50610 Federal Register / Vol. 86, No. 173 / Friday, September 10, 2021 / Rules and Regulations 

for loan guarantees, and when required, 

an executed Standard Form LLL, 

‘‘Disclosure of Lobbying Activities,’’ 

(see section 319, Pub. L. 101–121 (31 

U.S.C. 1352)). 

(4) Executed copy of Form AD–1047, 

‘‘Certification Regarding Debarment, 

Suspension, and Other Responsibility 

Matters—Primary Covered 

Transactions.’’ 

(5) Borrower’s determination of loan 

maturity. 

(6) A statement that the borrower is or 

is not delinquent on any Federal debt, 

such as income tax obligations or a loan 

or loan guarantee from another Federal 

agency. If delinquent, the reasons for the 

delinquency must be explained and 

RUS will take such explanation into 

consideration in deciding whether to 

approve the loan. RUS Form 490, 

‘‘Application for Telephone Loan or 

Guarantee,’’ contains a section for 

providing the required statement and 

any appropriate explanation. 

(7) Any other supporting data 

required by the Administrator. 

* * * * * 

(f) For all applications that request 

funding for retail broadband as defined 

in 7 CFR 1735.2, the application must 

include all information required for the 

public notice as stated in 7 CFR 

1735.23(a). 

* * * * * 

Subpart J—Final Loan Approval 

Procedures 

■ 14. Amend § 1737.90 by revising 

paragraph (a)(6) to read as follows: 

§ 1737.90 Loan approval requirements. 

(a) * * * 

(6) All environmental review 

requirements must be met in accordance 

with 7 CFR part 1970. The Agency may 

obligate, but not disperse, funds under 

the program pursuant to 7 U.S.C. 950cc– 

1, before the completion of the 

otherwise required environmental, 

historical, or other types of reviews if 

the Secretary of Agriculture determines 

that subsequent site-specific review 

shall be adequate and easily 

accomplished for the location of towers, 

poles, or other broadband facilities in 

the service area of the awardee without 

compromising the project or the 

required reviews. 

* * * * * 

Christopher A. McLean, 

Acting Administrator, Rural Utilities Service. 

[FR Doc. 2021–19319 Filed 9–9–21; 8:45 am] 

BILLING CODE 3410–15–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0780; Project 

Identifier AD–2021–00916–E; Amendment 

39–21728; AD 2021–19–10] 

RIN 2120–AA64 

Airworthiness Directives; International 

Aero Engines, LLC Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

International Aero Engines, LLC (IAE) 

PW1122G–JM, PW1124G1–JM, 

PW1124G–JM, PW1127G1–JM, 

PW1127GA–JM, PW1127G–JM, 

PW1129G–JM, PW1130G–JM, 

PW1133GA–JM, and PW1133G–JM 

model turbofan engines. This AD was 

prompted by a root cause analysis of an 

event involving an uncontained failure 

of a high-pressure turbine (HPT) disk 

that resulted in high-energy debris 

penetrating the engine cowling on an 

Airbus Model A321–231 airplane, 

powered by IAE V2533–A5 model 

turbofan engines. This AD requires 

removing certain HPT 1st-stage and HPT 

2nd-stage disks from service. The FAA 

is issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective September 

27, 2021. 

The FAA must receive comments on 

this AD by October 25, 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, 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. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0780; 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 street address for 

the Docket Operations is listed above. 

FOR FURTHER INFORMATION CONTACT: 

Mark Taylor, Aviation Safety Engineer, 

ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: 

(781) 238–7229; fax: (781) 238–7199; 

email: Mark.Taylor@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

On March 18, 2020, an Airbus Model 

A321–231 airplane, powered by IAE 

V2533–A5 model turbofan engines, 

experienced an uncontained HPT 1ststage disk failure that resulted in highenergy debris penetrating the engine 

cowling. Based on a preliminary 

analysis of this event, on March 21, 

2020, the FAA issued Emergency AD 

2020–07–51 (followed by publication in 

the Federal Register on April 13, 2020, 

as a Final Rule, Request for Comments 

(85 FR 20402)), which requires the 

removal from service of certain HPT 1ststage disks installed on IAE V2522–A5, 

V2524–A5, V2525–D5, V2527–A5, 

V2527E–A5, V2527M–A5, V2528–D5, 

V2530–A5, and V2533–A5 model 

turbofan engines. 

