27494 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 

TABLE A—SUPPLEMENTAL BALANCE SHEET INFORMATION

Banks 1 Associations 2

Financial 

assistance 

corporation 

Eliminations 

Combined 

without 

insurance 

fund 3

Insurance fund 

and related 

combination 

entries 

Combined 

with insurance 

fund 

Cash and investments.

Net loans.

Restricted assets.

Other Assets.

Total assets.

Total liabilities.

Protected borrower capital 4.

Restricted capital.

Capital stock and surplus.

Total liabilities, protected borrower capital, 

and capital stock and surplus.

1Provided combined financial data of all FCS banks, including any consolidated subsidiaries of the banks. 

2Provide association-only combined financial data of all FCS associations. 

3Provide the combined financial data of all columns on the left. 

4Any item that is no longer applicable, e.g., protected borrower stock, may be omitted. 

TABLE B—SUPPLEMENTAL INCOME STATEMENT INFORMATION

Banks 1 Associations 2

Financial 

assistance 

corporation 

Eliminations 

Combined 

without 

insurance 

fund 3

Insurance fund 

and related 

combination 

entries 

Combined with 

insurance fund 

Net interest income.

Provision for credit losses.

Other income.

Other expenses.

Net Income.

1Provide combined financial data of all FCS banks, including any consolidated subsidiaries of the banks. 

2Provide association-only combined financial data of all FCS associations. 

3Provide the combined financial data of all columns on the left. 

Dated: April 20, 2022. 

Ashley Waldron, 

Secretary, Farm Credit Administration Board. 

[FR Doc. 2022–08832 Filed 5–6–22; 8:45 am] 

BILLING CODE 6705–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2022–0511; Project 

Identifier AD–2022–00397–T; Amendment 

39–22043; AD 2022–10–05] 

RIN 2120–AA64 

Airworthiness Directives; Gulfstream 

Aerospace Corporation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is superseding 

Airworthiness Directive (AD) 2020–05– 

12, which applied to all Gulfstream 

Aerospace Corporation Model GVII– 

G500 and GVII–G600 airplanes. AD 

2020–05–12 required revising the 

existing airplane flight manual (AFM) to 

incorporate revised limitations and 

procedures. This AD was prompted by 

reports of two landing incidents in 

which the alpha limiter engaged in the 

landing flare in unstable air, resulting in 

high rate of descent landings and 

damage to the airplanes. This AD retains 

certain requirements, and also adds and 

replaces certain AFM sections with 

more restrictive limitations and 

procedures. The FAA is issuing this AD 

to address the unsafe condition on these 

products. 

DATES: This AD is effective May 9, 2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of March 13, 2020 (85 FR 14562, 

March 13, 2020). 

The FAA must receive comments on 

this AD by June 23, 2022. 

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. 

For service information identified in 

this final rule, contact Gulfstream 

Aerospace Corporation, Technical 

Publications Dept., P.O. Box 2206, 

Savannah, GA 31402–2206; telephone 

800–810–4853; fax 912–965–3520; email 

pubs@gulfstream.com; internet http://

www.gulfstream.com/customer-support. 

You may view this 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 206–231– 

3195. It is also available at https://

www.regulations.gov by searching for 

and locating Docket No. FAA–2022– 

0511. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2022–0511; 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 


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Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 27495 

final rule, any comments received, and 

other information. The street address for 

the Docket Operations is listed above. 

FOR FURTHER INFORMATION CONTACT: 

Sanford Proveaux, Aerospace Engineer, 

Certificate Management and Safety 

Oversight Section, FAA, Atlanta ACO 

Branch, 1701 Columbia Avenue, College 

Park, GA 30337; phone: 404–474–5566; 

email: Sanford.Proveaux@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The FAA issued AD 2020–05–12, 

Amendment 39–19860 (85 FR 14562, 

March 13, 2020) (AD 2020–05–12), for 

all Gulfstream Aerospace Corporation 

Model GVII–G500 and GVII–G600 

airplanes. AD 2020–05–12 required 

revising the existing AFM to limit the 

maximum crosswind component for 

landing and increase the normal 

approach speeds, based on steady-state 

winds and wind gusts. AD 2020–05–12 

was prompted by a report of a landing 

incident, which occurred on February 6, 

2020, where the alpha (angle of attack) 

limiter engaged during the landing flare 

in unstable air, resulting in a high rate 

of descent landing and damage to the 

airplane. The FAA issued AD 2020–05– 

12 to address inappropriate alpha 

limiter engagement during the landing 

flare, which can limit pilot pitch 

authority during a critical phase of flight 

near the ground, and result in a high 

rate of descent landing with possible 

consequent loss of control of the 

airplane on landing. 

Actions Since AD 2020–05–12 Was 

Issued 

After the FAA issued AD 2020–05–12, 

a second landing event occurred on 

April 4, 2022. As in the first event, the 

alpha limiter engaged during the 

landing flare in unstable air, resulting in 

a high rate of descent landing and 

damage to the airplane. In both events, 

the angle of attack (AOA) protection 

function (alpha limiter) of the flight 

control computer (FCC) engaged and 

overrode the pilot pitch control inputs 

which the flight control law erroneously 

predicted would exceed the stall AOA. 

