001 through 30065, 30067 through 30165, 30167 through 30187, 30189 through 30296, and 30298 through 30332; Model 205B helicopters, S/Ns 30066, 30166, 30188, and 30297; and Model 212 helicopters, S/Ns 30501 through 30999, 31101 through 31311, 32101 through 32142, and 35001 through 35103. Transport Canada advises that during an investigation of a Bell Textron Inc., Model 212 fatal accident in Canada, it was discovered that a pin P/N 204–012–104–005 with an S/N prefix ‘‘FNFS’’, sheared off during flight, leading to detachment of the main rotor blade and the main rotor head. The pin had accumulated only 20 hours of service, and inspection of another Canadian Bell Textron Inc., Model 212 helicopter found a pin of the same P/N, made by the same manufacturer, with the same S/N prefix ‘‘FNFS’’, to be deformed after only approximately 29 hours in service. According to Transport Canada, failure of a pin will result in detachment of the main rotor blade and loss of control of the helicopter. Transport Canada also advises that, although the defective pins were only reported on Bell Textron Inc., Model 212 helicopters, pins of the same P/N can also be installed on Bell Textron Inc., Model 204B, 205A–1, and 205B helicopters. While the cause of failure has not been determined, as a precautionary measure and to address the risk of detachment of affected pins in flight, Bell has issued alert service bulletins that specify replacing pins P/N 204–012–104–005 that have S/N prefix ‘‘FNFS’’. 
Accordingly, Transport Canada 
Emergency AD CF–2021–23 requires replacement of affected pins. Transport Canada considers its emergency AD an interim action and states that further AD action may follow. 
After Emergency AD 2021–15–51 was 
issued, the FAA determined that pin P/N 204–012–104–005 with S/N prefix ‘‘FNFS’’ could also be installed on restricted category helicopters originally manufactured by Bell Textron Inc. These helicopters include, but are not limited to, the following: 
•Rotorcraft Development 
Corporation Model HH–1K helicopters; 
•Robinson Air Crane Inc.; Rotorcraft 
Development Corporation; and Tamarack Helicopters, Inc., Model TH–1F helicopters; 
•Bell Textron Inc.; Overseas Aircraft 
Support, Inc. (type certificate previously held by JTBAM, Inc.); and Rotorcraft Development Corporation Model TH–1L helicopters; 
•Richards Heavylift Helo, Inc., 
Model UH–1A helicopters; 
•International Helicopters, Inc.; 
Overseas Aircraft Support, Inc.; Red Tail Flying Services, LLC; Richards Heavylift Helo, Inc.; Rotorcraft Development Corporation; Southwest Florida Aviation International, Inc. (helicopters with an SW204 or SW204HP designation are Southwest Florida Aviation International, Inc., Model UH–1B helicopters); and WSH, LLC (type certificate previously held by San Joaquin Helicopters), Model UH–1B helicopters; 
•Bell Textron Inc.; Overseas Aircraft 
Support, Inc.; Rotorcraft Development Corporation; Smith Helicopters; and West Coast Fabrications Model UH–1E helicopters; 
•AST, Inc.; California Department of 
Forestry; Robinson Air Crane, Inc.; Rotorcraft Development Corporation; and Tamarack Helicopters, Inc., Model UH–1F helicopters; 
•Arrow Falcon Exporters Inc.; Global 
Helicopter Technology, Inc.; Hagglund Helicopters, LLC; JJASPP Engineering Services, LLC; Northwest Rotorcraft, LLC; Overseas Aircraft Support, Inc.; Richards Heavylift Helo, Inc.; Rotorcraft Development Corporation; Southwest Florida Aviation International, Inc. (helicopters with an SW205 designation are Southwest Florida Aviation International, Inc., Model UH–1H helicopters); and Tamarack Helicopters, Inc., Model UH–1H helicopters; 
•Bell Textron Inc.; Overseas Aircraft 
Support, Inc.; and Rotorcraft Development Corporation Model UH–1L helicopters; and 
•Robinson Air Crane, Inc.; and 
Rotorcraft Development Corporation Model UH–1P helicopters. 
Therefore, the FAA issued Emergency 
AD 2021–15–52 to address the unsafe condition on these helicopters. Emergency AD 2021–15–52 requires removing the affected pins from service and prohibits installing those pins on any helicopter. The FAA sent the emergency AD to all known U.S. owners and operators of these helicopters. 
FAA’s Determination 
The FAA is issuing this AD because 
the agency evaluated all the relevant 
information and determined the unsafe condition described previously is likely to exist or develop in other products of these same type designs. 
