93230 Federal Register / Vol. 89, No. 228 / Tuesday, November 26, 2024 / Proposed Rules 

(g) Required Actions 

(1) Within the compliance times specified 

in paragraphs (g)(1)(i) through (iii) of this AD, 

replace the affected stage 1 turbine forward 

cooling plate or stage 2 turbine aft cooling 

plate, as applicable, with a replacement P/N 

eligible for installation, in accordance with 

Table 1 to paragraph (g)(1) of this AD: 

(i) For Group 1 engines with an affected 

part installed, replace the affected part at the 

next exposure of the gas generator stator 

assembly that occurs after the effective date 

of this AD. 

(ii) For Group 2 engines with an affected 

part installed having 7,000 part cycles since 

new (PCSN) or less as of the effective date 

of this AD, replace the affected part at the 

next exposure of the gas generator stator 

assembly or within 2,000 flight cycles (FCs) 

but before reaching 7,500 PCSN, whichever 

occurs first after the effective date of this AD. 

(iii) For Group 2 engines with an affected 

part installed having more than 7,000 PCSN 

as of the effective date of this AD, replace the 

affected part at the next exposure of the gas 

generator stator assembly or within 500 FCs, 

whichever occurs first after the effective date 

of this AD. 

TABLE 1 TO PARAGRAPH (g)(1): COOLING PLATE REPLACEMENT P/NS

Engine group Part name Affected P/N Replacement P/N 

1 ............................ Stage 1 turbine forward cooling plate ............................................................ 6064T08P01 6064T08P04 

1 ............................ Stage 2 turbine aft cooling plate .................................................................... 6064T07P05 6064T07P07 

1 ............................ Stage 2 turbine aft cooling plate .................................................................... 6068T36P01 6068T36P04 

2 ............................ Stage 1 turbine forward cooling plate ............................................................ 6064T08P01 6064T08P03 or 

6064T08P04 

2 ............................ Stage 2 turbine aft cooling plate .................................................................... 6064T07P05 6064T07P07 

2 ............................ Stage 2 turbine aft cooling plate .................................................................... 6068T36P01 6068T36P04 

(h) Definitions 

For the purpose of this AD: 

(1) ‘‘Group 1 engines’’ are GE Model CT7– 

5A2, CT7–5A3, CT7–9B, CT7–9B1, CT7–9B2, 

CT7–9D, and CT7–9D2 engines. 

(2) ‘‘Group 2 engines’’ are GE Model CT7– 

7A, CT7–7A1, CT7–9C, and CT7–9C3 

engines. 

(3) ‘‘Exposure of the gas generator stator 

assembly’’ is when the gas generator rotor 

and stator assembly are separated from the 

combustor module. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, AIR–520 Continued 

Operational Safety 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 AIR–520 Continued 

Operational Safety Branch, send it to the 

attention of the person identified in 

paragraph (j) of this AD and email to: 

AMOC@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/ 

certificate holding district office. 

(j) Additional Information 

For more information about this AD, 

contact Sungmo Cho, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, Des 

Moines, WA 98198; phone: (781) 238–7241; 

email: sungmo.d.cho@faa.gov. 

(k) Material Incorporated by Reference 

None. 

Issued on November 20, 2024. 

Peter A. White, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–27664 Filed 11–25–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2538; Project 

Identifier MCAI–2023–01211–E] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

Deutschland Ltd & Co KG Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to 

supersede Airworthiness Directive (AD) 

2022–24–06, which applies to certain 

Rolls-Royce Deutschland Ltd & Co KG 

(RRD) Model BR700–710A1–10, BR700– 

710A2–20, and BR700–710C4–11 

engines. AD 2022–24–06 requires initial 

and repetitive visual inspections of 

certain low-pressure compressor (LPC) 

rotor (fan) disks and replacement of any 

LPC rotor (fan) disk with cracks 

detected. AD 2022–24–06 also allows 

for modification of the engine in 

accordance with RRD service 

information as a terminating action to 

these inspections. Since the FAA issued 

AD 2022–24–06, the manufacturer 

published updated service information 

and revised the engine maintenance 

manual (EMM) to provide instructions 

for an improved ultrasonic inspection 

method, which prompted this AD. This 

proposed AD would require initial and 

repetitive visual inspections of certain 

LPC rotor (fan) disks and replacement of 

any LPC rotor (fan) disk with cracks 

detected and would allow modification 

of the engine as a terminating action to 

the inspections, as specified in a 

European Union Aviation Safety Agency 

(EASA) AD, which is proposed for 

incorporation by reference. The FAA is 

proposing this AD to address the unsafe 

condition on these products. 