This resulted in a high rate of descent 

landing on the runway. Additionally, 

the pilots in both events had full aftstick input when the aircraft contacted 

the runway, and the full-up pitch 

control did not arrest the high rate of 

descent landing. 

The Model GVII–G500 and GVII–G600 

alpha limiter function of the FCC is 

designed to prevent aerodynamic stalls 

and operates when airborne and 

operating in normal control law. The 

FCC uses many inputs including current 

AOA, rate of change of AOA, and pilot 

control stick inputs to determine alpha 

limiter activation. If the FCC predicts 

that critical AOA values will be 

exceeded, the FCC will activate the 

alpha limiting function. The FCC may 

activate the alpha limiting function 

when the AOA is not close to stall. 

Depending on the rate of AOA increase 

and pilot stick input, the alpha limiter 

may command nose down elevator to 

prevent a stall. It is clear from an 

analysis of both events that unintended 

alpha limiter engagement is primarily 

caused by rapid, large, and oscillating 

pilot control inputs near approach 

reference speeds, induced by unstable 

atmospheric conditions and gusty 

winds. 

The aircraft level hazard is that 

inappropriate alpha limiter engagement 

during the landing flare, which can 

limit the pilot’s ability to control pitch 

during a critical phase of flight near the 

ground, can result in a high rate of 

descent landing with possible 

consequent loss of control of the 

airplane on landing. It has been 

determined that the operating 

limitations mandated by AD 2020–05– 

12 are not adequate to prevent another 

occurrence. For these reasons, the AFM 

wind and gust operating limitations 

have been further restricted in this AD. 

Pilot Adherence to AFM Revisions To 

Mitigate the Unsafe Condition of 

Unintended Alpha Limiter Engagement 

These more restrictive operating 

limitations do not relieve a pilot from 

their other regulatory obligations, 

including verifying destination wind 

forecasts prior to departure, monitoring 

winds en route, verifying that the 

approach briefing includes a cockpit 

brief of winds and weather, and 

confirming that the winds are still 

within acceptable limits just prior to 

landing. Pilots are responsible for 

becoming familiar with this information 

when performing preflight actions 

under 14 CFR part 91.103, 91.151, and 

91.167. Furthermore, these limitations 

can only be exceeded when the pilot is 

exercising their authority under 14 CFR 

part 91.3. 

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. 

Related Service Information Under 1 

CFR Part 51 

This AD retains certain requirements 

of AD 2020–05–12, which requires the 

following sections of Gulfstream GVII– 

G500 Airplane Flight Manual, GAC– 

AC–GVII–G500–OPS–0001, Revision 5, 

dated March 3, 2020, which the Director 

of the Federal Register approved for 

incorporation by reference as of March 

13, 2020 (85 FR 14562, March 13, 2020). 

• Section 01–27–10, ‘‘Normal Control 

Laws,’’ of Chapter 01, ‘‘LIMITATIONS.’’ 

• Step 8., ‘‘Final Approach Fix,’’ of 

Section 04–08–40, ‘‘One Engine 

Inoperative Landing Procedure,’’ of 

Chapter 04, ‘‘EMERGENCY 

PROCEDURES.’’ 

• Step 11., ‘‘Landing,’’ of Section 03– 

12–10, ‘‘Zero Flaps or Partial Flaps 

Landings,’’ of Chapter 03, ‘‘ABNORMAL 

PROCEDURES.’’ 

• Step 15., ‘‘Approach Speed,’’ of 

Section 01–03–40, ‘‘Airspeed 

Limitations,’’ of Chapter 01, 

‘‘LIMITATIONS.’’ 

This AD also requires the following 

sections of Gulfstream GVII–G600 

Airplane Flight Manual, GAC–AC– 

GVII–G600–OPS–0001, Revision 3, 

dated March 3, 2020, which the Director 

of the Federal Register approved for 

incorporation by reference as of March 

13, 2020 (85 FR 14562, March 13, 2020). 

• Section 01–27–10, ‘‘Normal Control 

Laws,’’ of Chapter 01, ‘‘LIMITATIONS.’’ 

• Steps 3. and 4. of Section 01–34–40, 

‘‘Takeoff and Landing Data (TOLD),’’ of 

Chapter 01, ‘‘LIMITATIONS.’’ 

• Step 8., ‘‘Final Approach Fix,’’ of 

Section 04–08–40, ‘‘One Engine 

Inoperative Landing Procedure,’’ of 

Chapter 04, ‘‘EMERGENCY 

PROCEDURES.’’ 

• Step 11., ‘‘Landing,’’ of Section 03– 

12–10, ‘‘Zero Flaps or Partial Flaps 

Landings,’’ of Chapter 03, ‘‘ABNORMAL 

PROCEDURES.’’ 

This service information 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. 

