63502 Federal Register / Vol. 79, No. 206 / Friday, October 24, 2014 / Rules and Regulations 

(e) * * * 

(1) Three preliminary copies of each 

information statement, proxy statement, 

form of proxy, and other item of 

soliciting material to be furnished to 

security holders concurrently therewith, 

shall be filed with the FDIC by the bank, 

State savings association, or any other 

person making a solicitation subject to 

12 CFR 335.401 at least ten calendar 

days (or 15 calendar days in the case of 

other than routine meetings, as defined 

in paragraph (e)(2) of this section) prior 

to the date such item is first sent or 

given to any security holders, or such 

shorter date as may be authorized. 

(2) * * * 

(i) A meeting with respect to which 

no one is soliciting proxies subject to 12 

CFR 335.401 other than on behalf of the 

bank or State savings association and at 

which the bank or State savings 

association intends to present no 

matters other than: 

* * * * * 

(ii) The bank or State savings 

association does not comment upon or 

refer to a solicitation in opposition (as 

defined in 17 CFR 240.14a–6) in 

connection with the meeting in its 

proxy material. 

(f) * * * 

(2) The FDIC may, upon the written 

request of the bank or State savings 

association, and where consistent with 

the protection of investors, permit the 

omission of one or more of the 

statements or disclosures herein 

required, or the filing in substitution 

therefor of appropriate statements or 

disclosures of comparable character. 

* * * * * 

§ 335.901 [Removed] 

■ 8. Remove § 335.901. 

PART 390—REGULATIONS 

TRANSFERRED FROM THE OFFICE OF 

THRIFT SUPERVISION 

■ 9. The authority citation for part 390 

is revised to read as follows: 

Authority: 12 U.S.C. 1819. 

Subpart B also issued under 12 U.S.C. 

1818. 

Subpart C also issued under 5 U.S.C. 504; 

554–557; 12 U.S.C. 1464; 1467; 1468; 1817; 

1818; 1820; 1829; 3349, 4717; 15 U.S.C. 78l; 

78o–5; 78u–2; 28 U.S.C. 2461 note; 31 U.S.C. 

5321; 42 U.S.C. 4012a. 

Subpart D also issued under 12 U.S.C. 

1817; 1818; 1820; 15 U.S.C. 78l. 

Subpart E also issued under 12 U.S.C. 

1813; 1831m; 15 U.S.C. 78. 

Subpart F also issued under 5 U.S.C. 552; 

559; 12 U.S.C. 2901 et seq. 

Subpart G also issued under 12 U.S.C. 2810 

et seq., 2901 et seq.; 15 U.S.C. 1691; 42 U.S.C. 

1981, 1982, 3601–3619. 

Subpart I also issued under 12 U.S.C. 

1831x. 

Subpart J also issued under 12 U.S.C. 

1831p–1. 

Subpart L also issued under 12 U.S.C. 

1831p–1. 

Subpart M also issued under 12 U.S.C. 

1818. 

Subpart N also issued under 12 U.S.C. 

1821. 

Subpart O also issued under 12 U.S.C. 

1828. 

Subpart P also issued under 12 U.S.C. 

1470; 1831e; 1831n; 1831p–1; 3339. 

Subpart Q also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464. 

Subpart R also issued under 12 U.S.C. 

1463; 1464; 1831m; 1831n; 1831p–1. 

Subpart S also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1468a; 1817; 1820; 

1828; 1831e; 1831o; 1831p–1; 1881–1884; 

3207; 3339; 15 U.S.C. 78b; 78l; 78m; 78n; 

78p; 78q; 78w; 31 U.S.C. 5318; 42 U.S.C. 

4106. 

Subpart T also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78l; 78m; 

78n; 78w. 

Subpart V also issued under 12 U.S.C. 

3201–3208. 

Subpart W also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78l; 78m; 

78n; 78p; 78w. 

Subpart X also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828; 3331 et seq. 

Subpart Y also issued under 12 U.S.C. 

1831o. 

Subpart Z also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828 (note). 

Subpart U [Removed and Reserved] 

■ 10. Remove and reserve part 390 

subpart U consisting of §§ 390.390 

through 390.395. 