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Related Service Information 
The FAA reviewed Bell Alert Service 
Bulletin (ASB) UH–1H–21–21 and Bell 
ASB UH–1H–II–21–31. Each ASB is dated July 7, 2021 and specifies removing all P/N 204–012–104–005 pins with an S/N prefix ‘‘FNFS’’ before next flight. These ASBs also specify that, although the investigation is still in progress, removing these pins from service is required. These ASBs state that these pins may not have been manufactured in accordance with the engineering design requirements and may therefore shear as a result of this nonconformance. 
AD Requirements 
This AD requires removing pins P/N 
204–012–104–005 with an S/N prefix 
‘‘FNFS’’ before further flight. This AD also prohibits installing those pins on any helicopter as of the effective date of this AD. 
Interim Action 
The FAA considers this AD to be an 
interim action. If final action is later 
identified, the FAA might consider further rulemaking. 
Justification for Immediate Adoption 
and Determination of the Effective Date 
Section 553(b)(3)(B) of the 
Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for ‘‘good cause,’’ finds that those procedures are ‘‘impracticable, unnecessary, or contrary to the public interest.’’ Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause. 
An unsafe condition exists that 
required the immediate adoption of Emergency AD 2021–15–52, issued on July 8, 2021, to all known U.S. owners and operators of these helicopters. The FAA found that the risk to the flying public justified waiving notice and comment prior to adoption of this rule because the required corrective actions must be completed before further flight. These conditions still exist, therefore, notice and opportunity for prior public comment are impracticable and contrary to the public interest pursuant to 5 U.S.C. 553(b)(3)(B). 
In addition, the FAA finds that good 
cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days, for the same reasons the FAA found good cause to forego 
notice and comment. 
Comments Invited 
The FAA invites you to send any 
written data, views, or arguments about 
this final rule. Send your comments to an address listed under 
ADDRESSES . 
Include ‘‘Docket No. FAA–2021–0605; Project Identifier AD–2021–00805–R’’ at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments 
received by the closing date and may amend this final rule because of those comments. 
Except for Confidential Business 
Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to https://www.regulations.gov, including any 
personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule. 
Confidential Business Information 
CBI is commercial or financial 
information that is both customarily and 
actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this AD contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this AD, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ‘‘PROPIN.’’ The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this AD. Submissions containing CBI should be sent to David Wilson, Aerospace Engineer, DSCO Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222– 5786; email david.wilson@faa.gov. Any 
commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking. 
Regulatory Flexibility Act 
The requirements of the Regulatory 
Flexibility Act (RFA) do not apply when 
an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without prior notice and comment, RFA analysis is not required. 
Costs of Compliance 
The FAA estimates that this AD 
affects 529 helicopters of U.S. Registry. 
Labor rates are estimated at $85 per work-hour. Based on these numbers, the FAA estimates the following costs to comply with this AD. 
Replacing up to four pins takes about 
20 work-hours and parts cost about $1,756 for four pins for an estimated cost of up to $3,456 per helicopter. 
Authority for This Rulemaking 
Title 49 of the United States Code 
specifies the FAA’s authority to issue 
rules on aviation safety. 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. 
The FAA is issuing this rulemaking 
under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: General requirements. Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. 
Regulatory Findings 
This AD will not have federalism 
implications under Executive Order 
13132. This AD will not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. 
For the reasons discussed, I certify 
that this AD: 
(1) Is not a ‘‘significant regulatory 
action’’ under Executive Order 12866, and 
(2) Will not affect intrastate aviation 
in Alaska. 
List of Subjects in 14 CFR Part 39 
Air transportation, Aircraft, Aviation 
safety, Incorporation by reference, 
Safety. 
The Amendment 
Accordingly, under the authority 
delegated to me by the Administrator, 
the FAA amends 14 CFR part 39 as follows: 
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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 [Amended] 
■2. The FAA amends § 39.13 by adding 
the following new airworthiness directive: 
2021–15–52 Various Restricted Category 
Helicopters: Amendment 39–21664; 
Docket No. FAA–2021–0605; Project 
Identifier AD–2021–00805–R. 
(a) Effective Date 
This airworthiness directive (AD) is 
effective without actual notice on August 13, 2021. Emergency AD 2021–15–52, issued on July 8, 2021, which contained the requirements of this amendment, was effective with actual notice. 
(b) Affected ADs 
None. 
(c) Applicability 
This AD applies to various restricted 
category helicopters originally manufactured 
by Bell Textron Inc. (Bell), certificated in any category, with an outboard main rotor hub strap pin (pin) part number 204–012–104– 005 with a serial number prefix ‘‘FNFS’’ installed. These helicopters include but are not limited to: 
(1) Rotorcraft Development Corporation 
Model HH–1K helicopters; 
(2) Robinson Air Crane Inc.; Rotorcraft 
Development Corporation; and Tamarack Helicopters, Inc., Model TH–1F helicopters; 
(3) Bell; Overseas Aircraft Support, Inc. 