AD Requirements 

This AD retains some of the AFM 

revisions required by AD 2020–05–12, 

as listed under the Related Service 

Information under 1 CFR part 51 section 

of this final rule. 

For Model GVII–G500 airplanes, this 

AD also requires revising the following 

sections of the existing AFM to include 

more restrictive limitations and 

procedures. 

• ‘‘Wind Conditions’’ of Section 01– 

02–10: ‘‘Runway, Slope, and Wind 

Conditions,’’ of Chapter 01, 

‘‘LIMITATIONS.’’ 

• ‘‘Day and Night, Visual and 

Instrument Flight Rules’’ of Section 01– 

03–10: ‘‘Types of Airplane Operations 

Permitted,’’ of Chapter 01, 

‘‘LIMITATIONS.’’ 


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• ‘‘Approach Speed’’ of Section 01– 

03–40: ‘‘Airspeed Limitations,’’ of 

Chapter 01, ‘‘LIMITATIONS.’’ 

• Section 01–22–10: ‘‘Autothrottle,’’ 

of Chapter 01, ‘‘LIMITATIONS.’’ 

• ‘‘WARNING’’ information 

preceding ‘‘Approach/Landing 

Airspeeds’’ of Section 02–05–50: 

‘‘Landing,’’ of Chapter 02, ‘‘NORMAL 

OPERATIONS.’’ 

• ‘‘Introduction’’ and ‘‘Example’’ 

sections of Section 05–11–10: 

‘‘Threshold Speeds’’ of Chapter 05, 

‘‘PERFORMANCE.’’ 

For Model GVII–G600 airplanes, this 

AD also requires adding or replacing the 

following sections of the existing AFM 

to include more restrictive limitations 

and procedures. 

• ‘‘Wind Conditions’’ of Section 01– 

02–10: ‘‘Runway, Slope, and Wind 

Conditions,’’ of Chapter 01, 

‘‘LIMITATIONS.’’ 

• ‘‘Day and Night, Visual and 

Instrument Flight Rules’’ of Section 01– 

03–10: ‘‘Types of Airplane Operations 

Permitted,’’ of Chapter 01, 

‘‘LIMITATIONS.’’ 

• ‘‘Approach Speed’’ of Section 01– 

03–40: ‘‘Airspeed Limitations,’’ of 

Chapter 01, ‘‘LIMITATIONS.’’ 

• Section 01–22–10: ‘‘Autothrottle,’’ 

of Chapter 01, ‘‘LIMITATIONS.’’ 

• ‘‘WARNING’’ information 

preceding ‘‘Approach/Landing 

Airspeeds’’ of Section 02–05–50: 

‘‘Landing,’’ of Chapter 02, ‘‘NORMAL 

OPERATIONS.’’ 

• ‘‘Introduction’’ and ‘‘Example’’ 

sections of Section 05–11–10: 

‘‘Threshold Speeds’’ of Chapter 05, 

‘‘PERFORMANCE.’’ 

Interim Action 

The FAA considers this AD to be an 

interim action. The manufacturer is 

developing a modification that will 

address the unsafe condition identified 

in this AD. Once this modification is 

developed, approved, and available, the 

FAA might consider additional 

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 

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 forgoing notice 

and comment prior to adoption of this 

rule because inappropriate alpha limiter 

engagement during the landing flare can 

limit pilot pitch authority during a 

critical phase of flight near the ground 

and could result in a high rate of 

descent landing with possible 

consequent loss of control of the 

airplane. Given the significance of the 

risk presented by this unsafe condition, 

it must be immediately addressed. 

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 forgo 

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–2022–0511 

and Project Identifier AD–2022–00397– 

T’’ 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 Sanford Proveaux, 

Aerospace Engineer, Certificate 

Management and Safety Oversight 

Section, FAA, Atlanta ACO Branch, 

1701 Columbia Avenue, College Park, 

GA 30337; phone: 404–474–5566; email: 

Sanford.Proveaux@faa.gov. Any 

commentary that the FAA receives that 

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 notice 

and comment, RFA analysis is not 

required. 

Costs of Compliance 

The FAA estimates that this AD 

affects 120 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 

AFM revision .......................... 1 work-hour × $85 per hour = $85 ......................................... $0 $85 $10,200 


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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 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: 

■ a. Removing Airworthiness Directive 

(AD) 2020–05–12, Amendment 39– 

19860 (85 FR 14562, March 13, 2022); 

and 

■ b. Adding the following new AD: 

2022–10–05 Gulfstream Aerospace 

Corporation: Amendment 39–22043; 

Docket No. FAA–2022–0511; Project 

Identifier AD–2022–00397–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective May 9, 2022. 

(b) Affected ADs 

This AD replaces AD 2020–05–12, 

Amendment 39–19860 (85 FR 14562, March 

13, 2020) (AD 2020–05–12). 

(c) Applicability 

This AD applies to all Gulfstream 

Aerospace Corporation Model GVII–G500 

and GVII–G600 airplanes, certificated in any 

category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 27, Flight controls. 