■ 11. In § 390.321, revise paragraph 

(b)(2) to read as follows: 

§ 390.321 Regulatory reports. 

* * * * * 

(b) * * * 

(2) Exceptions. Regulatory reporting 

requirements that are not consistent 

with GAAP, if any, are not required to 

be reflected in the audited financial 

statements, including financial 

statements contained in securities 

filings submitted to the FDIC pursuant 

to the Securities Exchange Act of 1934 

or subpart W and 12 CFR part 192. 

* * * * * 

§ 390.380 [Amended] 

■ 12. In § 390.380, remove paragraph 

(a)(3). 

Dated at Washington, DC, this 21st day of 

October, 2014. 

By order of the Board of Directors, Federal 

Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2014–25336 Filed 10–23–14; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0292; Directorate 

Identifier 2014–CE–011–AD; Amendment 

39–18001; AD 2014–15–02 R1] 

RIN 2120–AA64 

Airworthiness Directives; FiberglasTechnik Rudolf Lindner GmbH & Co. 

KG Gliders 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG (type certificates 

formerly held by GROB–WERKE GMBH 

& CO KG and BURKHART GROB LUFTUND RAUMFAHRT GmbH & CO KG) 

Models G102 STANDARD ASTIR III, 

G102 CLUB ASTIR III, G102 CLUB 

ASTIR IIIb, G103 TWIN II, G103A TWIN 

II ACRO, G103C TWIN III ACRO, and G 

103 C Twin III SL gliders. This AD 

revises AD 2014–15–02, which required 

inspection of the rudder control unit for 

installation of plastic cable pulleys and 

replacement of plastic cable pulleys 

with aluminum cable pulleys. This AD 

retains the actions of AD 2014–15–02 

but clarifies the suffixes of serial 

numbers (S/Ns) in paragraph (c) 

Applicability. This AD was prompted 

by reports of plastic control cable 

pulleys developing cracks due to aging, 

which could lead to breaking of the 

pulley and potentially jamming the 

rudder control unit, possibly resulting 

in loss of control. We are issuing this 

AD to require actions to address the 

unsafe condition on these products. 

DATES: This final rule is effective 

October 24, 2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of August 27, 2014 (79 FR 42658, July 

23, 2014). 

We must receive comments on this 

AD by December 8, 2014. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://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. 


rmajette on DSK2TPTVN1PROD with RULES
Federal Register / Vol. 79, No. 206 / Friday, October 24, 2014 / Rules and Regulations 63503 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this AD, contact Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG, Steige 

3, D–88487 Walpertshofen, Germany; 

telephone: +49 (0) 7353/22 43; fax: +49 

(0) 7353/30 96; email: info@LTBLindner.com; Web site: http://www.ltblindner.com/home.104.html. You may 

view this referenced service information 

at the FAA, Small Airplane Directorate, 

901 Locust, Kansas City, Missouri 

64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0292; or in person at the Docket 

Management Facility between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (telephone (800) 647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: jim.rutherford@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On July 14, 2014, we issued AD 2014– 

15–02, Amendment 39–17904 (79 FR 

42658, July 23, 2014), for GROB– 

WERKE GMBH & CO KG Models G102 

STANDARD ASTIR III, G102 CLUB 

ASTIR III, and G102 CLUB ASTIR IIIb 

gliders and BURKHART GROB LUFT— 

UND RAUMFAHRT GmbH & CO KG 

Models G103 TWIN II, G103A TWIN II 

ACRO, G103C TWIN III ACRO, and G 

103 C Twin III SL gliders. That AD 

required inspection of the rudder 

control unit for installation of plastic 

cable pulleys and replacement of plastic 

cable pulleys with aluminum cable 

pulleys. That AD resulted from reports 

of plastic control cable pulleys 

developing cracks due to aging, which 

could lead to breaking of the pulley and 

potentially jamming the rudder control 

unit, possibly resulting in loss of 

control. We issued that AD to require 

actions to address the unsafe condition 

on these products. 

Actions Since AD Was Issued 

Since we issued AD 2014–15–02 (79 

FR 42658, July 23, 2014), it was 

determined that to avoid any confusion 

regarding applicability to a given glider, 

the AD should be revised to include 

references to certain suffixes of S/Ns in 

paragraph (c) Applicability. 