Pratt & Whitney (PW) determined that 

the failure of the V2533–A5 model 

turbofan engine was due to an 

undetected subsurface material defect in 

an HPT disk that may affect the life of 

the part. In June 2021, PW expanded its 

root cause analysis to include a review 

of records for all other IAE and PW 

engines that contain parts of similar 

material. 

On July 29, 2021, PW provided its 

PW1100G analysis results to the FAA. 

PW’s analysis identified a different 

population of HPT 1st-stage and HPT 

2nd-stage disks installed on IAE 

PW1122G–JM, PW1124G1–JM, 

PW1124G–JM, PW1127G1–JM, 

PW1127GA–JM, PW1127G–JM, 

PW1129G–JM, PW1130G–JM, 

PW1133GA–JM, and PW1133G–JM 

model turbofan engines that are also 

affected by the unsafe condition in AD 

2020–07–51 and require removal from 

service. This condition, if not 

addressed, could result in uncontained 

HPT disk failure, release of high-energy 

debris, damage to the engine, damage to 

the airplane, and loss of the airplane. 

The FAA is issuing this AD to address 

the unsafe condition on these products. 

FAA’s Determination 

The FAA is issuing this AD because 

the agency has determined the unsafe 

condition described previously is likely 

to exist or develop in other products of 

the same type design. 


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Federal Register / Vol. 86, No. 173 / Friday, September 10, 2021 / Rules and Regulations 50611 

AD Requirements 

This AD requires the removal from 

service of certain HPT 1st-stage and 

HPT 2nd-stage disks installed on 

PW1122G–JM, PW1124G1–JM, 

PW1124G–JM, PW1127G1–JM, 

PW1127GA–JM, PW1127G–JM, 

PW1129G–JM, PW1130G–JM, 

PW1133GA–JM, and PW1133G–JM 

model turbofan engines. 

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 

requires the immediate adoption of this 

AD without providing an opportunity 

for public comments prior to adoption. 

The FAA has found that the risk to the 

flying public justifies foregoing notice 

and comment prior to adoption of this 

rule. PW determined that the failure of 

the V2533–A5 model turbofan engine 

was due to an undetected subsurface 

material defect in an HPT disk that may 

affect the life of the part. Based on the 

follow-on analysis performed since that 

event, PW has identified a different 

population of affected HPT 1st-stage and 

HPT 2nd-stage disks installed on IAE 

PW1122G–JM, PW1124G1–JM, 

PW1124G–JM, PW1127G1–JM, 

PW1127GA–JM, PW1127G–JM, 

PW1129G–JM, PW1130G–JM, 

PW1133GA–JM, and PW1133G–JM 

model turbofan engines that are affected 

by the same unsafe condition as 

contained in AD 2020–07–51 and 

require removal from service. These 

HPT disks have the highest risk of 

failure and require removal within 30 

days after the effective date of this AD 

to prevent additional HPT disk failures 

and maintain an acceptable level of 

safety. This unsafe condition may result 

in loss of the airplane. The FAA 

considers removal of certain HPT 1ststage and HPT 2nd-stage disks to be an 

urgent safety issue. Accordingly, 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–2021–0780 

and Project Identifier AD–2021–00916– 

E’’ 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 Mark Taylor, Aviation 

Safety Engineer, ECO Branch, FAA, 

1200 District Avenue, Burlington, MA 

01803. 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 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 3 engines installed on airplanes 

of U.S. registry. 

The FAA estimates the following 

costs to comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Remove HPT 1st-stage or HPT 2nd-stage 

disk.

94 work-hours × $85 per hour = $7,990 ........ $171,430 $179,420 $538,260 

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 


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50612 Federal Register / Vol. 86, No. 173 / Friday, September 10, 2021 / Rules and Regulations 

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 above, 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: 

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: 

2021–19–10 International Aero Engines, 

LLC: Amendment 39–21728; Docket No. 

