100926 Federal Register / Vol. 89, No. 240 / Friday, December 13, 2024 / Proposed Rules 

bleed system. The FAA is issuing this AD to 

address the unsafe condition, which if not 

addressed, could result in dual engine 

failure. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Requirements 

Except as specified in paragraph (h) of this 

AD: Comply with all required actions and 

compliance times specified in, and in 

accordance with Transport Canada AD CF– 

2024–30, dated August 27, 2024 (Transport 

Canada AD CF–2024–30). 

(h) Exception to Transport Canada AD CF– 

2024–30 

(1) Where Transport Canada AD CF–2024– 

30 refers to its effective date, this AD requires 

using the effective date of this AD. 

(2) Where paragraph B. of Transport 

Canada AD CF–2024–30 specifies to ‘‘inform 

all flight crews of these changes in the AFM 

procedures and thereafter operate the 

aeroplane accordingly,’’ this AD does not 

require those actions as those actions are 

already required by existing FAA operating 

regulations (see 14 CFR 91.9, 14 CFR 91.505, 

and 14 CFR 121.137). 

(i) Additional AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Validation Branch, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or 

responsible Flight Standards Office, as 

appropriate. If sending information directly 

to the manager of the International Validation 

Branch, send it to the attention of the person 

identified in paragraph (j) of this AD and 

email to: AMOC@faa.gov. Before using any 

approved AMOC, notify your appropriate 

principal inspector, or lacking a principal 

inspector, the manager of the responsible 

Flight Standards Office. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain instructions 

from a manufacturer, the instructions must 

be accomplished using a method approved 

by the Manager, International Validation 

Branch, FAA; or Transport Canada; or Airbus 

Canada Limited Partnership’s Transport 

Canada Design Approval Organization 

(DAO). If approved by the DAO, the approval 

must include the DAO-authorized signature. 

(j) Additional Information 

For more information about this AD, 

contact Joseph Catanzaro, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; phone: 516–228– 

7300; email: 9-avs-nyaco-cos@faa.gov. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the material listed in this paragraph under 5 

U.S.C. 552(a) and 1 CFR part 51. 

(2) You must use this material as 

applicable to do the actions required by this 

AD, unless this AD specifies otherwise. 

(i) Transport Canada AD CF–2024–30, 

dated August 27, 2024. 

(ii) [Reserved] 

(3) For Transport Canada material 

identified in this AD, contact Transport 

Canada, Transport Canada National Aircraft 

Certification, 159 Cleopatra Drive, Nepean, 

Ontario K1A 0N5, Canada; telephone 888– 

663–3639; email TC.AirworthinessDirectivesConsignesdenavigabilite.TC@tc.gc.ca; 

website at tc.canada.ca/en/aviation. 

(4) You may view this material at the FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 2200 South 216th St., Des 

Moines, WA. For information on the 

availability of this material at the FAA, call 

206–231–3195. 

(5) You may view this material at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

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

ibr-locations or email fr.inspection@nara.gov. 

Issued on December 9, 2024. 

Peter A. White, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–29302 Filed 12–12–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2556; Project 

Identifier MCAI–2024–00247–T] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to adopt a 

new airworthiness directive (AD) for 

certain Airbus SAS Model A300 series 

airplanes; Model A300 B4–600, B4– 

600R, and F4–600R series airplanes, and 

Model A300 C4–605R Variant F 

airplanes (collectively called Model 

A300–600 series airplanes); and Model 

A310 series airplanes. This proposed 

AD was prompted by investigations that 

found cracks on the main deck cargo 

door (MDCD) actuator bearing fitting 

caused by fatigue. This proposed AD 

would require an operational limitation 

to the MDCD opening angle, repetitive 

detailed visual inspection (DET) of the 

MDCD actuator bearing fittings, and 

replacement if any cracks are found, as 

specified in a European Union Aviation 

Safety Agency (EASA) AD, which is 

proposed for incorporation by reference 

(IBR). The FAA is proposing this AD to 

address the unsafe condition on these 

products. 

DATES: The FAA must receive comments 

on this proposed AD by January 27, 

2025. 

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 

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. 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–2556; 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 NPRM, the mandatory 

continuing airworthiness information 

(MCAI), any comments received, and 

other information. The street address for 

Docket Operations is listed above. 

Material Incorporated by Reference: 

• For EASA material identified in this 

proposed AD, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne, 

Germany; telephone +49 221 8999 000; 

email ADs@easa.europa.eu; website 

easa.europa.eu. You may find this 

material on the EASA website at 

ad.easa.europa.eu. It is also available at 

regulations.gov under Docket No. FAA– 

2024–2556. 