Relevant Service Information 

We reviewed Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG Service 

Bulletin SB–G05, dated January 17, 

2014; and Fiberglas-Technik Rudolf 

Lindner GmbH & Co. KG Instructions A/ 

I–G05, dated January 17, 2014. The 

service information describes 

procedures for inspection of the rudder 

control unit for installation of plastic 

cable pulleys and replacement of plastic 

cable pulleys with aluminum cable 

pulleys. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all the relevant information 

and determined that to avoid any 

confusion about applicability to a given 

glider, AD 2014–15–02 (79 FR 42658, 

July 23, 2014) should be revised to 

include references to certain suffixes of 

S/Ns in paragraph (c) Applicability. 

AD Requirements 

This AD requires accomplishing the 

actions specified in the service 

information described previously. 

Change to Existing AD 

This AD retains all requirements of 

AD 2014–15–02 (79 FR 42658, July 23, 

2014), but revises paragraph (c) 

Applicability to include references to 

certain suffixes in referenced S/Ns of 

gliders. 

FAA’s Justification and Determination 

of the Effective Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. We received no comments on the 

previous AD, and this action only 

clarifies the applicability to a given 

glider and does not add any actions that 

increase the burden over the previous 

AD. Therefore, we find that notice and 

opportunity for prior public comment 

are unnecessary and that good cause 

exists for making this amendment 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not provide you with notice and 

an opportunity to provide your 

comments before it becomes effective. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include the docket number 

FAA–2014–0292 and directorate 

identifier 2014–CE–011–AD at the 

beginning of your comments. We 

specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this AD because of those 

comments. 

We will post all comments we 

receive, without change, to http://

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD will affect 

118 products of U.S. registry. We also 

estimate that it would take about .5 

work-hour per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $5,015, or $42.50 per product. 

In addition, we estimate that any 

necessary follow-on actions would take 

about 2 work-hours and require parts 

costing $244, for a cost of $414 per 

product. We have no way of 

determining the number of products 

that may need these actions. 

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. 

We are 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. 


rmajette on DSK2TPTVN1PROD with RULES
63504 Federal Register / Vol. 79, No. 206 / Friday, October 24, 2014 / Rules and Regulations 

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, 

(2) Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) Will 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. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends part 39 of the Federal 

Aviation Regulations (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 

removing airworthiness directive (AD) 

2014–15–02 (79 FR 42658, July 23, 

2014) and adding the following new AD: 

2014–15–02 R1 Fiberglas-Technik Rudolf 

Lindner GmbH & Co. KG (type 

certificates formerly held by GROB– 

WERKE GMBH & CO KG and 

BURKHART GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG): 

Amendment 39–18001; Docket No. 

FAA–2014–0292; Directorate Identifier 

2014–CE–011–AD. 

(a) Effective Date 

This AD is effective October 24, 2014. 

(b) Affected ADs 

This AD revises AD 2014–15–02 (79 FR 

42658, July 23, 2014) Amendment 39–17904. 

(c) Applicability 

This AD applies to the following model 

and serial number Fiberglas-Technik Rudolf 

Lindner GmbH & Co. KG (type certificates 

formerly held by GROB–WERKE GMBH & CO 

KG and BURKHART GROB LUFT-UND 

RAUMFAHRT GmbH & CO KG) gliders, 

certificated in any category. 

(1) G102 STANDARD ASTIR III, S/N 5501 

through 5652 (Suffix ‘‘S’’). 

(2) G102 CLUB ASTIR III, S/N 5501 

through 5652 (Suffix ‘‘C’’). 

(3) G102 CLUB ASTIR IIIb, S/N 5501 

through 5652 (Suffix ‘‘Cb’’). 

(4) G103 TWIN II, S/N 3730 through 34078. 

(5) G103A TWIN II ACRO, S/N 3730 

through 34078 (Suffix ‘‘K’’). 

(6) G103C TWIN III ACRO, S/N 34101 

through 34203. 

(7) G 103 C Twin III SL, S/N 35002 through 

35051. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

originated by an aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as plastic 

control cable pulleys developing cracks due 

to aging. We are issuing this AD to detect and 

correct plastic control cable pulleys in the 

rudder control unit, which could lead to 

breaking of the pulley and potentially 

jamming the rudder control unit, possibly 

resulting in loss of control of the glider. 