(e) Unsafe Condition 

This AD was prompted by reports of two 

landing incidents in which the alpha limiter 

engaged in the landing flare in unstable air, 

resulting in high rate of descent landings and 

damage to the airplanes. The FAA is issuing 

this AD to address inappropriate alpha 

limiter engagement during the landing flare, 

which can limit pilot pitch authority during 

a critical phase of flight near the ground, and 

result in a high rate of descent landing with 

possible consequent loss of control of the 

airplane on landing. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Requirements for Certain AFM 

Revisions for GVII–G500, With Revised 

Paragraph References 

This introductory text to paragraph (g) 

restates the requirements of the introductory 

text to paragraph (g) of AD 2020–05–12, with 

revised paragraph references. For Model 

GVII–G500 airplanes: Within 5 days after 

March 13, 2020 (the effective date of AD 

2020–05–12), revise the existing airplane 

flight manual (AFM) for your airplane to 

incorporate the information specified in 

paragraphs (g)(1) through (4) of this AD. 

(1) This paragraph (g)(1) restates the 

information in paragraph (g)(3) of AD 2020– 

05–12, with no changes. Section 01–27–10, 

‘‘Normal Control Laws,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ of the Gulfstream GVII– 

G500 Airplane Flight Manual, GAC–AC– 

GVII–G500–OPS–0001, Revision 5, dated 

March 3, 2020. 

(2) This paragraph (g)(2) restates the 

information in paragraph (g)(4) of AD 2020– 

05–12, with no changes. Step 5. of Section 

01–34–40, ‘‘Takeoff and Landing Data 

(TOLD),’’ of Chapter 01, ‘‘LIMITATIONS,’’ of 

the Gulfstream GVII–G500 Airplane Flight 

Manual, GAC–AC–GVII–G500–OPS–0001, 

Revision 5, dated March 3, 2020. 

(3) This paragraph (g)(3) restates the 

information in paragraph (g)(6) of AD 2020– 

05–12, with no changes. Step 11. ‘‘Landing,’’ 

of Section 03–12–10, ‘‘Zero Flaps or Partial 

Flaps Landings,’’ of Chapter 03, 

‘‘ABNORMAL PROCEDURES,’’ of the 

Gulfstream GVII–G500 Airplane Flight 

Manual, GAC–AC–GVII–G500–OPS–0001, 

Revision 5, dated March 3, 2020. 

(4) This paragraph (g)(4) restates the 

information in paragraph (g)(7) of AD 2020– 

05–12, with no changes. Step 8. ‘‘Final 

Approach Fix,’’ of Section 04–08–40, ‘‘One 

Engine Inoperative Landing Procedure,’’ of 

Chapter 04, ‘‘EMERGENCY PROCEDURES,’’ 

of the Gulfstream GVII–G500 Airplane Flight 

Manual, GAC–AC–GVII–G500–OPS–0001, 

Revision 5, dated March 3, 2020. 

(h) Retained Requirements for Certain AFM 

Revisions for GVII–G600, With Revised 

Paragraph References 

This introductory text to paragraph (h) 

restates the requirements of the introductory 

text to paragraph (h) of AD 2020–05–12, with 

revised paragraph references. For Model 

GVII–G600 airplanes: Within 5 days after 

March 13, 2020 (the effective date of AD 

2020–05–12), revise the existing AFM for 

your airplane to incorporate the information 

specified in paragraphs (h)(1) through (4) of 

this AD. 

(1) This paragraph (h)(1) restates the 

information in paragraph (h)(3) of AD 2020– 

05–12, with no changes. Section 01–27–10, 

‘‘Normal Control Laws,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ of the Gulfstream GVII– 

G600 Airplane Flight Manual, GAC–AC– 

GVII–G600–OPS–0001, Revision 3, dated 

March 3, 2020. 

(2) This paragraph (h)(2) restates the 

information in paragraph (h)(4) of AD 2020– 

05–12, with no changes. Steps 3. and 4. of 

Section 01–34–40, ‘‘Takeoff and Landing 

Data (TOLD),’’ of Chapter 01, 

‘‘LIMITATIONS,’’ of the Gulfstream GVII– 

G600 Airplane Flight Manual, GAC–AC– 

GVII–G600–OPS–0001, Revision 3, dated 

March 3, 2020. 

(3) This paragraph (h)(3) restates the 

information in paragraph (h)(6) of AD 2020– 

05–12, with no changes. Step 11., ‘‘Landing,’’ 

of Section 03–12–10, ‘‘Zero Flaps or Partial 

Flaps Landings,’’ of Chapter 03, 

‘‘ABNORMAL PROCEDURES,’’ of the 

Gulfstream GVII–G600 Airplane Flight 

Manual, GAC–AC–GVII–G600–OPS–0001, 

Revision 3, dated March 3, 2020. 