• You may view this material at the 

FAA, Airworthiness Products Section, 

Operational Safety Branch, 2200 South 

216th St., Des Moines, WA. For 

information on the availability of this 

material at the FAA, call 206–231–3195. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aviation Safety Engineer, FAA, 

1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; phone: 206–231– 

3225; email: Dan.Rodina@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

The FAA invites you to send any 

written relevant data, views, or 

arguments about this proposal. Send 

your comments to an address listed 

under the ADDRESSES section. Include 

‘‘Docket No. FAA–2024–2556; Project 

Identifier MCAI–2024–00247–T’’ at the 


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Federal Register / Vol. 89, No. 240 / Friday, December 13, 2024 / Proposed Rules 100927 

beginning of your comments. The most 

helpful comments reference a specific 

portion of the proposal, 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 

proposal 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 

regulations.gov, including any personal 

information you provide. The agency 

will also post a report summarizing each 

substantive verbal contact received 

about this NPRM. 

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 NPRM 

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 NPRM, 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 

NPRM. Submissions containing CBI 

should be sent to Dan Rodina, Aviation 

Safety Engineer, FAA, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 

11590; phone: 206–231–3225; email: 

Dan.Rodina@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. 

Background 

EASA, which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2024– 

0092R1, dated July 10, 2024 (EASA AD 

2024–0092R1) (also referred to as the 

MCAI), to correct an unsafe condition 

for certain Airbus SAS Model A300 

series, A300–600 series, and A310 series 

airplanes. The MCAI states that 

investigations found cracks on the 

MDCD actuator bearing fitting caused by 

fatigue. There is no unsafe condition 

during flight when the cargo door if 

fully closed, latched, and locked. 

However, if not detected and corrected, 

this cracking could lead to MDCD 

undamped free fall from the open 

position during MDCD operations or 

during cargo loading/off-loading, 

resulting in injury to people on the 

ground. 

The FAA is proposing this AD to 

address the unsafe condition on these 

products. 

You may examine the MCAI in the 

AD docket at regulations.gov under 

Docket No. FAA–2024–2556. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

EASA AD 2024–0092R1 specifies 

procedures for an operational limitation 

to the MDCD opening angle, repetitive 

DET of the MDCD actuator bearing 

fittings, and replacement of both MDCD 

actuator bearing fittings if any crack is 

found on any MDCD actuator bearing 

fitting. 

This material is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section. 

FAA’s Determination 

This product has been approved by 

the aviation authority of another 

country and is approved for operation in 

the United States. Pursuant to the FAA’s 

bilateral agreement with this State of 

Design Authority, it has notified the 

FAA of the unsafe condition described 

in the MCAI referenced above. The FAA 

is issuing this NPRM after determining 

that the unsafe condition described 

previously is likely to exist or develop 

in other products of the same type 

design. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would require 

accomplishing the actions specified in 

EASA AD 2024–0092R1 described 

previously, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD. 

Explanation of Required Compliance 

Information 

In the FAA’s ongoing efforts to 

improve the efficiency of the AD 

process, the FAA developed a process to 

use some civil aviation authority (CAA) 

ADs as the primary source of 

information for compliance with 

requirements for corresponding FAA 

ADs. The FAA has been coordinating 

this process with manufacturers and 

CAAs. As a result, the FAA proposes to 

incorporate EASA AD 2024–0092R1 by 

reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2024– 

0092R1 in its entirety through that 

incorporation, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD. 

Using common terms that are the same 

as the heading of a particular section in 

EASA AD 2024–0092R1 does not mean 

that operators need comply only with 

that section. For example, where the AD 

requirement refers to ‘‘all required 

actions and compliance times,’’ 

compliance with this AD requirement is 

not limited to the section titled 

‘‘Required Action(s) and Compliance 

Time(s)’’ in EASA AD 2024–0092R1. 

Material required by EASA AD 2024– 

0092R1 for compliance will be available 

at regulations.gov under Docket No. 

FAA–2024–2556 after the FAA final 

rule is published. 

Interim Action 

The FAA considers that this proposed 

AD would be an interim action. If final 

action is later identified, the FAA might 

consider further rulemaking then. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 128 

airplanes of U.S. registry. The FAA 

estimates the following costs to comply 

with this proposed AD: 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

1 work-hour × $85 per hour = $85 .............................................................................................. $0 $85 $10,880 

The FAA estimates the following 

costs to do any necessary on-condition 

actions that would be required based on 

the results of any required actions. The 

FAA has no way of determining the 


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100928 Federal Register / Vol. 89, No. 240 / Friday, December 13, 2024 / Proposed Rules 

number of aircraft that might need this 

on-condition action: 

ESTIMATED COSTS OF ON-CONDITION ACTIONS

Labor cost Parts cost Cost per product 

500 work-hours × $85 per hour = $42,500 ..................................................................................................... $34,600 $77,100 

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 

The FAA determined that this 

proposed AD would not have federalism 

implications under Executive Order 

13132. This proposed AD would 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 this proposed regulation: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Would not affect intrastate 

aviation in Alaska, and 

(3) Would not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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: 

Airbus SAS: Docket No. FAA–2024–2556; 

Project Identifier MCAI–2024–00247–T. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by January 27, 

2025. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the Airbus SAS 

airplanes identified in paragraphs (c)(1) 

through (6) of this AD, certified in any 

category, manufactured in freighter model 

configuration. 