FAA–2021–0780; Project Identifier AD– 

2021–00916–E. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective September 27, 2021. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to International Aero 

Engines, LLC (IAE) PW1122G–JM, 

PW1124G1–JM, PW1124G–JM, PW1127G1– 

JM, PW1127GA–JM, PW1127G–JM, 

PW1129G–JM, PW1130G–JM, PW1133GA– 

JM, and PW1133G–JM model turbofan 

engines with an installed: 

(1) High-pressure turbine (HPT) 1st-stage 

disk, part number (P/N) 30G6201 or 

30G7301, with a serial number (S/N) listed in 

Figure 1 to paragraph (c) of this AD; or 

(2) HPT 2nd-stage disk, P/N 30G5502 or 

30G6602, with an S/N listed in Figure 2 to 

paragraph (c) of this AD. 

BILLING CODE 4910–13–P 


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Figure 1 to Paragraph (c)-HPT 1st-Stage Disk, PIN 30G6201 or 30G7301 

HPT 1st-Stage Disk PIN HPT 1st-Stage Disk SIN 

30G6201 LKLBCG9614 

30G6201 LKLBDX9135 

30G6201 LKLBEF4499 

30G6201 LKLBCL8431 

30G6201 LKLBDX9233 

30G6201 LKLBDX9159 

30G6201 LKLBDX9273 

30G6201 LKLBBX3713 

30G6201 LKLBDX9200 

30G6201 LKLBDX9276 

30G6201 LKLBDA1782 

30G6201 LKLBEF4550 

30G7301 LKLBEK6166 

30G7301 LKLBEY0974 

30G7301 LKLBEJ7493 

30G7301 LKLBEY4908 

30G7301 LKLBEP5334 

30G7301 LKLBEX5852 

30G7301 LKLBFA2128 

30G7301 LKLBEY4944 

30G7301 LKLBGF8458 
Federal Register / Vol. 86, No. 173 / Friday, September 10, 2021 / Rules and Regulations 50613 

BILLING CODE 4910–13–C 


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Figure 2 to Paragraph (c)- HPT 2nd-Stage Disk, PIN 30G5502 or 30G6602 

HPT 2nd-Stage Disk PIN HPT 2nd-Stage Disk SIN 

30G5502 LKLBCC0lll 

30G5502 LKLBD40504 

30G5502 LKLBD40476 

30G5502 LKLBC29705 

30G5502 LKLBC29734 

30G5502 LKLBCP4546 

30G5502 LKLBCP4502 

30G5502 LKLBC02866 

30G5502 LKLBCP4501 

30G5502 LKLBBX2558 

30G5502 LKLBC02909 

30G5502 LKLBC02820 

30G5502 LKLBC02871 

30G5502 LKLBC02859 

30G5502 LKLBC02877 

30G5502 LKLBBX2564 

30G5502 LKLBCP4555 

30G5502 LKLBBX2576 

30G5502 LKLBC29762 

30G5502 LKLBC02860 

30G5502 LKLBC02881 

30G5502 LKLBC02864 

30G5502 LKLBC02876 

30G5502 LKLBC02880 

30G5502 LKLBD40491 

30G5502 LKLBC02873 

30G5502 LKLBBX2560 

30G5502 LKLBCP4504 

30G5502 LKLBC02840 

30G5502 LKLBD40433 

30G5502 LKLBD40437 

30G6602 LKLBEX5800 

30G6602 LKLBEK1972 

30G6602 LKLBEP4213 

30G6602 LKLBFD4429 

30G6602 LKLBFD4445 

30G6602 LKLBGJ4215 

30G6602 LKLBFD4402 
50614 Federal Register / Vol. 86, No. 173 / Friday, September 10, 2021 / Rules and Regulations 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 7250, Turbine Section. 

(e) Unsafe Condition 

This AD was prompted by an analysis 

performed by Pratt & Whitney of an event 

involving an uncontained failure of an HPT 

1st-stage disk that resulted in high-energy 

debris penetrating the engine cowling. The 

FAA is issuing this AD to prevent failure of 

the HPT 1st-stage and HPT 2nd-stage disks. 