DATES: The FAA must receive comments 

on this NPRM by January 10, 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–2024–2538; 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; phone: +49 221 8999 000; 

email: ADs@easa.europa.eu. You may 

find this material on the EASA website 

at ad.easa.europa.eu. 

• You may view this material at the 

FAA, Airworthiness Products Section, 

Operational Safety Branch, 1200 District 


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Federal Register / Vol. 89, No. 228 / Tuesday, November 26, 2024 / Proposed Rules 93231 

Avenue, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call (817) 222– 

5110. 

FOR FURTHER INFORMATION CONTACT: 

Barbara Caufield, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, 

Des Moines, WA 98198; phone: (781) 

238–7146; email: barbara.caufield@

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 ADDRESSES. Include ‘‘Docket No. 

FAA–2024–2538; Project Identifier 

MCAI–2023–01211–E’’ at the 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 the 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 Barbara Caufield, 

Aviation Safety Engineer, FAA, 2200 

South 216th Street, Des Moines, WA 

98198. Any commentary that the FAA 

receives which is not specifically 

designated as CBI will be placed in the 

public docket for this rulemaking. 

Background 

The FAA issued AD 2022–24–06, 

Amendment 39–22246 (87 FR 73919, 

December 2, 2022) (AD 2022–24–06), for 

certain RRD Model BR700–710A1–10, 

BR700–710A2–20, and BR700–710C4– 

11 engines. AD 2022–24–06 was 

prompted by an MCAI originated by 

EASA, which is the Technical Agent for 

the Member States of the European 

Union. EASA issued AD 2022–0110, 

dated June 15, 2022 (EASA AD 2022– 

0110), to correct an unsafe condition 

identified as cracks on certain LPC rotor 

(fan) disks. 

AD 2022–24–06 requires initial and 

repetitive visual inspections of certain 

LPC rotor (fan) disks and replacement of 

any LPC rotor (fan) disk with cracks 

detected. The FAA issued AD 2022–24– 

06 to prevent failure of the LPC rotor fan 

or blade. 

Actions Since AD 2022–24–06 Was 

Issued 

Since the FAA issued AD 2022–24– 

06, EASA superseded EASA AD 2022– 

0110 and issued AD 2022–0110R1, 

dated November 22, 2023 (EASA AD 

2022–0110R1) (also referred to as the 

MCAI). The MCAI states that the 

manufacturer published updated service 

information and revised the EMM to 

provide instructions for an improved 

ultrasonic inspection method for certain 

LPC rotor (fan) disks. 

You may examine the MCAI in the 

AD docket at regulations.gov under 

Docket No. FAA–2024–2538. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

The FAA reviewed EASA AD 2022– 

0110R1, which specifies procedures for 

initial and repetitive visual inspections 

of certain LPC rotor (fan) disks, and 

replacement of any LPC rotor (fan) disk 

with cracks detected. 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 

These products have been approved 

by the aviation authority of another 

country and are 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 on other products of 

the same type design. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would retain all of 

the requirements of AD 2022–24–06. 

This proposed AD would require 

accomplishing the actions specified in 

the MCAI described previously, except 

for any differences identified as 

exceptions in the regulatory text of this 

proposed AD. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 586 

engines installed on airplanes of U.S. 

registry. 

The FAA estimates the following 

costs to comply with this proposed AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspect LPC compressor rotor (fan) disk ........ 4 work-hours × $85 per hour = $340 ............. $0 $340 $199,240 

The FAA estimates the following 

costs to do any necessary replacements 

that would be required based on the 

results of the proposed inspection. The 

agency has no way of determining the 

number of engines that might need these 

replacements: 


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93232 Federal Register / Vol. 89, No. 228 / Tuesday, November 26, 2024 / Proposed Rules 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per 

product 

Replace LPC compressor rotor (fan) disk .................... 10 work-hours × $85 per hour = $850 ......................... $470,000 $470,850 

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 that the 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: 

■ a. Removing Airworthiness Directive 

2022–24–06, Amendment 39–22246 (87 

FR 73919, December 2, 2022); and 

■ b. Adding the following new 

airworthiness directive: 

Rolls-Royce Deutschland Ltd & Co KG: 

Docket No. FAA–2024–2538; Project 

Identifier MCAI–2023–01211–E. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by January 10, 

2025. 