(f) Actions and Compliance 

Comply with this AD within the 

compliance times specified in paragraphs 

(f)(1) through (f)(3) of this AD, unless already 

done. 

(1) For all Models G103C TWIN III ACRO 

and G 103 C Twin III SL gliders: Within 3 

months after August 27, 2014 (the effective 

date retained from AD 2014–15–02, 

Amendment 39–17904 (79 FR 42658, July 23, 

2014)), inspect the rudder control unit for 

installation of plastic cable pulleys. If plastic 

cable pulleys are installed, before further 

flight, replace the plastic cable pulleys with 

aluminum cable pulleys following the 

actions and instructions of Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG Service 

Bulletin SB–G05 and Fiberglas-Technik 

Rudolf Lindner GmbH & Co. KG Instructions 

A/I–G05, both dated January 17, 2014. 

(2) For all Models G102 STANDARD 

ASTIR III, G102 CLUB ASTIR III, G102 CLUB 

ASTIR IIIb, G103 TWIN II, and G103A TWIN 

II ACRO gliders: Within 1 month after August 

27, 2014 (the effective date retained from AD 

2014–15–02, Amendment 39–17904 (79 FR 

42658, July 23, 2014)), inspect the rudder 

control unit for installation of plastic cable 

pulleys. If plastic cable pulleys are installed, 

before further flight, replace the plastic cable 

pulleys with aluminum cable pulleys 

following the actions and instructions of 

Fiberglas-Technik Rudolf Lindner GmbH & 

Co. KG Service Bulletin SB–G05 and 

Fiberglas-Technik Rudolf Lindner GmbH & 

Co. KG Instructions A/I–G05, both dated 

January 17, 2014. 

(3) As of August 27, 2014 (the effective 

date retained from AD 2014–15–02, 

Amendment 39–17904 (79 FR 42658, July 23, 

2014)), do not install any plastic control 

cable pulley in the rudder control unit of any 

glider identified in paragraphs (c)(1) through 

(c)(7) of this AD. 

(g) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Jim Rutherford, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 329– 

4090; email: jim.rutherford@faa.gov. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(h) Related Information 

Refer to European Aviation Safety Agency 

(EASA) AD No.: 2014–0067, dated March 18, 

2014, for related information. The MCAI can 

be found in the AD docket on the Internet at: 

http://www.regulations.gov/

#!documentDetail;D=FAA-2014-0292-0002. 

(i) 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 the AD specifies otherwise. 

(3) The following service information was 

approved for IBR on August 27, 2014 (79 FR 

42658, July 23, 2014). 

(i) Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG Service Bulletin SB–G05, 

dated January 17, 2014. 

(ii) Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG Instructions A/I–G05, dated 

January 17, 2014. 

(4) For Fiberglas-Technik Rudolf Lindner 

GmbH & Co. KG service information 

identified in this AD, contact FiberglasTechnik Rudolf Lindner GmbH & Co. KG, 

Steige 3, D–88487 Walpertshofen, Germany; 

telephone: +49 (0) 7353/22 43; fax: +49 (0) 

7353/30 96; email: info@LTB-Lindner.com; 

Web site: http://www.ltb-lindner.com/

home.104.html. 

(5) You may view this service information 

at the FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. 

(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, call 


rmajette on DSK2TPTVN1PROD with RULES
Federal Register / Vol. 79, No. 206 / Friday, October 24, 2014 / Rules and Regulations 63505 

202–741–6030, or go to: http://

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

Issued in Kansas City, Missouri, on 

October 15, 2014. 

Derek Morgan, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–25287 Filed 10–23–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No. 30985; Amdt. No. 516] 

IFR Altitudes; Miscellaneous 

Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This amendment adopts 

miscellaneous amendments to the 

required IFR (instrument flight rules) 

altitudes and changeover points for 

certain Federal airways, jet routes, or 

direct routes for which a minimum or 

maximum en route authorized IFR 

altitude is prescribed. This regulatory 

action is needed because of changes 

occurring in the National Airspace 

System. These changes are designed to 

provide for the safe and efficient use of 

the navigable airspace under instrument 

conditions in the affected areas. 