(type certificate previously held by JTBAM, Inc.); and Rotorcraft Development Corporation Model TH–1L helicopters; 
(4) Richards Heavylift Helo, Inc., Model 
UH–1A helicopters; 
(5) International Helicopters, Inc.; Overseas 
Aircraft Support, Inc.; Red Tail Flying Services, LLC; Richards Heavylift Helo, Inc.; Rotorcraft Development Corporation; Southwest Florida Aviation International, Inc.,; and WSH, LLC (type certificate previously held by San Joaquin Helicopters), Model UH–1B helicopters; 
Note 1 to paragraph (c)(5): Helicopters 
with an SW204 or SW204HP designation are Southwest Florida Aviation International, Inc., Model UH–1B helicopters. 
(6) Bell; Overseas Aircraft Support, Inc.; 
Rotorcraft Development Corporation; Smith Helicopters; and West Coast Fabrications Model UH–1E helicopters; 
(7) AST, Inc.; California Department of 
Forestry; Robinson Air Crane, Inc.; Rotorcraft Development Corporation; and Tamarack Helicopters, Inc., Model UH–1F helicopters; 
(8) Arrow Falcon Exporters Inc.; Global 
Helicopter Technology, Inc.; Hagglund Helicopters, LLC; JJASPP Engineering Services, LLC; Northwest Rotorcraft, LLC; Overseas Aircraft Support, Inc.; Richards Heavylift Helo, Inc.; Rotorcraft Development Corporation; Southwest Florida Aviation International, Inc.; and Tamarack 
Helicopters, Inc., Model UH–1H helicopters; 
Note 2 to paragraph (c)(8): Helicopters 
with an SW205 designation are Southwest Florida Aviation International, Inc. Model UH–1H helicopters. 
(9) Bell; Overseas Aircraft Support, Inc.; 
and Rotorcraft Development Corporation Model UH–1L helicopters; and 
(10) Robinson Air Crane, Inc.; and 
Rotorcraft Development Corporation Model UH–1P helicopters. 
(d) Subject 
Joint Aircraft System Component (JASC) 
Code: 6200, Main Rotor System. (e) Unsafe Condition 
This AD was prompted by a fatal accident 
in which a pin sheared off during flight, 
which resulted in the main rotor blade and the main rotor head detaching from the helicopter. The FAA is issuing this AD to address this unsafe condition and prevent loss of control of the helicopter. 
(f) Compliance 
Comply with this AD within the 
compliance times specified, unless already 
done. 
(g) Required Actions 
(1) Before further flight, remove from 
service any pin that is identified in the 
introductory text of paragraph (c) of this AD. 
(2) As of the effective date of this AD, do 
not install any pin that is identified in the introductory text of paragraph (c) of this AD on any helicopter. 
(h) Special Flight Permits 
Special flight permits are prohibited. 
(i) Alternative Methods of Compliance 
(AMOCs) 
(1) The Manager, DSCO 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 DSCO Branch, send it to the attention of the person identified in paragraph (j)(1) of this AD. Information may be emailed to: 9-ASW-190-COS@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. 
(j) Related Information 
(1) For more information about this AD, 
contact David Wilson, Aerospace Engineer, 
DSCO Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5786; email david.wilson@faa.gov. 
(2) The subject of this AD is addressed in 
Transport Canada Emergency AD CF–2021– 23, dated July 5, 2021 and FAA Emergency AD 2021–15–51, dated July 6, 2021. You may view those ADs at https://www.regulations.gov in Docket No. FAA– 
2021–0605. Issued on July 21, 2021. 
Gaetano A. Sciortino, 
Deputy Director for Strategic Initiatives, 
Compliance & Airworthiness Division, Aircraft Certification Service. 
[FR Doc. 2021–16222 Filed 7–27–21; 11:15 am] 
BILLING CODE 4910–13–P 
DEPARTMENT OF TRANSPORTATION 
Federal Aviation Administration 
14 CFR Part 71 
[Docket No. FAA–2020–0544; Airspace 
Docket No. 19–AAL–93] 
RIN 2120–AA66 
Removal of Air Traffic Service (ATS) 
Route V–482; Alaska 
AGENCY : Federal Aviation 
Administration (FAA), DOT. 
ACTION : Final rule. 
SUMMARY : This action revokes one 
Alaskan VHF Omnidirectional Range (VOR) Federal airway V–482 in the state of Alaska. The removal is required due to tree encroachment on the Johnstone Point VOR/Distance Measuring Equipment (DME) that renders the airway unusable. 
DATES : Effective date 0901 UTC, October 
7, 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 http://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 : 
Christopher McMullin, Rules and Regulations Group, Office of Policy, Federal Aviation Administration, 800 Independence Avenue SW, Washington, DC 20591; telephone: (202) 267–8783. 
SUPPLEMENTARY INFORMATION : 
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