(4) This paragraph (h)(4) restates the 

information in paragraph (h)(7) of AD 2020– 

05–12, with no changes. Step 8., ‘‘Final 

Approach Fix,’’ of Section 04–08–40, ‘‘One 

Engine Inoperative Landing Procedure,’’ of 

Chapter 04, ‘‘EMERGENCY PROCEDURES,’’ 

of the Gulfstream GVII–G600 Airplane Flight 

Manual, GAC–AC–GVII–G600–OPS–0001, 

Revision 3, dated March 3, 2020. 

(i) New Requirements: AFM Revision for 

GVII–G500 

For Model GVII–G500 airplanes: Within 3 

days after the effective date of this AD, revise 

the existing AFM for your airplane as 

specified in paragraphs (i)(1) through (6) of 

this AD. 

(1) Replace the information in ‘‘Wind 

Conditions’’ of Section 01–02–10: ‘‘Runway, 

Slope, and Wind Conditions,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 1 to paragraph (i)(1) of this AD. 

BILLING CODE 4910–13–P 


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(2) Replace the information in ‘‘Day and 

Night, Visual and Instrument Flight Rules’’ of 

Section 01–03–10: ‘‘Types of Airplane 

Operations Permitted,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 2 to paragraph (i)(2) of this AD. 

(3) Replace the information in ‘‘Approach 

Speed’’ of Section 01–03–40: ‘‘Airspeed 

Limitations,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 3 to paragraph (i)(3) of this AD. 


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Figure 1 to paragraph (i)(l)-Section 01-02-10: Runway, Slope, and Wind 

Conditions 

01-02-10: Runway, Slope, and Wind Conditions 

3. Wind Conditions 

a. The maximum wind speed for landing (including gusts) is 15 knots. 

b. The maximum wind gust for landing is 5 knots. 

c. Maximum tailwind component approved for takeoff and landing: 10 knots 

d. When operating in a flight control law mode other than normal (i.e., alternate, 

direct, or backup), maximum crosswind component for landing: 10 knots 

e. Maximum tailwind component for landing with flaps 10° or less is zero knots. 

Figure 2 to paragraph (i)(2)-Section 01-03-10: Types of Airplane 

Operations Permitted 

01-03-10: Types of Airplane Operations Permitted 

2. Day and Night, Visual and Instrument Flight Rules 

a. All approaches must be stabilized by 1000 ft AGL, including visual maneuvers. 

b. Vertical guidance from an ILS or FMS-based approach is required for night 

landings. 
Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 27499 

(4) To Section 01–22–10: ‘‘Autothrottle,’’ of 

Chapter 01, ‘‘LIMITATIONS,’’ add the 

information in figure 4 to paragraph (i)(4) of 

this AD. 


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Figure 3 to paragraph (i)(3)-Sectian 01-03-40: Airspeed Limitations 

01-03-40: Airspeed Limitations 

15. Approach Speed 

a. Approach speed additives (Flaps 39) are half the steady state wind plus the 

gust increment up to a maximum additive of 20 knots. 

b. Minimum approach speed during normal operations is VREF + 10 knots, unless 

otherwise specified in a non-normal procedure. 

c. Approach Speed shall be maintained to the runway threshold and shall be 

used to determine landing performance except for abnormal flap approaches. 

Abnormal flap approaches must comply with the procedures in section 

03-12-10: Zero Flaps or Partial Flaps Landings. 

Figure 4 to paragraph (i)(4)-Section 01-22-10: Autothrottle 

01-22-10: Autothrottle 

2. Use of the Autothrottle for approach and landing is required during normal 

operations. I Note 

Pilot will physically guard the throttles until touchdown, and override or 

disconnect the autothrottle if performance is not as expected. 
27500 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 

(5) Replace the ‘‘WARNING’’ information 

preceding ‘‘Approach/Landing Airspeeds’’ of 

Section 02–05–50: ‘‘Landing,’’ of Chapter 02, 

‘‘NORMAL OPERATIONS,’’ with the 

information in figure 5 to paragraph (i)(5) of 

this AD. 

(6) Replace the ‘‘Introduction’’ and 

‘‘Examples’’ sections of Section 05–11–10: 

‘‘Threshold Speeds’’ of Chapter 05, 

‘‘PERFORMANCE,’’ with the information in 

figure 6 to paragraph (i)(6) of this AD. 


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Figure 5 to paragraph (i)(S) - Section 02-05-50: Landing 

02-05-50: Landing 

I WARNING 

EXCEPT AS REQUIRED IN AN EMERGENCY OR AS DIRECTED BY A 

NON-NORMAL PROCEDURE, MINIMUM APPROACH SPEED IS VREF 

+10. APPROACH SPEED SHALL BE MAINTAINED TO THE 

THRESHOLD AND SHALL BE USED TO DETERMINE LANDING 

DISTANCE. 