DATES: Effective Date: 0901 UTC, 

November 13, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Harry Hodges, Flight Procedure 

Standards Branch (AMCAFS–420), 

Flight Technologies and Programs 

Division, Flight Standards Service, 

Federal Aviation Administration, Mike 

Monroney Aeronautical Center, 6500 

South MacArthur Blvd. Oklahoma City, 

OK 73169 (Mail Address: P.O. Box 

25082 Oklahoma City, OK. 73125) 

telephone: (405) 954–4164. 

SUPPLEMENTARY INFORMATION: This 

amendment to part 95 of the Federal 

Aviation Regulations (14 CFR part 95) 

amends, suspends, or revokes IFR 

altitudes governing the operation of all 

aircraft in flight over a specified route 

or any portion of that route, as well as 

the changeover points (COPs) for 

Federal airways, jet routes, or direct 

routes as prescribed in part 95. 

The Rule 

The specified IFR altitudes, when 

used in conjunction with the prescribed 

changeover points for those routes, 

ensure navigation aid coverage that is 

adequate for safe flight operations and 

free of frequency interference. The 

reasons and circumstances that create 

the need for this amendment involve 

matters of flight safety and operational 

efficiency in the National Airspace 

System, are related to published 

aeronautical charts that are essential to 

the user, and provide for the safe and 

efficient use of the navigable airspace. 

In addition, those various reasons or 

circumstances require making this 

amendment effective before the next 

scheduled charting and publication date 

of the flight information to assure its 

timely availability to the user. The 

effective date of this amendment reflects 

those considerations. In view of the 

close and immediate relationship 

between these regulatory changes and 

safety in air commerce, I find that notice 

and public procedure before adopting 

this amendment are impracticable and 

contrary to the public interest and that 

good cause exists for making the 

amendment effective in less than 30 

days. 

Conclusion 

The FAA has determined that this 

regulation only involves an established 

body of technical regulations for which 

frequent and routine amendments are 

necessary to keep them operationally 

current. It, therefore—(1) is not a 

‘‘significant regulatory action’’ under 

Executive Order 12866; (2) is not a 

‘‘significant rule’’ under DOT 

Regulatory Policies and Procedures (44 

FR 11034; February 26, 1979); and (3) 

does not warrant preparation of a 

regulatory evaluation as the anticipated 

impact is so minimal. For the same 

reason, the FAA certifies that this 

amendment will not have a significant 

economic impact on a substantial 

number of small entities under the 

criteria of the Regulatory Flexibility Act. 

List of Subjects in 14 CFR Part 95 

Airspace, Navigation (air). 

Issued in Washington, DC, on October 9, 

2014. 

John Duncan, 

Director, Flight Standards Service. 

Adoption of the Amendment 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, part 95 of the Federal 

Aviation Regulations (14 CFR part 95) is 

amended as follows effective at 0901 

UTC, November 13, 2014. 

■ 1. The authority citation for part 95 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40103, 40106, 

40113, 40114, 40120, 44502, 44514, 44719, 

44721. 

■ 2. Part 95 is amended to read as 

follows: 

PART 95—[AMENDED] 

REVISIONS TO IFR ALTITUDES & CHANGEOVER POINT AMENDMENT 516 

[Effective date November 13, 2014] 

From To MEA MAA 

§ 95.3000 Low Altitude RNAV Routes 

§ 95.3295 RNAV Route T295 is Amended to Delete 

BANGOR, ME VORTAC ................................................... PRINCETON, ME VOR/DME ........................................... 3100 17500 

§ 95.3325 RNAV Route T325 is Added to Read 

BOWLING GREEN, KY VORTAC .................................... RENRO, KY FIX ............................................................... *4500 17500 

*2400—MOCA 

RENRO, KY FIX ............................................................... LOONE, KY FIX ............................................................... *4500 17500 

*2100—MOCA 

LOONE, KY FIX ................................................................ APALO, IN FIX ................................................................. *4500 17500 

*2100—MOCA 

APALO, IN FIX .................................................................. BUNKA, IN FIX ................................................................ 2500 17500 

BUNKA, IN FIX ................................................................. TERRE HAUTE, IN VORTAC .......................................... 2400 17500 


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