The unsafe condition, if not addressed, could 

result in uncontained HPT disk failure, 

release of high-energy debris, damage to the 

engine, damage to the airplane, and loss of 

the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

(1) For IAE model turbofan engines with an 

HPT 1st-stage disk, P/N 30G6201 or 30G7301, 

with an S/N listed in Figure 1 to paragraph 

(c) of this AD, within 30 days after the 

effective days of the AD, remove the HPT 1ststage disk from service. 

(2) For IAE model turbofan engines with an 

HPT 2nd-stage disk, P/N 30G5502 or 

30G6602, with an S/N listed in Figure 2 to 

paragraph (c) of this AD, within 30 days after 

the effective days of the AD, remove the HPT 

2nd-stage disk from service. 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, ECO 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 (i) of this AD. 

Information may be emailed to: ANE-ADAMOC@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. 

(i) Related Information 

For more information about this AD, 

contact Mark Taylor, Aviation Safety 

Engineer, ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: (781) 

238–7229; fax: (781) 238–7199; email: 

Mark.Taylor@faa.gov. 

(j) Material Incorporated by Reference 

None. 

Issued on September 7, 2021. 

Lance T. Gant, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2021–19600 Filed 9–8–21; 11:15 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2021–0529; Airspace 

Docket No. 21–ASO–18] 

RIN 2120–AA66 

Amendment of Class E Airspace; 

Monroe, NC 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action amends Class E 

airspace extending upward from 700 

feet above the surface for CharlotteMonroe Executive Airport, Monroe, NC. 

The FAA is taking this action as a result 

of the Charlotte Class B Biennial 

Review. This action also updates the 

airport’s name to Charlotte-Monroe 

Executive Airport (formerly Monroe 

Airport). In addition, this action updates 

the geographic coordinates of the airport 

to coincide with the FAA’s database. 

Controlled airspace is necessary for the 

safety and management of instrument 

flight rules (IFR) operations in the area. 

DATES: Effective 0901 UTC, December 2, 

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 Airspace Policy 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 

fr.inspection@nara.gov or go to https:// 

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

ibr-locations.html. 

FOR FURTHER INFORMATION CONTACT: John 

Fornito, Operations Support Group, 

Eastern Service Center, Federal Aviation 

Administration, 1701 Columbia Ave., 

College Park, GA 30337; Telephone 

(404) 305–6364. 

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 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 amends the 

Class E airspace extending upward from 

700 feet above the surface in Monroe, 

NC, to support IFR operations in the 

area. 

History 

The FAA published a notice of 

proposed rulemaking in the Federal 

Register (86 FR 35419, July 6, 2021) for 

Docket No. FAA–2021–0529 to amend 

Class E airspace extending upward from 

700 feet above the surface at CharlotteMonroe Executive Airport, Monroe, NC. 

Interested parties were invited to 

participate in this rulemaking effort by 

submitting written comments on the 

proposal to the FAA. One comment 

supporting this action was received. 

Class E airspace designations are 

published in Paragraph 6005 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 Class E airspace designations 

listed in this document will be 

published subsequently in the Order. 

Availability and Summary of 

Documents for Incorporation by 

Reference 

This document amends FAA Order 

7400.11E, Airspace Designations and 

Reporting Points, dated July 21, 2020, 

and effective September 15, 2020. FAA 

Order 7400.11E is publicly available as 

listed in the ADDRESSES section of this 

document. FAA Order 7400.11E lists 

Class A, B, C, D, and E airspace areas, 

air traffic routes, and reporting points. 

The Rule 

The FAA is amending 14 CFR part 71 

by amending the Class E airspace 

extending upward from 700 feet above 

the surface at Charlotte-Monroe 

Executive Airport, Monroe, NC, by 

increasing the radius to 9.0 miles, 

(formerly 6.3 miles). In addition, this 

action updates the airport’s name to 

Charlotte-Monroe Executive Airport 

(formerly Monroe Airport) and updates 

the geographical coordinates to coincide 

with the FAA’s database. 

FAA Order 7400.11, Airspace 

Designations and Reporting Points, is 


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