4. Approach/Landing Airspeeds .......................................................... Verify 
Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 27501 


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Figure 6 to paragraph (i)(6)-Section 05-11-10: Threshold Speeds 

05-11-10: Threshold Speeds 

Introduction 

1. Threshold speeds, VREF, for landing distance are shown for normal flap setting 39° 

in Figure 1. Threshold Speed for Landing Distance, Flaps 39°, Wing Anti-Ice OFF 

And ON for Wing Anti-Ice OFF and ON operations. Abnormal flap settings 20° and 

10° threshold speeds for Wing Anti-Ice OFF and ON conditions are shown in 

Figure 2. Threshold Speed for Landing Distance, Flaps 20°, Wing Anti-Ice OFF 

And ON and Figure 3. Threshold Speed for Landing Distance, Flaps 10°, Wing 

Anti-Ice OFF And ON. For the abnormal flap setting 0°, threshold speeds shown in 

Figure 4. Threshold Speed for Landing Distance, Flaps 0°, Wing Anti-Ice ON are 

effective for Wing Anti-Ice ON operations. 

2. Normally, landings will be conducted only at the landing flap setting of 39°. 

Additional charts are provided for reduced flap settings to be used when an 

abnormal landing at a reduced flap setting is required. The landing threshold 

speeds shown are effective throughout the certified weight, temperature and 

altitude range of the airplane. 

I WARNING 

EXCEPT AS REQUIRED IN AN EMERGENCY OR AS DIRECTED BY A 

NON-NORMAL PROCEDURE, MINIMUM APPROACH SPEED IS VREF 

+10. APPROACH SPEED SHALL BE MAINTAINED TO THE 

THRESHOLD AND SHALL BE USED TO DETERMINE LANDING 

DISTANCE. 

I CAUTION I 

TIRESPEED LIMITATIONS WILL BE EXCEEDED IF TOUCHDOWN IS 

MADE IN EXCESS OF 195 KNOTS GROUNDSPEED. 

Note 

Landing distance in 05-11-30: Landing Distance and maximum landing 

weight 05-11-20: Tire Speed and BKE Limited Maximum Landing Weight 

shall be calculated utilizing planned speed at the threshold. 

Examples 

1. Determine the final approach and threshold speeds for landing at a normal flap 

(39°) setting. 

a. Given: 

• Landing Gross Weight= 58,000 pounds (26,308 kg) 

• Airport Pressure Altitude = 2000 feet 

b. Solution: 

• Threshold Speed (VREF) = 125 KIAS 

• Final Approach Speed (VREF +10 KIAS = 135 KIAS 
27502 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 

(j) New Requirements: AFM Revision for 

GVII–G600 

For Model GVII–G600 airplanes: Within 3 

days after the effective date of this AD, revise 

the existing AFM for your airplane as 

specified in paragraphs (j)(1) through (6) of 

this AD. 

(1) Replace the information in ‘‘Wind 

Conditions’’ of Section 01–02–10: ‘‘Runway, 

Slope, and Wind Conditions,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 7 to paragraph (j)(1) of this AD. 

(2) Replace the information in ‘‘Day and 

Night, Visual and Instrument Flight Rules’’ of 

Section 01–03–10: ‘‘Types of Airplane 

Operations Permitted,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 8 to paragraph (j)(2) of this AD. 

(3) Replace the information in ‘‘Approach 

Speed’’ of Section 01–03–40: ‘‘Airspeed 

Limitations,’’ of Chapter 01, 

‘‘LIMITATIONS,’’ with the information in 

figure 9 to paragraph (j)(3) of this AD. 


khammond on DSKJM1Z7X2PROD with RULESER09MY22.045</GPH> ER09MY22.046</GPH>

Figure 7 to paragraph G)(l)-Section 01-02-10: Runway, Slope, and Wind 

Conditions 

01-02-10: Runway, Slope, and Wind Conditions 

3. Wind Conditions 

a. The maximum wind speed for landing (including gusts) is 15 knots. 

b. The maximum wind gust for landing is 5 knots. 

c. Maximum tailwind component approved for takeoff and landing: 10 knots 

d. When operating in a flight control law mode other than normal (i.e., alternate, 

direct, or backup), maximum crosswind component for landing: 10 knots 

e. Maximum tailwind component for landing with flaps 10° or less is zero knots. 

Figure 8 to paragraph G)(2)-Section 01-03-10: Types of Airplane 

Operations Permitted 

01-03-10: Types of Airplane Operations Permitted 

2. Day and Night, Visual and Instrument Flight Rules 

a. All approaches must be stabilized by 1000 ft AGL, including visual maneuvers. 

b. Vertical guidance from an ILS or FMS-based approach is required for night 

landings. 
Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 27503 

(4) To Section 01–22–10: ‘‘Autothrottle,’’ of 

Chapter 01, ‘‘LIMITATIONS,’’ add the 

information in figure 10 to paragraph (j)(4) of 

this AD. 


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Figure 9 to paragraph (j)(3)-Section 01-03-40: Airspeed Limitations 

01-03-40: Airspeed Limitations 

15. Approach Speed 

a. Approach speed additives (Flaps 39) are half the steady state wind plus the 

gust increment up to a maximum additive of 20 knots. 

b. Minimum approach speed during normal operations is VREF + 10 knots, unless 

otherwise specified in a non-normal procedure. 

c. Approach Speed shall be maintained to the runway threshold and shall be 

used to determine landing performance except for abnormal flap approaches. 