(1) Model A300 B4–2C, B4–103, and B4– 

203 airplanes. 

(2) Model A300 B4–601, B4–603, B4–620, 

and B4–622 airplanes. 

(3) Model A300 B4–605R and B4–622R 

airplanes. 

(4) Model A300 C4–605R Variant F 

airplanes. 

(5) Model A300 F4–605R and F4–622R 

airplanes. 

(6) Model A310–203, –204, –221, –222, 

–304, –322, –324, and –325 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 52, Doors. 

(e) Unsafe Condition 

This AD was prompted by investigations 

that found cracks on the main deck cargo 

door (MDCD) actuator bearing fitting caused 

by fatigue. The FAA is issuing this AD to 

address potential cracking of the MDCD 

actuator bearing fittings. The unsafe 

condition, if not addressed, could lead to 

MDCD undamped free fall from open 

position during MDCD operations or during 

cargo loading/off-loading, resulting in injury 

to people on the ground. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Requirements 

Except as specified in paragraphs (h) and 

(i) of this AD: Comply with all required 

actions and compliance times specified in, 

and in accordance with, European Union 

Aviation Safety Agency (EASA) AD 2024– 

0092R1, dated July 10, 2024 (EASA AD 

2024–0092R1). 

(h) Exceptions to EASA AD 2024–0092R1 

(1) Where EASA AD 2024–0092R1 refers to 

April 26, 2024 (the effective date of the 

original issue of EASA AD 2024–0092R1), 

this AD requires using the effective date of 

this AD. 

(2) This AD does not adopt the ‘‘Remarks’’ 

section of EASA AD 2024–0092R1. 

(i) No Reporting Requirement 

Although the material referenced in EASA 

AD 2024–0092R1 specifies to submit certain 

information to the manufacturer, this AD 

does not include that requirement. 

(j) Additional AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Validation Branch, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or 

responsible Flight Standards Office, as 

appropriate. If sending information directly 

to the manager of the International Validation 

Branch, send it to the attention of the person 

identified in paragraph (k) of this AD and 

email to: AMOC@faa.gov. Before using any 

approved AMOC, notify your appropriate 

principal inspector, or lacking a principal 

inspector, the manager of the responsible 

Flight Standards Office. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain instructions 

from a manufacturer, the instructions must 

be accomplished using a method approved 

by the Manager, International Validation 

Branch, FAA; or EASA; or Airbus SAS’s 

EASA Design Organization Approval (DOA). 

If approved by the DOA, the approval must 

include the DOA-authorized signature. 

(3) Required for Compliance (RC): Except 

as required by paragraph (j)(2) of this AD, if 

any material referenced in EASA AD 2024– 

0092R1 contains paragraphs that are labeled 

as RC, the instructions in RC paragraphs, 

including subparagraphs under an RC 

paragraph, must be done to comply with this 

AD; any paragraphs, including subparagraphs 

under those paragraphs, that are not 

identified as RC are recommended. The 

instructions in paragraphs, including 

subparagraphs under those paragraphs, not 


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Federal Register / Vol. 89, No. 240 / Friday, December 13, 2024 / Proposed Rules 100929 

identified as RC may be deviated from using 

accepted methods in accordance with the 

operator’s maintenance or inspection 

program without obtaining approval of an 

AMOC, provided the instructions identified 

as RC can be done and the airplane can be 

put back in an airworthy condition. Any 

substitutions or changes to instructions 

identified as RC require approval of an 

AMOC. 

(k) Additional Information 

For more information about this AD, 

contact Dan Rodina, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; phone: 206–231– 

3225; email: Dan.Rodina@faa.gov. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the material listed in this paragraph under 5 

U.S.C. 552(a) and 1 CFR part 51. 

(2) You must use this material as 

applicable to do the actions required by this 

AD, unless this AD specifies otherwise. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2024–0092R1, dated July 10, 

2024. 

(ii) [Reserved]. 

(3) For EASA material identified in this 

AD, contact EASA, Konrad-Adenauer-Ufer 3, 

50668 Cologne, Germany; telephone +49 221 

8999 000; email ADs@easa.europa.eu; 

website easa.europa.eu. You may find this 

material on the EASA website at 

ad.easa.europa.eu. 

(4) You may view this material at the FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 2200 South 216th St., Des 

Moines, WA. For information on the 

availability of this material at the FAA, call 

206–231–3195. 