(b) Affected ADs 

This AD replaces AD 2022–24–06, 

Amendment 39–22246 (87 FR 73919, 

December 2, 2022) (AD 2022–24–06). 

(c) Applicability 

This AD applies to Rolls-Royce 

Deutschland Ltd & Co KG (RRD) Model 

BR700–710A1–10, BR700–710A2–20, and 

BR700–710C4–11 engines as identified in 

European Union Aviation Safety Agency AD 

2022–0110R1, dated November 22, 2023 

(EASA AD 2022–0110R1). 

(d) Subject 

Joint Aircraft Service Component (JASC) 

Code 7230, Turbine Engine Compressor 

Section. 

(e) Unsafe Condition 

This AD was prompted by reports of cracks 

on certain low-pressure compressor (LPC) 

rotor (fan) disks. The FAA is issuing this AD 

to prevent failure of the LPC rotor fan or 

blade. The unsafe condition, if not addressed, 

could result in high energy debris release, 

damage to the airplane, and reduced control 

of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

Except as specified in paragraphs (h) and 

(i) of this AD: Perform all required actions 

within the compliance times specified in, 

and in accordance with, EASA AD 2022– 

0110R1. 

(h) Exceptions to EASA AD 2022–0110R1 

(1) Where EASA AD 2022–0110R1 requires 

compliance from its effective date, this AD 

requires using the effective date of this AD. 

(2) Where EASA AD 2022–0110R1 requires 

compliance from ‘‘29 June 2022 [the effective 

date of the original issue of this AD],’’ this 

AD requires replacing that text with ‘‘January 

6, 2023 (the effective date of AD 2022–24– 

06).’’ 

(3) This AD does not require compliance 

with paragraph (7) of EASA AD 2022– 

0110R1. The actions required by paragraph 7 

of EASA AD 2022–0110R1 were included in 

AD 2022–26–02, Amendment 39–22280 (87 

FR 78846, December 23, 2022), and for this 

AD may be used for informational purposes. 

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

paragraph of EASA AD 2022–0110R1. 

(i) No Reporting Requirement 

Although the service information 

referenced in EASA AD 2022–0110R1 

specifies to submit certain information to the 

manufacturer, this AD does not include that 

requirement. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, AIR–520 Continued 

Operational Safety 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 AIR–520 Continued 

Operational Safety Branch, send it to the 

attention of the person identified in 

paragraph (k) of this AD and email to: 

AMOC@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. 

(k) Additional Information 

For more information about this AD, 

contact Barbara Caufield, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, Des 

Moines, WA 98198; phone: (781) 238–7146; 

email: barbara.caufield@faa.gov. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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 the AD specifies otherwise. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2022–0110R1, dated November 

22, 2023. 

(ii) [Reserved] 


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(3) For EASA material identified in this 

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

50668 Cologne, Germany; phone: +49 221 

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

website: easa.europa.eu. You may find this 

EASA AD on the EASA website at 

ad.easa.europa.eu. 

(4) You may view this material at FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 1200 District Avenue, 

Burlington, MA 01803. For information on 

the availability of this material at the FAA, 

call (817) 222–5110. 

(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 November 20, 2024. 

Peter A. White, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–27660 Filed 11–25–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2024–2512; Airspace 

Docket No. 24–AEA–9] 

RIN 2120–AA66 

Amendment of Domestic Very High 

Frequency Omnidirectional Range 

(VOR) Federal Airways V–1, V–29, V– 

38, V–139, and V–286; Eastern United 

States 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: This action proposes to 

amend domestic Very High Frequency 

Omnidirectional Range (VOR) Federal 

Airways V–1, V–29, V–38, V–139, and 

V–286 in the eastern United States. The 

FAA is taking this action due to the 

planned decommissioning of the 

Salisbury, MD (SBY) VOR/Tactical Air 

Navigation (VORTAC) and the Snow 

Hill, MD (SWL), VORTAC. This action 

is in support of the FAA’s VOR 

Minimum Operational Network (MON) 

Program. 

DATES: Comments must be received on 

or before January 10, 2025. 