Abnormal flap approaches must comply with the procedures in section 

03-12-10: Zero Flaps or Partial Flaps Landings. 

Figure 10 to paragraph (j)(4)- Section 01-22-10: Autothrottle 

01-22-10: Autothrottle 

2. Use of the Autothrottle for approach and landing is required during normal 

operations. I Note 

Pilot will physically guard the throttles until touchdown, and override or disconnect the 

autothrottle if performance is not as expected. 
27504 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 

(5) Replace the ‘‘WARNING’’ information 

preceding ‘‘Approach/Landing Airspeeds’’ of 

Section 02–05–50: ‘‘Landing,’’ of Chapter 02, 

‘‘NORMAL OPERATIONS,’’ with the 

information in figure 11 to paragraph (j)(5) of 

this AD. 

(6) Replace the ‘‘Introduction’’ and 

‘‘Examples’’ sections of Section 05–11–10: 

‘‘Threshold Speeds’’ of Chapter 05, 

‘‘PERFORMANCE,’’ with the information in 

figure 12 to paragraph (j)(6) of this AD. 


khammond on DSKJM1Z7X2PROD with RULESER09MY22.049</GPH>

Figure 11 to paragraph (j)(S) - Section 02-05-50: Landing 

02-05-50: Landing 

WARNING 

EXCEPT AS REQUIRED IN AN EMERGENCY OR AS DIRECTED BY A 

NON-NORMAL PROCEDURE, MINIMUM APPROACH SPEED IS VREF 

+10. APPROACH SPEED SHALL BE MAINTAINED TO THE 

THRESHOLD AND SHALL BE USED TO DETERMINE LANDING 

DISTANCE. 

4. Approach/Landing Airspeeds ...................................................... Verify 
Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 27505 


khammond on DSKJM1Z7X2PROD with RULESER09MY22.050</GPH>

Figure 12 to paragraph (j)(6)-Section 05-11-10: Threshold Speeds 

05-11-10: Threshold Speeds 

Introduction 

1. Threshold speeds, VREF, for landing distance are shown for normal flap setting 39° 

in Figure 1. Threshold Speed for Landing Distance, Flaps 39°, Wing Anti-Ice OFF 

And ON for Wing Anti-Ice OFF and ON operations. Abnormal flap settings 20° and 

10° threshold speeds for Wing Anti-Ice OFF and ON conditions are shown in 

Figure 2. Threshold Speed for Landing Distance, Flaps 20°, Wing Anti-Ice OFF 

And ON and Figure 3. Threshold Speed for Landing Distance, Flaps 10°, Wing 

Anti-Ice OFF And ON. For the abnormal flap setting 0°, threshold speeds shown in 

Figure 4. Threshold Speed for Landing Distance, Flaps 0°, Wing Anti-Ice ON are 

effective for Wing Anti-Ice ON operations. 

2. Normally, landings will be conducted only at the landing flap setting of 39°. 

Additional charts are provided for reduced flap settings to be used when an 

abnormal landing at a reduced flap setting is required. The landing threshold 

speeds shown are effective throughout the certified weight, temperature and 

altitude range of the airplane. 

I WARNING 

EXCEPT AS REQUIRED IN AN EMERGENCY OR AS DIRECTED BY A NONNORMAL PROCEDURE, MINIMUM APPROACH SPEED IS VREF +10. 

APPROACH SPEED SHALL BE MAINTAINED TO THE THRESHOLD AND 

SHALL BE USED TO DETERMINE LANDING DISTANCE. 

I CAUTION 

TIRESPEED LIMITATIONS WILL BE EXCEEDED IF TOUCHDOWN IS MADE IN 

EXCESS OF 195 KNOTS GROUNDSPEED. 

NOTE 

Landing distance in 05-11-30: Landing Distance and maximum landing weight 05-

11-20: Tire Speed and BKE Limited Maximum Landing Weight shall be calculated 

utilizing planned speed at the threshold. 

Examples 

Determine the final approach and threshold speeds for landing at a normal flap (39°) 

setting. 

Given: 

• Landing Gross Weight= 58,000 pounds (26,308 kg) 

• Airport Pressure Altitude = 2000 feet 

Solution: 

• Threshold Speed (VREF) = 111 KIAS 

• Final Approach Speed (VREF +10 KIAS) = 121 KIAS 
27506 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Rules and Regulations 

BILLING CODE 4910–13–C 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Atlanta 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 responsible Flight 

Standards 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 (l) of this 

AD. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the responsible Flight Standards Office. 

(3) AMOC 7A0–22–06968, dated April 29, 

2022, was approved as an AMOC for the 

requirements for AD 2020–05–12, and is 

approved as an AMOC for the requirements 

of paragraphs (g) and (h) of this AD. Other 

AMOCs previously issued for the 

requirements of AD 2020–05–12 are not 

approved as an AMOC for the requirements 

of this AD. 