(5) You may view this material at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

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

ibr-locations or email fr.inspection@nara.gov. 

Issued on December 9, 2024. 

Peter A. White, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–29356 Filed 12–12–24; 8:45 am] 

BILLING CODE 4910–13–P 

ENVIRONMENTAL PROTECTION 

AGENCY 

40 CFR Part 122 

[EPA–HQ–OW–2021–0169; FRL–12219–01– 

OW] 

Modification to 2022 National Pollutant 

Discharge Elimination System 

(NPDES) Construction General Permit 

(CGP) for Stormwater Discharges From 

Construction Activities 

AGENCY: Environmental Protection 

Agency (EPA). 

ACTION: Notification; request for public 

comment. 

SUMMARY: The Environmental Protection 

Agency (EPA) is proposing a narrow 

modification to its 2022 CGP to expand 

the list of areas eligible for coverage to 

include construction projects in Lands 

of Exclusive Federal Jurisdiction. This 

modification is necessary because the 

EPA is the permitting authority in Lands 

of Exclusive Federal Jurisdiction, and 

when the CGP was issued on February 

17, 2022, the permit did not specifically 

provide eligibility for all of these areas. 

The proposed modification would also 

clarify the CGP requirements that apply 

to projects that discharge to receiving 

waters within Lands of Exclusive 

Federal Jurisdiction. The EPA seeks 

comment only on the proposed permit 

revisions and the accompanying fact 

sheet. The fact sheet and proposed 

permit modification can be found at 

https://www.epa.gov/npdes/stormwaterdischarges-construction-activities. 

DATES: Comments on the proposed 

permit modification must be received 

on or before January 13, 2025. 

ADDRESSES: You may send comments, 

identified by Docket ID No. EPA–HQ– 

OW–2021–0169, by any of the following 

methods: 

• Federal eRulemaking Portal: 

https://www.regulations.gov/. Follow 

the online instructions for submitting 

comments. 

• Mail: U.S. Environmental 

Protection Agency, EPA Docket Center, 

Office of Water, Docket, Mail Code 

28221T, 1200 Pennsylvania Avenue 

NW, Washington, DC 20460. 

• Hand Delivery or Courier: EPA 

Docket Center, WJC West Building, 

Room 3334, 1301 Constitution Avenue 

NW, Washington, DC 20004. The Docket 

Center’s hours of operations are 8:30 

a.m. to 4:30 p.m., Monday—Friday 

(except Federal Holidays). 

Instructions: All submissions received 

must include the Docket ID No. for this 

rulemaking. Comments received may be 

posted without change to https://

www.regulations.gov, including 

personal information provided. For 

detailed instructions on sending 

comments and additional information 

on the rulemaking process, see the 

‘‘Public Participation’’ heading of the 

SUPPLEMENTARY INFORMATION section of 

this document. 

FOR FURTHER INFORMATION CONTACT: Greg 

Schaner, EPA Headquarters, Office of 

Water, Office of Wastewater 

Management at (202) 564–0721 or by 

email at schaner.greg@epa.gov. 

SUPPLEMENTARY INFORMATION: This 

section is organized as follows: 

Table of Contents 

I. General Information 

A. Does this action apply to me? 

B. Public Participation 

C. Finalizing the Proposed Permit 

Modification 

D. Who are the EPA Regional Contacts for 

This Permit? 

II. Permit Modification Background 

A. Permitting of Stormwater Discharges 

From Construction Activities 

B. Background on Lands of Exclusive 

Federal Jurisdiction 

C. Why is a Modification to the 2022 CGP 

Necessary 

III. Summary of Proposed Permit Changes 

IV. Public Notice of Clean Water Act Section 

401 Certification for Lands of Exclusive 

Federal Jurisdiction 

V. Paperwork Reduction Act (PRA) 

VI. 2022 CGP Incremental Cost Analysis 

VII. Executive Order 12866: Regulatory 

Planning and Review and Executive 

Order 14094: Modernizing Regulatory 

Review 

VIII. Executive Order 12898: Federal Actions 

To Address Environmental Justice in 

Minority Populations and Low-Income 

Populations and Executive Order 14096: 

Revitalizing Our Nation’s Commitment 

to Environmental Justice for All 

IX. Executive Order 13175: Consultation and 

Coordination With Indian Tribal 

Governments 

X. Executive Order 13211: Actions That 

Significantly Affect Energy Supply, 

Distribution, or Use 

XI. Compliance With the National 

Environmental Policy Act (NEPA) for the 

National Pollutant Discharge Elimination 

System (NPDES) General Permit for 

Discharges from Construction Activities 

I. General Information 

A. Does this action apply to me? 

This proposed permit modification 

covers the following entities, as 

categorized in the North American 

Industry Classification System (NAICS), 

where they are conducting construction 

activities in Lands of Exclusive Federal 

Jurisdiction: 


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