ADDRESSES: Send comments identified 

by FAA Docket No. FAA–2024–2512 

and Airspace Docket No. 24–AEA–9 

using any of the following methods: 

* Federal eRulemaking Portal: Go to 

www.regulations.gov and follow the 

online instructions for sending your 

comments electronically. 

* Mail: Send comments to Docket 

Operations, M–30; U.S. Department of 

Transportation, 1200 New Jersey 

Avenue SE, Room W12–140, West 

Building Ground Floor, Washington, DC 

20590–0001. 

* Hand Delivery or Courier: Take 

comments to Docket Operations in 

Room W12–140 of the West Building 

Ground Floor at 1200 New Jersey 

Avenue SE, Washington, DC, between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. 

* Fax: Fax comments to Docket 

Operations at (202) 493–2251. 

Docket: Background documents or 

comments received may be read at 

www.regulations.gov at any time. 

Follow the online instructions for 

accessing the docket or go to the Docket 

Operations in Room W12–140 of the 

West Building Ground Floor at 1200 

New Jersey Avenue SE, Washington, 

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

through Friday, except Federal holidays. 

FAA Order JO 7400.11J, Airspace 

Designations and Reporting Points, and 

subsequent amendments can be viewed 

online at www.faa.gov/air_traffic/ 

publications/. You may also contact the 

Rules and Regulations Group, Policy 

Directorate, Federal Aviation 

Administration, 600 Independence 

Avenue SW, Washington, DC 20597; 

telephone: (202) 267–8783. 

FOR FURTHER INFORMATION CONTACT: 

Brian Vidis, Rules and Regulations 

Group, Policy Directorate, Federal 

Aviation Administration, 600 

Independence Avenue SW, Washington, 

DC 20597; telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

Authority for This Rulemaking 

The FAA’s authority to issue rules 

regarding aviation safety is found in 

Title 49 of the United States Code. 

Subtitle I, section 106 describes the 

authority of the FAA Administrator. 

Subtitle VII, Aviation Programs, 

describes in more detail the scope of the 

agency’s authority. This rulemaking is 

promulgated under the authority 

described in Subtitle VII, Part A, 

Subpart I, section 40103. Under that 

section, the FAA is charged with 

prescribing regulations to assign the use 

of the airspace necessary to ensure the 

safety of aircraft and the efficient use of 

airspace. This regulation is within the 

scope of that authority as it amends the 

route structure to maintain the efficient 

flow of air traffic within the National 

Airspace System (NAS). 

Comments Invited 

The FAA invites interested persons to 

participate in this rulemaking by 

submitting written comments, data, or 

views. Comments are specifically 

invited on the overall regulatory, 

aeronautical, economic, environmental, 

and energy-related aspects of the 

proposal. The most helpful comments 

reference a specific portion of the 

proposal, explain the reason for any 

recommended change, and include 

supporting data. To ensure the docket 

does not contain duplicate comments, 

commenters should submit only one 

time if comments are filed 

electronically, or commenters should 

send only one copy of written 

comments if comments are filed in 

writing. 

The FAA will file in the docket all 

comments it receives, as well as a report 

summarizing each substantive public 

contact with FAA personnel concerning 

this proposed rulemaking. Before acting 

on this proposal, the FAA will consider 

all comments it receives on or before the 

closing date for comments. The FAA 

will consider comments filed after the 

comment period has closed if it is 

possible to do so without incurring 

expense or delay. The FAA may change 

this proposal in light of the comments 

it receives. 

Privacy: In accordance with 5 U.S.C. 

553(c), DOT solicits comments from the 

public to better inform its rulemaking 

process. DOT posts these comments, 

without edit, including any personal 

information the commenter provides, to 

www.regulations.gov, as described in 

the system of records notice (DOT/ALL– 

14 FDMS), which can be reviewed at 

www.dot.gov/privacy. 

Availability of Rulemaking Documents 

An electronic copy of this document 

may be downloaded through the 

internet at www.regulations.gov. 

Recently published rulemaking 

documents can also be accessed through 

the FAA’s web page at www.faa.gov/air_

traffic/publications/airspace_

amendments/. 

You may review the public docket 

containing the proposal, any comments 

received and any final disposition in 

person in the Dockets Operations office 

(see ADDRESSES section for address, 

phone number, and hours of 

operations). An informal docket may 

also be examined during normal 

business hours at the office of the 

Eastern Service Center, Federal Aviation 

Administration, Room 210, 1701 

Columbia Avenue, College Park, GA 

30337. 


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