(l) Related Information 

For more information about this AD, 

contact Sanford Proveaux, Aerospace 

Engineer, Certificate Management and Safety 

Oversight Section, FAA, Atlanta ACO 

Branch, 1701 Columbia Avenue, College 

Park, GA 30337; phone: 404–474–5566; 

email: Sanford.Proveaux@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. 

(3) The following service information was 

approved for IBR on March 13, 2020 (85 FR 

14562, March 13, 2020). 

(i) Gulfstream GVII–G500 Airplane Flight 

Manual, GAC–AC–GVII–G500–OPS–0001, 

Revision 5, dated March 3, 2020. 

(A) Section 01–27–10, ‘‘Normal Control 

Laws,’’ of Chapter 01, ‘‘LIMITATIONS.’’ 

(B) Step 8., ‘‘Final Approach Fix,’’ of 

Section 04–08–40, ‘‘One Engine Inoperative 

Landing Procedure,’’ of Chapter 04, 

‘‘EMERGENCY PROCEDURES.’’ 

(C) Step 11., ‘‘Landing,’’ of Section 03–12– 

10, ‘‘Zero Flaps or Partial Flaps Landings,’’ 

of Chapter 03, ‘‘ABNORMAL 

PROCEDURES.’’ 

(D) Step 15., ‘‘Approach Speed,’’ of Section 

01–03–40, ‘‘Airspeed Limitations,’’ of 

Chapter 01, ‘‘LIMITATIONS.’’ 

(ii) Gulfstream GVII–G600 Airplane Flight 

Manual, GAC–AC–GVII–G600–OPS–0001, 

Revision 3, dated March 3, 2020. 

(A) Section 01–27–10, ‘‘Normal Control 

Laws,’’ of Chapter 01, ‘‘LIMITATIONS.’’ 

(B) Steps 3. and 4. of Section 01–34–40, 

‘‘Takeoff and Landing Data (TOLD),’’ of 

Chapter 01, ‘‘LIMITATIONS.’’ 

(C) Step 8., ‘‘Final Approach Fix,’’ of 

Section 04–08–40, ‘‘One Engine Inoperative 

Landing Procedure,’’ of Chapter 04, 

‘‘EMERGENCY PROCEDURES.’’ 

(D) Step 11., ‘‘Landing,’’ of Section 03–12– 

10, ‘‘Zero Flaps or Partial Flaps Landings,’’ 

of Chapter 03, ‘‘ABNORMAL 

PROCEDURES.’’ 

(4) For service information identified in 

this AD, contact Gulfstream Aerospace 

Corporation, Technical Publications Dept., 

P.O. Box 2206, Savannah, GA 31402–2206; 

telephone 800–810–4853; fax 912–965–3520; 

email pubs@gulfstream.com; internet http://

www.gulfstream.com/customer-support. 

(5) You may view this 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 

206–231–3195. 

(6) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

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

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

Issued on May 2, 2022. 

Ross Landes, 

Deputy Director for Regulatory Operations, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2022–09925 Filed 5–5–22; 11:15 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2022–0129; Airspace 

Docket No. 22–AGL–8] 

RIN 2120–AA66 

Amendment of Class E Airspace; 

Marshall, MI 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action amends the Class 

E airspace at Marshall, MI. This action 

as the result of an airspace review 

conducted as part of the 

decommissioning of the Litchfield very 

high frequency (VHF) omnidirectional 

range (VOR) as part of the VOR Minimal 

Operational Network (MON) Program. 

DATES: Effective 0901 UTC, July 14, 

2022. The Director of the Federal 

Register approves this incorporation by 

reference action under 1 CFR 51, subject 

to the annual revision of FAA Order JO 

7400.11 and publication of conforming 

amendments. 

ADDRESSES: FAA Order JO 7400.11F, 

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. 

FOR FURTHER INFORMATION CONTACT: 

Jeffrey Claypool, Federal Aviation 

Administration, Operations Support 

Group, Central Service Center, 10101 

Hillwood Parkway, Fort Worth, TX 

76177; telephone (817) 222–5711. 

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 at Brooks 

Field, Marshall, MI, to support 

instrument flight rule operations at this 

airport. 

History 

The FAA published a notice of 

proposed rulemaking in the Federal 

Register (87 FR 11358; March 1, 2022) 

for Docket No. FAA–2022–0129 to 

amend the Class E airspace at Marshall, 

MI. Interested parties were invited to 

participate in this rulemaking effort by 

submitting written comments on the 

proposal to the FAA. No comments 

were received. 

Class E airspace designations are 

published in paragraph 6005 of FAA 

Order JO 7400.11F, dated August 10, 

2021, and effective September 15, 2021, 

which is incorporated by reference in 14 

CFR 71.1. The Class E airspace 

designations listed in this document 

will be published subsequently in FAA 

Order JO 7400.11. 

Availability and Summary of 

Documents for Incorporation by 

Reference 

This document amends FAA Order JO 

7400.11F, Airspace Designations and 

Reporting Points, dated August 10, 

2021, and effective September 15, 2021. 

FAA Order JO 7400.11F is publicly 

available as listed in the ADDRESSES


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